API tools faq
paste
MAKS_Enjoyer

Operational Functional Block Data

MAKS_Enjoyer
Sep 19th, 2022
82
0
Never
Add comment
Not a member of Pastebin yet? Sign Up, it unlocks many cool features!
text 122.93 KB | None | 0 0
raw download clone embed print report
  1. Your Engine is called: RS-177m "Elektron"
  2. Your Engine Cycle is: Staged Combustion (Fuel Rich)
  3. Your Oxidizer is: O3 (Ozone)
  4. Your Fuel is: H2 (Hydrogen)
  5. Your engine's nozzle type should be: Expanding Nozzle
  6. Your Altitude of operation is: 80 km+ (Vacuum)
  7. Tank repressurisation would be done Autogenously
  8. The Cooling Mechanism to be used would be Ablative Cooling
  9.  
  10.  
  11. Your Engine is called: CE-178K "Granis"
  12. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  13. Your Propellant is: Krypton
  14. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  15. Your Altitude of operation is: 80 km+ (Vacuum)
  16. Tank repressurisation would be impractical and unnecessary
  17. The Cooling Mechanism to be used would be Transpiration Cooling
  18.  
  19.  
  20. Your Engine is called: XLR-1005P "Yars"
  21. Your Engine Cycle is: Gridded Ion Thruster
  22. Your Propellant is: Mercury
  23. Your engine's nozzle type should be: Electrostatic Ion Nozzle
  24. Your Altitude of operation is: 80 km+ (Vacuum)
  25. Tank repressurisation would be impractical and unnecessary
  26. The Cooling Mechanism to be used would be Regenerative Cooling
  27.  
  28.  
  29. Your Engine is called: MV-292J "Proton"
  30. Your Engine Cycle is: "Expander Open" Pulsed Nuclear
  31. Your Propellant is: Water (H2O)
  32. Your Reactor's Fission Fuel is: 100-90% Uranium-235
  33. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  34. Your Altitude of operation is: 80 km+ (Vacuum)
  35. Tank repressurisation would be done Autogenously
  36. The Cooling Mechanism to be used would be Dump Cooling
  37.  
  38.  
  39. Your Engine is called: LE-62R "Rubin"
  40. Your Engine Cycle is: "Expander Open" Pulsed Nuclear
  41. Your Propellant is: Ammonia (NH3)
  42. Your Reactor's Fission Fuel is: 25-8% Plutonium-238
  43. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  44. Your Altitude of operation is: 80 km+ (Vacuum)
  45. Tank repressurisation would be done using Inert gas
  46. The Cooling Mechanism to be used would be Dump Cooling
  47.  
  48.  
  49. Your Engine is called: AR-723Z "Ariane"
  50. Your Engine Cycle is: Monopropellant (Decomposition)
  51. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  52. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  53. Your Altitude of operation is: 80 km+ (Vacuum)
  54. Tank repressurisation would be impractical and unnecessary
  55. The Cooling Mechanism to be used would be Ablative Cooling
  56.  
  57.  
  58. Your Engine is called: RS-820t "Convair"
  59. Your Engine Cycle is: Colloid Thruster
  60. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  61. Your engine's nozzle type should be: Capillary Emitter-Electrode Cone
  62. Your Altitude of operation is: 80 km+ (Vacuum)
  63. Tank repressurisation would be impractical and unnecessary
  64. The Cooling Mechanism to be used would be Transpiration Cooling
  65.  
  66.  
  67. Your Engine is called: BE-764Y "Tethys"
  68. Your Engine Cycle is: Expander (Closed)
  69. Your Oxidizer is: O3 (Ozone)
  70. Your Fuel is: C12H24 (Kerosene)
  71. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  72. Your Altitude of operation is: 80 km+ (Vacuum)
  73. Tank repressurisation would be done Autogenously
  74. The Cooling Mechanism to be used would be Regenerative Cooling
  75.  
  76.  
  77. Your Engine is called: HM-387G "Python"
  78. Your Engine Cycle is: Expander (Open/Bleed)
  79. Your Oxidizer is: O2 (Oxygen)
  80. Your Fuel is: B5H9 (Pentaborane)
  81. Your engine's nozzle type should be: Linear Aerospike Nozzle
  82. Your Altitude of operation is: Any Altitude (0-80 km+)
  83. Tank repressurisation would be done Autogenously
  84. The Cooling Mechanism to be used would be Film Cooling
  85.  
  86.  
  87. Your Engine is called: CE-281G "Minotaur"
  88. Your Engine Cycle is: Gas Generator
  89. Your Oxidizer is: AK20I: 80% HNO3 + 20% N2O4 (Nitric Acid)
  90. Your Fuel is: C2H5OH(Ethanol) 85%
  91. Your engine's nozzle type should be: Expanding Nozzle
  92. Your Altitude of operation is: 80 km+ (Vacuum)
  93. Tank repressurisation would be done using Inert gas
  94. The Cooling Mechanism to be used would be Radiative Cooling
  95.  
  96.  
  97. Your Engine is called: DOK-69T "Gamma"
  98. Your Engine Cycle is: Nuclear SaltWater
  99. Your Propellant is: Uranium TetraBromide (UBr4) + Water (H2O)
  100. Your Reactor's Fission Fuel is: 50% Uranium-235
  101. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  102. Your Altitude of operation is: 80 km+ (Vacuum)
  103. Tank repressurisation would be done Autogenously
  104. The Cooling Mechanism to be used would be Transpiration Cooling
  105.  
  106.  
  107. Your Engine is called: XLR-995J "Sokol"
  108. Your Engine Cycle is: Staged Combustion (Oxidizer Rich)
  109. Your Oxidizer is: O2 (Oxygen)
  110. Your Fuel is: C2H5OH(Ethanol) 85%
  111. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  112. Your Altitude of operation is: 80 km+ (Vacuum)
  113. Tank repressurisation would be done using Inert gas
  114. The Cooling Mechanism to be used would be Film Cooling
  115.  
  116.  
  117. Your Engine is called: RD-543F "Cassini"
  118. Your Engine Cycle is: Combustion Tap Off
  119. Your Oxidizer is: O2 (Oxygen)
  120. Your Fuel is: C2H5OH(Ethanol) 85%
  121. Your engine's nozzle type should be: Expansion-Deflection Nozzle
  122. Your Altitude of operation is: Any Altitude (0-80 km+)
  123. Tank repressurisation would be done using Inert gas
  124. The Cooling Mechanism to be used would be Dump Cooling
  125.  
  126.  
  127. Your Engine is called: RD-537M "Ithacus"
  128. Your Engine Cycle is: "Expander Open" Liquid Core
  129. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Hydrogen (H2) + Hexane (C6H14) as a remass
  130. Your Reactor's Fission Fuel is: 100-90% Uranium-235
  131. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  132. Your Altitude of operation is: 80 km+ (Vacuum)
  133. Tank repressurisation would be done using Inert gas
  134. The Cooling Mechanism to be used would be Film Cooling
  135.  
  136.  
  137. Your Engine is called: LM10-369V "Icarus"
  138. Your Engine Cycle is: "Expander Closed" Pulsed Nuclear
  139. Your Propellant is: Carbon Monoxide (CO)
  140. Your Reactor's Fission Fuel is: 20-8% Uranium-235
  141. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  142. Your Altitude of operation is: 80 km+ (Vacuum)
  143. Tank repressurisation would be done using Inert gas
  144. The Cooling Mechanism to be used would be Dump Cooling
  145.  
  146.  
  147. Your Engine is called: KDU-210x "Starshot"
  148. Your Engine Cycle is: Hall Effect Thruster
  149. Your Propellant is: Bismuth
  150. Your engine's nozzle type should be: Hall Effect Thruster Nozzle
  151. Your Altitude of operation is: 80 km+ (Vacuum)
  152. Tank repressurisation would be impractical and unnecessary
  153. The Cooling Mechanism to be used would be Radiative Cooling
  154.  
  155.  
  156. Your Engine is called: TQ-701s "Harmony"
  157. Your Engine Cycle is: Pressure-Fed
  158. Your Oxidizer is: AK27I: 73% HNO3 + 27% N2O4 (Nitric Acid)
  159. Your Fuel is: CH6N2 (MonomethylHydrazine)
  160. Your engine's nozzle type should be: Dual Bell Nozzle
  161. Your Altitude of operation is: 30-80 km (High Atmosphere)
  162. Tank repressurisation would be done using Inert gas
  163. The Cooling Mechanism to be used would be Transpiration Cooling
  164.  
  165.  
  166. Your Engine is called: TQ-293X "Colombus"
  167. Your Engine Cycle is: Dual Expander (Closed)
  168. Your Oxidizer is: O2 (Oxygen)
  169. Your Fuel is: H2 (Hydrogen)
  170. Your engine's nozzle type should be: Linear Aerospike Nozzle
  171. Your Altitude of operation is: Any Altitude (0-80 km+)
  172. Tank repressurisation would be done Autogenously
  173. The Cooling Mechanism to be used would be Regenerative Cooling
  174.  
  175.  
  176. Your Engine is called: BE-389S "Fram"
  177. Your Engine Cycle is: "Expander Open" Pulsed Nuclear
  178. Your Propellant is: Ammonia (NH3)
  179. Your Reactor's Fission Fuel is: 1-2% Plutonium-238
  180. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  181. Your Altitude of operation is: 80 km+ (Vacuum)
  182. Tank repressurisation would be done Autogenously
  183. The Cooling Mechanism to be used would be Regenerative Cooling
  184.  
  185.  
  186. Your Engine is called: KRD-606E "Yars"
  187. Your Engine Cycle is: Monopropellant (Decomposition)
  188. Your Propellant is: N2H4 (Hydrazine)
  189. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  190. Your Altitude of operation is: 80 km+ (Vacuum)
  191. Tank repressurisation would be impractical and unnecessary
  192. The Cooling Mechanism to be used would be Ablative Cooling
  193.  
  194.  
  195. Your Engine is called: RD-339z "Ingenuity"
  196. Your Engine Cycle is: Colloid Thruster
  197. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  198. Your engine's nozzle type should be: Capillary Emitter-Electrode Cone
  199. Your Altitude of operation is: 80 km+ (Vacuum)
  200. Tank repressurisation would be impractical and unnecessary
  201. The Cooling Mechanism to be used would be Dump Cooling
  202.  
  203.  
  204. Your Engine is called: AR-262F "Themis"
  205. Your Engine Cycle is: Nuclear SaltWater
  206. Your Propellant is: Uranium TetraBromide (UBr4) + Water (H2O)
  207. Your Reactor's Fission Fuel is: 100-90% Uranium-235
  208. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  209. Your Altitude of operation is: 80 km+ (Vacuum)
  210. Tank repressurisation would be done using Inert gas
  211. The Cooling Mechanism to be used would be Film Cooling
  212.  
  213.  
  214. Your Engine is called: RS-149m "Hera"
  215. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  216. Your Propellant is: Xenon
  217. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  218. Your Altitude of operation is: 80 km+ (Vacuum)
  219. Tank repressurisation would be impractical and unnecessary
  220. The Cooling Mechanism to be used would be Dump Cooling
  221.  
  222.  
  223. Your Engine is called: MV-1005y "Shtil"
  224. Your Engine Cycle is: Gas Generator
  225. Your Oxidizer is: O2 (Oxygen)
  226. Your Fuel is: C12H24 (Kerosene)
  227. Your engine's nozzle type should be: Expanding Nozzle
  228. Your Altitude of operation is: 80 km+ (Vacuum)
  229. Tank repressurisation would be done Autogenously
  230. The Cooling Mechanism to be used would be Film Cooling
  231.  
  232.  
  233. Your Engine is called: LRE-122L "Clementine"
  234. Your Engine Cycle is: Expander (Closed)
  235. Your Oxidizer is: F2 (Fluorine)
  236. Your Fuel is: NH3 (Ammonia)
  237. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  238. Your Altitude of operation is: 80 km+ (Vacuum)
  239. Tank repressurisation would be done Autogenously
  240. The Cooling Mechanism to be used would be Transpiration Cooling
  241.  
  242.  
  243. Your Engine is called: LM10-93G "Polyot"
  244. Your Engine Cycle is: Dual Expander (Open/Bleed)
  245. Your Oxidizer is: O2 (Oxygen)
  246. Your Fuel is: H2 (Hydrogen)
  247. Your engine's nozzle type should be: Linear Aerospike Nozzle
  248. Your Altitude of operation is: Any Altitude (0-80 km+)
  249. Tank repressurisation would be done Autogenously
  250. The Cooling Mechanism to be used would be Film Cooling
  251.  
  252.  
  253. Your Engine is called: R-278J "Dekto"
  254. Your Engine Cycle is: Nuclear SaltWater
  255. Your Propellant is: Uranium TetraBromide (UBr4) + Water (H2O)
  256. Your Reactor's Fission Fuel is: 50% Uranium-235
  257. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  258. Your Altitude of operation is: 80 km+ (Vacuum)
  259. Tank repressurisation would be done Autogenously
  260. The Cooling Mechanism to be used would be Transpiration Cooling
  261.  
  262.  
  263. Your Engine is called: XLR-49H "Obzor"
  264. Your Engine Cycle is: "Expander Closed" Pebble-Bed Core
  265. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Ammonia (NH3) as a remass
  266. Your Reactor's Fission Fuel is: 25-8% Uranium-235
  267. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  268. Your Altitude of operation is: 80 km+ (Vacuum)
  269. Tank repressurisation would be done using Inert gas
  270. The Cooling Mechanism to be used would be Transpiration Cooling
  271.  
  272.  
  273. Your Engine is called: NK-631p "Neutron"
  274. Your Engine Cycle is: "Expander Bleed" Pebble-Bed Core
  275. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Methane (CH4) as a remass
  276. Your Reactor's Fission Fuel is: 25-8% Uranium-235
  277. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  278. Your Altitude of operation is: 80 km+ (Vacuum)
  279. Tank repressurisation would be done Autogenously
  280. The Cooling Mechanism to be used would be Film Cooling
  281.  
  282.  
  283. Your Engine is called: RS-909B "Salyut"
  284. Your Engine Cycle is: Electric Pump Fed
  285. Your Oxidizer is: AK27I: 73% HNO3 + 27% N2O4 (Nitric Acid)
  286. Your Fuel is: CH6N2 (MonomethylHydrazine)
  287. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  288. Your Altitude of operation is: 80 km+ (Vacuum)
  289. Tank repressurisation would be done Autogenously
  290. The Cooling Mechanism to be used would be Ablative Cooling
  291.  
  292.  
  293. Your Engine is called: RS-875v "Electron"
  294. Your Engine Cycle is: Expander (Open/Bleed)
  295. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  296. Your Fuel is: N2H4 (Hydrazine)
  297. Your engine's nozzle type should be: Expansion-Deflection Nozzle
  298. Your Altitude of operation is: Any Altitude (0-80 km+)
  299. Tank repressurisation would be done Autogenously
  300. The Cooling Mechanism to be used would be Transpiration Cooling
  301.  
  302.  
  303. Your Engine is called: DOK-510y "Baikal"
  304. Your Engine Cycle is: MagnetoPlasmaDynamic Thruster
  305. Your Propellant is: Argon
  306. Your engine's nozzle type should be: Cathode Plug Magnetic Confinement Nozzle
  307. Your Altitude of operation is: 80 km+ (Vacuum)
  308. Tank repressurisation would be impractical and unnecessary
  309. The Cooling Mechanism to be used would be Transpiration Cooling
  310.  
  311.  
  312. Your Engine is called: KRD-397Y "Urgan"
  313. Your Engine Cycle is: Hall Effect Thruster
  314. Your Propellant is: Zinc
  315. Your engine's nozzle type should be: Hall Effect Thruster Nozzle
  316. Your Altitude of operation is: 80 km+ (Vacuum)
  317. Tank repressurisation would be impractical and unnecessary
  318. The Cooling Mechanism to be used would be Film Cooling
  319.  
  320.  
  321. Your Engine is called: KDTU-241v "Atlanta"
  322. Your Engine Cycle is: Full Flow Staged
  323. Your Oxidizer is: AK27P: 73% HNO3 + 27% N2O4 (Nitric Acid)
  324. Your Fuel is: C2H5OH(Ethanol) 85%
  325. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  326. Your Altitude of operation is: 80 km+ (Vacuum)
  327. Tank repressurisation would be done using Inert gas
  328. The Cooling Mechanism to be used would be Ablative Cooling
  329.  
  330.  
  331. Your Engine is called: AR-37S "Serenity"
  332. Your Engine Cycle is: Nuclear SaltWater
  333. Your Propellant is: Uranium TetraBromide (UBr4) + Water (H2O)
  334. Your Reactor's Fission Fuel is: 50% Uranium-235
  335. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  336. Your Altitude of operation is: 80 km+ (Vacuum)
  337. Tank repressurisation would be done Autogenously
  338. The Cooling Mechanism to be used would be Dump Cooling
  339.  
  340.  
  341. Your Engine is called: KDTU-94R "Hera"
  342. Your Engine Cycle is: Colloid Thruster
  343. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  344. Your engine's nozzle type should be: Capillary Emitter-Electrode Cone
  345. Your Altitude of operation is: 80 km+ (Vacuum)
  346. Tank repressurisation would be impractical and unnecessary
  347. The Cooling Mechanism to be used would be Film Cooling
  348.  
  349.  
  350. Your Engine is called: RD-920 "Yars"
  351. Your Engine Cycle is: "Vortex Confined" Liquid Core
  352. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Nitrogen (N2) as a remass
  353. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  354. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  355. Your Altitude of operation is: 80 km+ (Vacuum)
  356. Tank repressurisation would be done Autogenously
  357. The Cooling Mechanism to be used would be Regenerative Cooling
  358.  
  359.  
  360. Your Engine is called: AJ-187R "Nautilus"
  361. Your Engine Cycle is: "Expander Bleed" Solid Core
  362. Your Propellant is: Helium (He)
  363. Your Reactor's Fission Fuel is: 100-90% Plutonium-238
  364. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  365. Your Altitude of operation is: 80 km+ (Vacuum)
  366. Tank repressurisation would be done Autogenously
  367. The Cooling Mechanism to be used would be Radiative Cooling
  368.  
  369.  
  370. Your Engine is called: DST-434d "Oscar"
  371. Your Engine Cycle is: "Expander Bleed" Liquid Core
  372. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Water (H2O) as a remass
  373. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  374. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  375. Your Altitude of operation is: 80 km+ (Vacuum)
  376. Tank repressurisation would be done using Inert gas
  377. The Cooling Mechanism to be used would be Radiative Cooling
  378.  
  379.  
  380. Your Engine is called: AR-309x "Callisto"
  381. Your Engine Cycle is: Gridded Ion Thruster
  382. Your Propellant is: Caesium
  383. Your engine's nozzle type should be: Electrostatic Ion Nozzle
  384. Your Altitude of operation is: 80 km+ (Vacuum)
  385. Tank repressurisation would be impractical and unnecessary
  386. The Cooling Mechanism to be used would be Transpiration Cooling
  387.  
  388.  
  389. Your Engine is called: RD-171z "Malyutka"
  390. Your Engine Cycle is: Electric Pump Fed
  391. Your Oxidizer is: ClF5 (Chlorine Pentafluoride)
  392. Your Fuel is: C2H5OH(Ethanol) 85%
  393. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  394. Your Altitude of operation is: 0-10 km (Sea Level)
  395. Tank repressurisation would be done Autogenously
  396. The Cooling Mechanism to be used would be Radiative Cooling
  397.  
  398.  
  399. Your Engine is called: XS-366k "Gonets"
  400. Your Engine Cycle is: "Expander Bleed" Pebble-Bed Core
  401. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Methane (CH4) as a remass
  402. Your Reactor's Fission Fuel is: 25-8% Uranium-235
  403. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  404. Your Altitude of operation is: 80 km+ (Vacuum)
  405. Tank repressurisation would be done using Inert gas
  406. The Cooling Mechanism to be used would be Radiative Cooling
  407.  
  408.  
  409. Your Engine is called: AJ-498F "Thor"
  410. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  411. Your Propellant is: Argon
  412. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  413. Your Altitude of operation is: 80 km+ (Vacuum)
  414. Tank repressurisation would be impractical and unnecessary
  415. The Cooling Mechanism to be used would be Dump Cooling
  416.  
  417.  
  418. Your Engine is called: KDTU-250Z "Hera"
  419. Your Engine Cycle is: Expander (Open/Bleed)
  420. Your Oxidizer is: F2 (Fluorine)
  421. Your Fuel is: C2H5OH(Ethanol) 85%
  422. Your engine's nozzle type should be: Dual Bell Nozzle
  423. Your Altitude of operation is: 30-80 km (High Atmosphere)
  424. Tank repressurisation would be done Autogenously
  425. The Cooling Mechanism to be used would be Ablative Cooling
  426.  
  427.  
  428. Your Engine is called: XLR-442l "Contour"
  429. Your Engine Cycle is: "Expander Closed" Gas Core
  430. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Methane (CH4) as remass
  431. Your Reactor's Fission Fuel is: 25-8% Uranium-235
  432. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  433. Your Altitude of operation is: 80 km+ (Vacuum)
  434. Tank repressurisation would be done Autogenously
  435. The Cooling Mechanism to be used would be Regenerative Cooling
  436.  
  437.  
  438. Your Engine is called: MJ-115u "Tetrapoda"
  439. Your Engine Cycle is: Full Flow Staged
  440. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  441. Your Fuel is: CH3OH (Methanol)
  442. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  443. Your Altitude of operation is: 30-80 km (High Atmosphere)
  444. Tank repressurisation would be done using Inert gas
  445. The Cooling Mechanism to be used would be Radiative Cooling
  446.  
  447.  
  448. Your Engine is called: YF-100G "Sojourner"
  449. Your Engine Cycle is: Monopropellant (Decomposition)
  450. Your Propellant is: N2H4 (Hydrazine)
  451. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  452. Your Altitude of operation is: 80 km+ (Vacuum)
  453. Tank repressurisation would be impractical and unnecessary
  454. The Cooling Mechanism to be used would be Radiative Cooling
  455.  
  456.  
  457. Your Engine is called: AJ-854v "Clementine"
  458. Your Engine Cycle is: Electric Pump Fed
  459. Your Oxidizer is: AK20F: 80% HNO3 + 20% N2O4 (Nitric Acid)
  460. Your Fuel is: CH6N2 (MonomethylHydrazine)
  461. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  462. Your Altitude of operation is: 0-10 km (Sea Level)
  463. Tank repressurisation would be done Autogenously
  464. The Cooling Mechanism to be used would be Regenerative Cooling
  465.  
  466.  
  467. Your Engine is called: XS-258J "Zenit"
  468. Your Engine Cycle is: Colloid Thruster
  469. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  470. Your engine's nozzle type should be: Capillary Emitter-Electrode Cone
  471. Your Altitude of operation is: 80 km+ (Vacuum)
  472. Tank repressurisation would be impractical and unnecessary
  473. The Cooling Mechanism to be used would be Film Cooling
  474.  
  475.  
  476. Your Engine is called: KRD-164F "Archimedes"
  477. Your Engine Cycle is: Full Flow Staged
  478. Your Oxidizer is: AK20I: 80% HNO3 + 20% N2O4 (Nitric Acid)
  479. Your Fuel is: N2H4 (Hydrazine)
  480. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  481. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  482. Tank repressurisation would be done using Inert gas
  483. The Cooling Mechanism to be used would be Radiative Cooling
  484.  
  485.  
  486. Your Engine is called: LRE-641Y "Inertsiya"
  487. Your Engine Cycle is: Staged Combustion (Fuel Rich)
  488. Your Oxidizer is: O2 (Oxygen)
  489. Your Fuel is: NH3 (Ammonia)
  490. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  491. Your Altitude of operation is: 30-80 km (High Atmosphere)
  492. Tank repressurisation would be done using Inert gas
  493. The Cooling Mechanism to be used would be Dump Cooling
  494.  
  495.  
  496. Your Engine is called: HM-349M "Spitzer"
  497. Your Engine Cycle is: Expander (Open/Bleed)
  498. Your Oxidizer is: O2 (Oxygen)
  499. Your Fuel is: C2H5OH(Ethanol) 85%
  500. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  501. Your Altitude of operation is: 0-10 km (Sea Level)
  502. Tank repressurisation would be done Autogenously
  503. The Cooling Mechanism to be used would be Ablative Cooling
  504.  
  505.  
  506. Your Engine is called: HM-282G "Pratt"
  507. Your Engine Cycle is: Colloid Thruster
  508. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  509. Your engine's nozzle type should be: Capillary Emitter-Electrode Cone
  510. Your Altitude of operation is: 80 km+ (Vacuum)
  511. Tank repressurisation would be impractical and unnecessary
  512. The Cooling Mechanism to be used would be Film Cooling
  513.  
  514.  
  515. Your Engine is called: TQ-735E "Ingenuity"
  516. Your Engine Cycle is: Cold Gas Monopropellant
  517. Your Propellant is: Helium (He)
  518. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  519. Your Altitude of operation is: 80 km+ (Vacuum)
  520. Tank repressurisation would be impractical and unnecessary
  521. The Cooling Mechanism to be used would be unnecessary
  522.  
  523.  
  524. Your Engine is called: RS-920 "Chasovoy"
  525. Your Engine Cycle is: Pressure-Fed
  526. Your Oxidizer is: AK20K: 80% HNO3 + 20% N2O4 (Nitric Acid)
  527. Your Fuel is: N2H4 (Hydrazine)
  528. Your engine's nozzle type should be: Dual Bell Nozzle
  529. Your Altitude of operation is: 30-80 km (High Atmosphere)
  530. Tank repressurisation would be done using Inert gas
  531. The Cooling Mechanism to be used would be Radiative Cooling
  532.  
  533.  
  534. Your Engine is called: LM10-340n "Oscar"
  535. Your Engine Cycle is: Dual Expander (Closed)
  536. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  537. Your Fuel is: H2 (Hydrogen)
  538. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  539. Your Altitude of operation is: 30-80 km (High Atmosphere)
  540. Tank repressurisation would be done Autogenously
  541. The Cooling Mechanism to be used would be Film Cooling
  542.  
  543.  
  544. Your Engine is called: AR-830n "Araks"
  545. Your Engine Cycle is: Hall Effect Thruster
  546. Your Propellant is: Krypton
  547. Your engine's nozzle type should be: Hall Effect Thruster Nozzle
  548. Your Altitude of operation is: 80 km+ (Vacuum)
  549. Tank repressurisation would be impractical and unnecessary
  550. The Cooling Mechanism to be used would be Regenerative Cooling
  551.  
  552.  
  553. Your Engine is called: KRD-729u "Neutron"
  554. Your Engine Cycle is: Monopropellant (Decomposition)
  555. Your Propellant is: N2H4 (Hydrazine)
  556. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  557. Your Altitude of operation is: 80 km+ (Vacuum)
  558. Tank repressurisation would be impractical and unnecessary
  559. The Cooling Mechanism to be used would be Radiative Cooling
  560.  
  561.  
  562. Your Engine is called: NK-62M "Progress"
  563. Your Engine Cycle is: Expander (Open/Bleed)
  564. Your Oxidizer is: O3 (Ozone)
  565. Your Fuel is: C12H24 (Kerosene)
  566. Your engine's nozzle type should be: Expanding Nozzle
  567. Your Altitude of operation is: 80 km+ (Vacuum)
  568. Tank repressurisation would be done Autogenously
  569. The Cooling Mechanism to be used would be Dump Cooling
  570.  
  571.  
  572. Your Engine is called: XS-590F "Nautilus"
  573. Your Engine Cycle is: Electric Pump Fed
  574. Your Oxidizer is: AK20I: 80% HNO3 + 20% N2O4 (Nitric Acid)
  575. Your Fuel is: CH6N2 (MonomethylHydrazine)
  576. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  577. Your Altitude of operation is: 0-10 km (Sea Level)
  578. Tank repressurisation would be done Autogenously
  579. The Cooling Mechanism to be used would be Radiative Cooling
  580.  
  581.  
  582. Your Engine is called: RS-68G "Fortune"
  583. Your Engine Cycle is: Expander (Open/Bleed)
  584. Your Oxidizer is: F2 (Fluorine)
  585. Your Fuel is: C12H24 (Kerosene)
  586. Your engine's nozzle type should be: Dual Bell Nozzle
  587. Your Altitude of operation is: 30-80 km (High Atmosphere)
  588. Tank repressurisation would be done Autogenously
  589. The Cooling Mechanism to be used would be Film Cooling
  590.  
  591.  
  592. Your Engine is called: KDTU-26m "Nebula"
  593. Your Engine Cycle is: Expander (Closed)
  594. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  595. Your Fuel is: CH3OH (Methanol)
  596. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  597. Your Altitude of operation is: 30-80 km (High Atmosphere)
  598. Tank repressurisation would be done Autogenously
  599. The Cooling Mechanism to be used would be Ablative Cooling
  600.  
  601.  
  602. Your Engine is called: CE-543b "Melibea"
  603. Your Engine Cycle is: Expander (Open/Bleed)
  604. Your Oxidizer is: O2 (Oxygen)
  605. Your Fuel is: C6H5NH2 (Aniline)
  606. Your engine's nozzle type should be: Toroidal Aerospike Nozzle
  607. Your Altitude of operation is: Any Altitude (0-80 km+)
  608. Tank repressurisation would be done Autogenously
  609. The Cooling Mechanism to be used would be Radiative Cooling
  610.  
  611.  
  612. Your Engine is called: BE-490s "Carrack"
  613. Your Engine Cycle is: Staged Combustion (Fuel Rich)
  614. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  615. Your Fuel is: H2 (Hydrogen)
  616. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  617. Your Altitude of operation is: 0-10 km (Sea Level)
  618. Tank repressurisation would be done using Inert gas
  619. The Cooling Mechanism to be used would be Regenerative Cooling
  620.  
  621.  
  622. Your Engine is called: BE-599g "Vostok"
  623. Your Engine Cycle is: Hall Effect Thruster
  624. Your Propellant is: Iodine
  625. Your engine's nozzle type should be: Hall Effect Thruster Nozzle
  626. Your Altitude of operation is: 80 km+ (Vacuum)
  627. Tank repressurisation would be impractical and unnecessary
  628. The Cooling Mechanism to be used would be Radiative Cooling
  629.  
  630.  
  631. Your Engine is called: AR-242N "Pioneer"
  632. Your Engine Cycle is: "Magnetohydrodynamic(MHD) vortex" Gas Core
  633. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Ammonia (NH3) as remass
  634. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  635. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  636. Your Altitude of operation is: 80 km+ (Vacuum)
  637. Tank repressurisation would be done Autogenously
  638. The Cooling Mechanism to be used would be Dump Cooling
  639.  
  640.  
  641. Your Engine is called: NK-198l "Joist"
  642. Your Engine Cycle is: "Vortex Confined" Liquid Core
  643. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Hydrogen (H2) + Hexane (C6H14) as a remass
  644. Your Reactor's Fission Fuel is: 100-90% Uranium-235
  645. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  646. Your Altitude of operation is: 80 km+ (Vacuum)
  647. Tank repressurisation would be done using Inert gas
  648. The Cooling Mechanism to be used would be Regenerative Cooling
  649.  
  650.  
  651. Your Engine is called: CE-918A "Minerva"
  652. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  653. Your Propellant is: Xenon
  654. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  655. Your Altitude of operation is: 80 km+ (Vacuum)
  656. Tank repressurisation would be impractical and unnecessary
  657. The Cooling Mechanism to be used would be Transpiration Cooling
  658.  
  659.  
  660. Your Engine is called: RO-249v "Espadon"
  661. Your Engine Cycle is: "Expander Open" Solid Core
  662. Your Propellant is: Nitrogen (N2)
  663. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  664. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  665. Your Altitude of operation is: 80 km+ (Vacuum)
  666. Tank repressurisation would be done Autogenously
  667. The Cooling Mechanism to be used would be Radiative Cooling
  668.  
  669.  
  670. Your Engine is called: HM-241P "Emphasis"
  671. Your Engine Cycle is: Staged Combustion (Oxidizer Rich)
  672. Your Oxidizer is: O2 (Oxygen)
  673. Your Fuel is: N2H4 (Hydrazine)
  674. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  675. Your Altitude of operation is: 0-10 km (Sea Level)
  676. Tank repressurisation would be done Autogenously
  677. The Cooling Mechanism to be used would be Dump Cooling
  678.  
  679.  
  680. Your Engine is called: MJ-843k "Rhino"
  681. Your Engine Cycle is: Cold Gas Monopropellant
  682. Your Propellant is: Helium (He)
  683. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  684. Your Altitude of operation is: 80 km+ (Vacuum)
  685. Tank repressurisation would be impractical and unnecessary
  686. The Cooling Mechanism to be used would be unnecessary
  687.  
  688.  
  689. Your Engine is called: AR-748M "Contour"
  690. Your Engine Cycle is: Combustion Tap Off
  691. Your Oxidizer is: F2 (Fluorine)
  692. Your Fuel is: C2H5OH(Ethanol) 85%
  693. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  694. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  695. Tank repressurisation would be done using Inert gas
  696. The Cooling Mechanism to be used would be Radiative Cooling
  697.  
  698.  
  699. Your Engine is called: XS-670z "Kvant"
  700. Your Engine Cycle is: MagnetoPlasmaDynamic Thruster
  701. Your Propellant is: Neon
  702. Your engine's nozzle type should be: Cathode Plug Magnetic Confinement Nozzle
  703. Your Altitude of operation is: 80 km+ (Vacuum)
  704. Tank repressurisation would be impractical and unnecessary
  705. The Cooling Mechanism to be used would be Dump Cooling
  706.  
  707.  
  708. Your Engine is called: XS-321U "Surveyor"
  709. Your Engine Cycle is: Staged Combustion (Fuel Rich)
  710. Your Oxidizer is: O3 (Ozone)
  711. Your Fuel is: H2 (Hydrogen)
  712. Your engine's nozzle type should be: Expanding Nozzle
  713. Your Altitude of operation is: 80 km+ (Vacuum)
  714. Tank repressurisation would be done Autogenously
  715. The Cooling Mechanism to be used would be Film Cooling
  716.  
  717.  
  718. Your Engine is called: RS-108w "Kavkaz"
  719. Your Engine Cycle is: Colloid Thruster
  720. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  721. Your engine's nozzle type should be: Capillary Emitter-Electrode Cone
  722. Your Altitude of operation is: 80 km+ (Vacuum)
  723. Tank repressurisation would be impractical and unnecessary
  724. The Cooling Mechanism to be used would be Dump Cooling
  725.  
  726.  
  727. Your Engine is called: RS-43A "Lagrange"
  728. Your Engine Cycle is: Full Flow Staged
  729. Your Oxidizer is: AK20K: 80% HNO3 + 20% N2O4 (Nitric Acid)
  730. Your Fuel is: N2H4 (Hydrazine)
  731. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  732. Your Altitude of operation is: 30-80 km (High Atmosphere)
  733. Tank repressurisation would be done using Inert gas
  734. The Cooling Mechanism to be used would be Film Cooling
  735.  
  736.  
  737. Your Engine is called: R-551h "Philae"
  738. Your Engine Cycle is: Colloid Thruster
  739. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  740. Your engine's nozzle type should be: Capillary Emitter-Electrode Cone
  741. Your Altitude of operation is: 80 km+ (Vacuum)
  742. Tank repressurisation would be impractical and unnecessary
  743. The Cooling Mechanism to be used would be Film Cooling
  744.  
  745.  
  746. Your Engine is called: LRE-780H "Uran"
  747. Your Engine Cycle is: Gridded Ion Thruster
  748. Your Propellant is: Xenon
  749. Your engine's nozzle type should be: Electrostatic Ion Nozzle
  750. Your Altitude of operation is: 80 km+ (Vacuum)
  751. Tank repressurisation would be impractical and unnecessary
  752. The Cooling Mechanism to be used would be Dump Cooling
  753.  
  754.  
  755. Your Engine is called: LE-16 "Philae"
  756. Your Engine Cycle is: "Expander Closed" Liquid Core
  757. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Carbon Monoxide (CO) as a remass
  758. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  759. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  760. Your Altitude of operation is: 80 km+ (Vacuum)
  761. Tank repressurisation would be done using Inert gas
  762. The Cooling Mechanism to be used would be Film Cooling
  763.  
  764.  
  765. Your Engine is called: R-1007M "Panther"
  766. Your Engine Cycle is: Cold Gas Monopropellant
  767. Your Propellant is: Ammonia (NH3)
  768. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  769. Your Altitude of operation is: 80 km+ (Vacuum)
  770. Tank repressurisation would be impractical and unnecessary
  771. The Cooling Mechanism to be used would be unnecessary
  772.  
  773.  
  774. Your Engine is called: R-436K "Efir"
  775. Your Engine Cycle is: Monopropellant (Decomposition)
  776. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  777. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  778. Your Altitude of operation is: 80 km+ (Vacuum)
  779. Tank repressurisation would be impractical and unnecessary
  780. The Cooling Mechanism to be used would be Film Cooling
  781.  
  782.  
  783. Your Engine is called: AJ-457t "Insurgent"
  784. Your Engine Cycle is: "Vortex Confined" Liquid Core
  785. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Monoatomic Hydrogen (H) as a remass
  786. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  787. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  788. Your Altitude of operation is: 80 km+ (Vacuum)
  789. Tank repressurisation would be done Autogenously
  790. The Cooling Mechanism to be used would be Film Cooling
  791.  
  792.  
  793. Your Engine is called: KDTU-57S "Hyperion"
  794. Your Engine Cycle is: MagnetoPlasmaDynamic Thruster
  795. Your Propellant is: Lithium
  796. Your engine's nozzle type should be: Cathode Plug Magnetic Confinement Nozzle
  797. Your Altitude of operation is: 80 km+ (Vacuum)
  798. Tank repressurisation would be impractical and unnecessary
  799. The Cooling Mechanism to be used would be Radiative Cooling
  800.  
  801.  
  802. Your Engine is called: XLR-764m "Oscar"
  803. Your Engine Cycle is: Dual Expander (Open/Bleed)
  804. Your Oxidizer is: F2 (Fluorine)
  805. Your Fuel is: CH4 (Methane)
  806. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  807. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  808. Tank repressurisation would be done Autogenously
  809. The Cooling Mechanism to be used would be Dump Cooling
  810.  
  811.  
  812. Your Engine is called: DST-359F "Ross"
  813. Your Engine Cycle is: "Expander Open" Liquid Core
  814. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Nitrogen (N2) as a remass
  815. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  816. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  817. Your Altitude of operation is: 80 km+ (Vacuum)
  818. Tank repressurisation would be done Autogenously
  819. The Cooling Mechanism to be used would be Regenerative Cooling
  820.  
  821.  
  822. Your Engine is called: MV-902S "Clementine"
  823. Your Engine Cycle is: Nuclear SaltWater
  824. Your Propellant is: Uranium TetraBromide (UBr4) + Water (H2O)
  825. Your Reactor's Fission Fuel is: 25-8% Uranium-235
  826. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  827. Your Altitude of operation is: 80 km+ (Vacuum)
  828. Tank repressurisation would be done Autogenously
  829. The Cooling Mechanism to be used would be Transpiration Cooling
  830.  
  831.  
  832. Your Engine is called: KRD-448 "Svir"
  833. Your Engine Cycle is: Gas Generator
  834. Your Oxidizer is: N2O4 (Nitrogen Tetroxide)
  835. Your Fuel is: C2H5OH(Ethanol) 85%
  836. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  837. Your Altitude of operation is: 30-80 km (High Atmosphere)
  838. Tank repressurisation would be done using Inert gas
  839. The Cooling Mechanism to be used would be Radiative Cooling
  840.  
  841.  
  842. Your Engine is called: KDU-266P "Vega"
  843. Your Engine Cycle is: Expander (Closed)
  844. Your Oxidizer is: F2 (Fluorine)
  845. Your Fuel is: N2H4 (Hydrazine)
  846. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  847. Your Altitude of operation is: 0-10 km (Sea Level)
  848. Tank repressurisation would be done Autogenously
  849. The Cooling Mechanism to be used would be Dump Cooling
  850.  
  851.  
  852. Your Engine is called: XS-749W "Kristall"
  853. Your Engine Cycle is: Electric Pump Fed
  854. Your Oxidizer is: N2H4 (Hydrazine)
  855. Your Fuel is: B2H6 (Diborane)
  856. Your engine's nozzle type should be: Linear Aerospike Nozzle
  857. Your Altitude of operation is: Any Altitude (0-80 km+)
  858. Tank repressurisation would be done using Inert gas
  859. The Cooling Mechanism to be used would be Transpiration Cooling
  860.  
  861.  
  862. Your Engine is called: PKA-739n "Shrimp"
  863. Your Engine Cycle is: Gridded Ion Thruster
  864. Your Propellant is: Mercury
  865. Your engine's nozzle type should be: Electrostatic Ion Nozzle
  866. Your Altitude of operation is: 80 km+ (Vacuum)
  867. Tank repressurisation would be impractical and unnecessary
  868. The Cooling Mechanism to be used would be Film Cooling
  869.  
  870.  
  871. Your Engine is called: RS-706b "Orion"
  872. Your Engine Cycle is: Monopropellant (Decomposition)
  873. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  874. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  875. Your Altitude of operation is: 80 km+ (Vacuum)
  876. Tank repressurisation would be impractical and unnecessary
  877. The Cooling Mechanism to be used would be Dump Cooling
  878.  
  879.  
  880. Your Engine is called: R-521f "Reliant"
  881. Your Engine Cycle is: Gas Generator
  882. Your Oxidizer is: H2O2 (Hydrogen Peroxide) 95%
  883. Your Fuel is: C2H5OH(Ethanol) 75%
  884. Your engine's nozzle type should be: Toroidal Aerospike Nozzle
  885. Your Altitude of operation is: Any Altitude (0-80 km+)
  886. Tank repressurisation would be done using Inert gas
  887. The Cooling Mechanism to be used would be Film Cooling
  888.  
  889.  
  890. Your Engine is called: YF-840 "Spitzer"
  891. Your Engine Cycle is: Monopropellant (Decomposition)
  892. Your Propellant is: H2O2 (Hydrogen Peroxide)
  893. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  894. Your Altitude of operation is: 80 km+ (Vacuum)
  895. Tank repressurisation would be impractical and unnecessary
  896. The Cooling Mechanism to be used would be Film Cooling
  897.  
  898.  
  899. Your Engine is called: RS-373y "Luch"
  900. Your Engine Cycle is: "Expander Bleed" Pulsed Nuclear
  901. Your Propellant is: Oxygen (O2)
  902. Your Reactor's Fission Fuel is: 50% Uranium-235
  903. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  904. Your Altitude of operation is: 80 km+ (Vacuum)
  905. Tank repressurisation would be done Autogenously
  906. The Cooling Mechanism to be used would be Radiative Cooling
  907.  
  908.  
  909. Your Engine is called: RO-961U "Pulsar"
  910. Your Engine Cycle is: Gas Generator
  911. Your Oxidizer is: AK27I: 73% HNO3 + 27% N2O4 (Nitric Acid)
  912. Your Fuel is: C2H5OH(Ethanol) 85%
  913. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  914. Your Altitude of operation is: 30-80 km (High Atmosphere)
  915. Tank repressurisation would be done Autogenously
  916. The Cooling Mechanism to be used would be Dump Cooling
  917.  
  918.  
  919. Your Engine is called: RL-703N "Beta"
  920. Your Engine Cycle is: Staged Combustion (Oxidizer Rich)
  921. Your Oxidizer is: N2H4 (Hydrazine)
  922. Your Fuel is: C6H5NH2 (Aniline)
  923. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  924. Your Altitude of operation is: 0-10 km (Sea Level)
  925. Tank repressurisation would be done using Inert gas
  926. The Cooling Mechanism to be used would be Film Cooling
  927.  
  928.  
  929. Your Engine is called: NK-64 "Metis"
  930. Your Engine Cycle is: Combustion Tap Off
  931. Your Oxidizer is: O2 (Oxygen)
  932. Your Fuel is: N2H4 (Hydrazine)
  933. Your engine's nozzle type should be: Dual Bell Nozzle
  934. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  935. Tank repressurisation would be done Autogenously
  936. The Cooling Mechanism to be used would be Film Cooling
  937.  
  938.  
  939. Your Engine is called: LM10-875P "Cassini"
  940. Your Engine Cycle is: Expander (Closed)
  941. Your Oxidizer is: O2 (Oxygen)
  942. Your Fuel is: NH3 (Ammonia)
  943. Your engine's nozzle type should be: Dual Bell Nozzle
  944. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  945. Tank repressurisation would be done Autogenously
  946. The Cooling Mechanism to be used would be Dump Cooling
  947.  
  948.  
  949. Your Engine is called: PKA-389P "Kolibr"
  950. Your Engine Cycle is: MagnetoPlasmaDynamic Thruster
  951. Your Propellant is: Neon
  952. Your engine's nozzle type should be: Cathode Plug Magnetic Confinement Nozzle
  953. Your Altitude of operation is: 80 km+ (Vacuum)
  954. Tank repressurisation would be impractical and unnecessary
  955. The Cooling Mechanism to be used would be Regenerative Cooling
  956.  
  957.  
  958. Your Engine is called: PKA-45F "Prognoz"
  959. Your Engine Cycle is: "Expander Open" Gas Core
  960. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Oxygen (O2) as remass
  961. Your Reactor's Fission Fuel is: 100-90% Uranium-235
  962. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  963. Your Altitude of operation is: 80 km+ (Vacuum)
  964. Tank repressurisation would be done Autogenously
  965. The Cooling Mechanism to be used would be Radiative Cooling
  966.  
  967.  
  968. Your Engine is called: MV-480 "Asimov"
  969. Your Engine Cycle is: Monopropellant (Decomposition)
  970. Your Propellant is: H2O2 (Hydrogen Peroxide)
  971. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  972. Your Altitude of operation is: 80 km+ (Vacuum)
  973. Tank repressurisation would be impractical and unnecessary
  974. The Cooling Mechanism to be used would be Ablative Cooling
  975.  
  976.  
  977. Your Engine is called: RD-354T "Fortune"
  978. Your Engine Cycle is: "Expander Closed" Pebble-Bed Core
  979. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Nitrogen (N2) as a remass
  980. Your Reactor's Fission Fuel is: 50% Uranium-235
  981. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  982. Your Altitude of operation is: 80 km+ (Vacuum)
  983. Tank repressurisation would be done using Inert gas
  984. The Cooling Mechanism to be used would be Regenerative Cooling
  985.  
  986.  
  987. Your Engine is called: BE-1008 "Neman"
  988. Your Engine Cycle is: MagnetoPlasmaDynamic Thruster
  989. Your Propellant is: Lithium
  990. Your engine's nozzle type should be: Cathode Plug Magnetic Confinement Nozzle
  991. Your Altitude of operation is: 80 km+ (Vacuum)
  992. Tank repressurisation would be impractical and unnecessary
  993. The Cooling Mechanism to be used would be Film Cooling
  994.  
  995.  
  996. Your Engine is called: KDTU-756t "Crimson"
  997. Your Engine Cycle is: Colloid Thruster
  998. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  999. Your engine's nozzle type should be: Capillary Emitter-Electrode Cone
  1000. Your Altitude of operation is: 80 km+ (Vacuum)
  1001. Tank repressurisation would be impractical and unnecessary
  1002. The Cooling Mechanism to be used would be Radiative Cooling
  1003.  
  1004.  
  1005. Your Engine is called: BE-173K "Neman"
  1006. Your Engine Cycle is: Hall Effect Thruster
  1007. Your Propellant is: Argon
  1008. Your engine's nozzle type should be: Hall Effect Thruster Nozzle
  1009. Your Altitude of operation is: 80 km+ (Vacuum)
  1010. Tank repressurisation would be impractical and unnecessary
  1011. The Cooling Mechanism to be used would be Regenerative Cooling
  1012.  
  1013.  
  1014. Your Engine is called: XLR-677w "Rosetta"
  1015. Your Engine Cycle is: Full Flow Staged
  1016. Your Oxidizer is: AK27I: 73% HNO3 + 27% N2O4 (Nitric Acid)
  1017. Your Fuel is: C2H5OH(Ethanol) 85%
  1018. Your engine's nozzle type should be: Linear Aerospike Nozzle
  1019. Your Altitude of operation is: Any Altitude (0-80 km+)
  1020. Tank repressurisation would be done Autogenously
  1021. The Cooling Mechanism to be used would be Dump Cooling
  1022.  
  1023.  
  1024. Your Engine is called: LRE-297c "Icarus"
  1025. Your Engine Cycle is: Nuclear SaltWater
  1026. Your Propellant is: Uranium TetraBromide (UBr4) + Water (H2O)
  1027. Your Reactor's Fission Fuel is: 100-90% Uranium-235
  1028. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1029. Your Altitude of operation is: 80 km+ (Vacuum)
  1030. Tank repressurisation would be done Autogenously
  1031. The Cooling Mechanism to be used would be Film Cooling
  1032.  
  1033.  
  1034. Your Engine is called: KRD-172E "Portal"
  1035. Your Engine Cycle is: Pressure-Fed
  1036. Your Oxidizer is: ClF3 (Chlorine Trifluoride)
  1037. Your Fuel is: C2H5OH(Ethanol) 85%
  1038. Your engine's nozzle type should be: Linear Aerospike Nozzle
  1039. Your Altitude of operation is: Any Altitude (0-80 km+)
  1040. Tank repressurisation would be done Autogenously
  1041. The Cooling Mechanism to be used would be Transpiration Cooling
  1042.  
  1043.  
  1044. Your Engine is called: BE-381S "Insider"
  1045. Your Engine Cycle is: Gridded Ion Thruster
  1046. Your Propellant is: Xenon
  1047. Your engine's nozzle type should be: Electrostatic Ion Nozzle
  1048. Your Altitude of operation is: 80 km+ (Vacuum)
  1049. Tank repressurisation would be impractical and unnecessary
  1050. The Cooling Mechanism to be used would be Radiative Cooling
  1051.  
  1052.  
  1053. Your Engine is called: KDU-970Z "Dream"
  1054. Your Engine Cycle is: "Wheel Flow" Gas Core
  1055. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Water (H2O) as remass
  1056. Your Reactor's Fission Fuel is: 25-8% Uranium-235
  1057. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1058. Your Altitude of operation is: 80 km+ (Vacuum)
  1059. Tank repressurisation would be done Autogenously
  1060. The Cooling Mechanism to be used would be Dump Cooling
  1061.  
  1062.  
  1063. Your Engine is called: AR-937B "Tochka"
  1064. Your Engine Cycle is: "Vortex Confined" Pebble-Bed Core
  1065. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Methane (CH4) as a remass
  1066. Your Reactor's Fission Fuel is: 50% Uranium-235
  1067. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1068. Your Altitude of operation is: 80 km+ (Vacuum)
  1069. Tank repressurisation would be done Autogenously
  1070. The Cooling Mechanism to be used would be Dump Cooling
  1071.  
  1072.  
  1073. Your Engine is called: LRE-620E "Nematoda"
  1074. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  1075. Your Propellant is: Argon
  1076. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  1077. Your Altitude of operation is: 80 km+ (Vacuum)
  1078. Tank repressurisation would be impractical and unnecessary
  1079. The Cooling Mechanism to be used would be Regenerative Cooling
  1080.  
  1081.  
  1082. Your Engine is called: LRE-204t "Oberon"
  1083. Your Engine Cycle is: Combustion Tap Off
  1084. Your Oxidizer is: N2O4 (Nitrogen Tetroxide)
  1085. Your Fuel is: 75% CH6N2 + 25% N2H4 (UH-25)
  1086. Your engine's nozzle type should be: Expansion-Deflection Nozzle
  1087. Your Altitude of operation is: Any Altitude (0-80 km+)
  1088. Tank repressurisation would be done Autogenously
  1089. The Cooling Mechanism to be used would be Radiative Cooling
  1090.  
  1091.  
  1092. Your Engine is called: HM-543M "Quaoar"
  1093. Your Engine Cycle is: Full Flow Staged
  1094. Your Oxidizer is: AK20I: 80% HNO3 + 20% N2O4 (Nitric Acid)
  1095. Your Fuel is: C2H5OH(Ethanol) 85%
  1096. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  1097. Your Altitude of operation is: 0-10 km (Sea Level)
  1098. Tank repressurisation would be done Autogenously
  1099. The Cooling Mechanism to be used would be Dump Cooling
  1100.  
  1101.  
  1102. Your Engine is called: RS-982N "Bayern"
  1103. Your Engine Cycle is: Expander (Open/Bleed)
  1104. Your Oxidizer is: O2 (Oxygen)
  1105. Your Fuel is: C2H5OH(Ethanol) 85%
  1106. Your engine's nozzle type should be: Dual Bell Nozzle
  1107. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  1108. Tank repressurisation would be done Autogenously
  1109. The Cooling Mechanism to be used would be Transpiration Cooling
  1110.  
  1111.  
  1112. Your Engine is called: HM-685C "Joist"
  1113. Your Engine Cycle is: Staged Combustion (Fuel Rich)
  1114. Your Oxidizer is: F2 (Fluorine)
  1115. Your Fuel is: H2 (Hydrogen)
  1116. Your engine's nozzle type should be: Expansion-Deflection Nozzle
  1117. Your Altitude of operation is: Any Altitude (0-80 km+)
  1118. Tank repressurisation would be done using Inert gas
  1119. The Cooling Mechanism to be used would be Regenerative Cooling
  1120.  
  1121.  
  1122. Your Engine is called: KDU-938D "Kavkaz"
  1123. Your Engine Cycle is: Pressure-Fed
  1124. Your Oxidizer is: AK20I: 80% HNO3 + 20% N2O4 (Nitric Acid)
  1125. Your Fuel is: C2H5OH(Ethanol) 85%
  1126. Your engine's nozzle type should be: Dual Bell Nozzle
  1127. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  1128. Tank repressurisation would be done Autogenously
  1129. The Cooling Mechanism to be used would be Ablative Cooling
  1130.  
  1131.  
  1132. Your Engine is called: AJ-895I "Etalon"
  1133. Your Engine Cycle is: Nuclear SaltWater
  1134. Your Propellant is: Uranium TetraBromide (UBr4) + Water (H2O)
  1135. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  1136. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1137. Your Altitude of operation is: 80 km+ (Vacuum)
  1138. Tank repressurisation would be done Autogenously
  1139. The Cooling Mechanism to be used would be Transpiration Cooling
  1140.  
  1141.  
  1142. Your Engine is called: AJ-561G "Eagle"
  1143. Your Engine Cycle is: Gridded Ion Thruster
  1144. Your Propellant is: Caesium
  1145. Your engine's nozzle type should be: Electrostatic Ion Nozzle
  1146. Your Altitude of operation is: 80 km+ (Vacuum)
  1147. Tank repressurisation would be impractical and unnecessary
  1148. The Cooling Mechanism to be used would be Transpiration Cooling
  1149.  
  1150.  
  1151. Your Engine is called: HM-801S "Argosy"
  1152. Your Engine Cycle is: "Vortex Confined" Pebble-Bed Core
  1153. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Nitrogen (N2) as a remass
  1154. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  1155. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1156. Your Altitude of operation is: 80 km+ (Vacuum)
  1157. Tank repressurisation would be done using Inert gas
  1158. The Cooling Mechanism to be used would be Transpiration Cooling
  1159.  
  1160.  
  1161. Your Engine is called: MV-658F "Rubin"
  1162. Your Engine Cycle is: Expander (Closed)
  1163. Your Oxidizer is: O2 (Oxygen)
  1164. Your Fuel is: B2H6 (Diborane)
  1165. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1166. Your Altitude of operation is: 80 km+ (Vacuum)
  1167. Tank repressurisation would be done Autogenously
  1168. The Cooling Mechanism to be used would be Radiative Cooling
  1169.  
  1170.  
  1171. Your Engine is called: RS-947K "Pirs"
  1172. Your Engine Cycle is: "Expander Bleed" Gas Core
  1173. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Oxygen (O2) as remass
  1174. Your Reactor's Fission Fuel is: 50% Uranium-235
  1175. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1176. Your Altitude of operation is: 80 km+ (Vacuum)
  1177. Tank repressurisation would be done using Inert gas
  1178. The Cooling Mechanism to be used would be Radiative Cooling
  1179.  
  1180.  
  1181. Your Engine is called: DOK-832 "Asimov"
  1182. Your Engine Cycle is: Cold Gas Monopropellant
  1183. Your Propellant is: Carbon Dioxide (CO2)
  1184. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  1185. Your Altitude of operation is: 80 km+ (Vacuum)
  1186. Tank repressurisation would be impractical and unnecessary
  1187. The Cooling Mechanism to be used would be unnecessary
  1188.  
  1189.  
  1190. Your Engine is called: MJ-29M "Vyuga"
  1191. Your Engine Cycle is: Colloid Thruster
  1192. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  1193. Your engine's nozzle type should be: Capillary Emitter-Electrode Cone
  1194. Your Altitude of operation is: 80 km+ (Vacuum)
  1195. Tank repressurisation would be impractical and unnecessary
  1196. The Cooling Mechanism to be used would be Film Cooling
  1197.  
  1198.  
  1199. Your Engine is called: MJ-746g "Pirs"
  1200. Your Engine Cycle is: "Expander Bleed" Pebble-Bed Core
  1201. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Monoatomic Hydrogen (H) as a remass
  1202. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  1203. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1204. Your Altitude of operation is: 80 km+ (Vacuum)
  1205. Tank repressurisation would be done Autogenously
  1206. The Cooling Mechanism to be used would be Transpiration Cooling
  1207.  
  1208.  
  1209. Your Engine is called: AR-406K "Yastreb"
  1210. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  1211. Your Propellant is: Krypton
  1212. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  1213. Your Altitude of operation is: 80 km+ (Vacuum)
  1214. Tank repressurisation would be impractical and unnecessary
  1215. The Cooling Mechanism to be used would be Radiative Cooling
  1216.  
  1217.  
  1218. Your Engine is called: YF-918R "Kybau"
  1219. Your Engine Cycle is: Electric Pump Fed
  1220. Your Oxidizer is: O3 (Ozone)
  1221. Your Fuel is: H2 (Hydrogen)
  1222. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  1223. Your Altitude of operation is: 30-80 km (High Atmosphere)
  1224. Tank repressurisation would be done Autogenously
  1225. The Cooling Mechanism to be used would be Film Cooling
  1226.  
  1227.  
  1228. Your Engine is called: MV-71G "Twitch"
  1229. Your Engine Cycle is: "Expander Open" Solid Core
  1230. Your Propellant is: Hydrogen (H)
  1231. Your Reactor's Fission Fuel is: 25-8% Plutonium-238
  1232. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1233. Your Altitude of operation is: 80 km+ (Vacuum)
  1234. Tank repressurisation would be done using Inert gas
  1235. The Cooling Mechanism to be used would be Film Cooling
  1236.  
  1237.  
  1238. Your Engine is called: RO-182Z "Artyom"
  1239. Your Engine Cycle is: Full Flow Staged
  1240. Your Oxidizer is: AK20K: 80% HNO3 + 20% N2O4 (Nitric Acid)
  1241. Your Fuel is: N2H4 (Hydrazine)
  1242. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1243. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  1244. Tank repressurisation would be done Autogenously
  1245. The Cooling Mechanism to be used would be Dump Cooling
  1246.  
  1247.  
  1248. Your Engine is called: AJ-123D "Solaris"
  1249. Your Engine Cycle is: Hall Effect Thruster
  1250. Your Propellant is: Xenon
  1251. Your engine's nozzle type should be: Hall Effect Thruster Nozzle
  1252. Your Altitude of operation is: 80 km+ (Vacuum)
  1253. Tank repressurisation would be impractical and unnecessary
  1254. The Cooling Mechanism to be used would be Dump Cooling
  1255.  
  1256.  
  1257. Your Engine is called: R-195n "Potok"
  1258. Your Engine Cycle is: Dual Expander (Closed)
  1259. Your Oxidizer is: F2 (Fluorine)
  1260. Your Fuel is: H2 (Hydrogen)
  1261. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1262. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  1263. Tank repressurisation would be done Autogenously
  1264. The Cooling Mechanism to be used would be Radiative Cooling
  1265.  
  1266.  
  1267. Your Engine is called: LRE-453V "Orion"
  1268. Your Engine Cycle is: Staged Combustion (Oxidizer Rich)
  1269. Your Oxidizer is: N2O4 (Nitrogen Tetroxide)
  1270. Your Fuel is: C6H5NH2 (Aniline)
  1271. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1272. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  1273. Tank repressurisation would be done using Inert gas
  1274. The Cooling Mechanism to be used would be Transpiration Cooling
  1275.  
  1276.  
  1277. Your Engine is called: LE-500Y "Roton"
  1278. Your Engine Cycle is: Staged Combustion (Oxidizer Rich)
  1279. Your Oxidizer is: N2H4 (Hydrazine)
  1280. Your Fuel is: C2H8N2 (UnsymetricalDimethylHydrazine)
  1281. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  1282. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  1283. Tank repressurisation would be done using Inert gas
  1284. The Cooling Mechanism to be used would be Transpiration Cooling
  1285.  
  1286.  
  1287. Your Engine is called: DST-317U "Glonass"
  1288. Your Engine Cycle is: Monopropellant (Decomposition)
  1289. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  1290. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  1291. Your Altitude of operation is: 80 km+ (Vacuum)
  1292. Tank repressurisation would be impractical and unnecessary
  1293. The Cooling Mechanism to be used would be Dump Cooling
  1294.  
  1295.  
  1296. Your Engine is called: XS-840 "Tenacity"
  1297. Your Engine Cycle is: "Vortex Confined" Gas Core
  1298. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Carbon Dioxide (CO2) as remass
  1299. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  1300. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1301. Your Altitude of operation is: 80 km+ (Vacuum)
  1302. Tank repressurisation would be done Autogenously
  1303. The Cooling Mechanism to be used would be Transpiration Cooling
  1304.  
  1305.  
  1306. Your Engine is called: PKA-35N "Romb"
  1307. Your Engine Cycle is: Dual Expander (Open/Bleed)
  1308. Your Oxidizer is: F2 (Fluorine)
  1309. Your Fuel is: CH4 (Methane)
  1310. Your engine's nozzle type should be: Dual Bell Nozzle
  1311. Your Altitude of operation is: 30-80 km (High Atmosphere)
  1312. Tank repressurisation would be done Autogenously
  1313. The Cooling Mechanism to be used would be Radiative Cooling
  1314.  
  1315.  
  1316. Your Engine is called: BE-166F "Jubilance"
  1317. Your Engine Cycle is: Dual Expander (Closed)
  1318. Your Oxidizer is: O2 (Oxygen)
  1319. Your Fuel is: H2 (Hydrogen)
  1320. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1321. Your Altitude of operation is: 30-80 km (High Atmosphere)
  1322. Tank repressurisation would be done Autogenously
  1323. The Cooling Mechanism to be used would be Dump Cooling
  1324.  
  1325.  
  1326. Your Engine is called: R-204t "FireFly"
  1327. Your Engine Cycle is: Full Flow Staged
  1328. Your Oxidizer is: N2O4 (Nitrogen Tetroxide)
  1329. Your Fuel is: C2H5OH(Ethanol) 75%
  1330. Your engine's nozzle type should be: Dual Bell Nozzle
  1331. Your Altitude of operation is: 30-80 km (High Atmosphere)
  1332. Tank repressurisation would be done Autogenously
  1333. The Cooling Mechanism to be used would be Transpiration Cooling
  1334.  
  1335.  
  1336. Your Engine is called: KRD-687D "Tsyklon"
  1337. Your Engine Cycle is: "Expander Bleed" Pebble-Bed Core
  1338. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Nitrogen (N2) as a remass
  1339. Your Reactor's Fission Fuel is: 100-90% Uranium-235
  1340. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1341. Your Altitude of operation is: 80 km+ (Vacuum)
  1342. Tank repressurisation would be done using Inert gas
  1343. The Cooling Mechanism to be used would be Dump Cooling
  1344.  
  1345.  
  1346. Your Engine is called: HM-445J "Asimov"
  1347. Your Engine Cycle is: "Magnetohydrodynamic(MHD) vortex" Gas Core
  1348. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Nitrogen (N2) as remass
  1349. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  1350. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1351. Your Altitude of operation is: 80 km+ (Vacuum)
  1352. Tank repressurisation would be done using Inert gas
  1353. The Cooling Mechanism to be used would be Film Cooling
  1354.  
  1355.  
  1356. Your Engine is called: RD-915t "Kosmos"
  1357. Your Engine Cycle is: Combustion Tap Off
  1358. Your Oxidizer is: N2O4 (Nitrogen Tetroxide)
  1359. Your Fuel is: B2H6 (Diborane)
  1360. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  1361. Your Altitude of operation is: 80 km+ (Vacuum)
  1362. Tank repressurisation would be done using Inert gas
  1363. The Cooling Mechanism to be used would be Dump Cooling
  1364.  
  1365.  
  1366. Your Engine is called: RL-844X "Aelita"
  1367. Your Engine Cycle is: "Expander Closed" Pulsed Nuclear
  1368. Your Propellant is: Ammonia (NH3)
  1369. Your Reactor's Fission Fuel is: 20-8% Uranium-235
  1370. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1371. Your Altitude of operation is: 80 km+ (Vacuum)
  1372. Tank repressurisation would be done using Inert gas
  1373. The Cooling Mechanism to be used would be Regenerative Cooling
  1374.  
  1375.  
  1376. Your Engine is called: KDU-898R "Parlos"
  1377. Your Engine Cycle is: "Expander Open" Pulsed Nuclear
  1378. Your Propellant is: Oxygen (O2)
  1379. Your Reactor's Fission Fuel is: 1-2% Plutonium-238
  1380. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1381. Your Altitude of operation is: 80 km+ (Vacuum)
  1382. Tank repressurisation would be done Autogenously
  1383. The Cooling Mechanism to be used would be Film Cooling
  1384.  
  1385.  
  1386. Your Engine is called: DST-113J "Sojourner"
  1387. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  1388. Your Propellant is: Argon
  1389. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  1390. Your Altitude of operation is: 80 km+ (Vacuum)
  1391. Tank repressurisation would be impractical and unnecessary
  1392. The Cooling Mechanism to be used would be Transpiration Cooling
  1393.  
  1394.  
  1395. Your Engine is called: LE-186W "Contour"
  1396. Your Engine Cycle is: Dual Expander (Closed)
  1397. Your Oxidizer is: F2 (Fluorine)
  1398. Your Fuel is: CH4 (Methane)
  1399. Your engine's nozzle type should be: Linear Aerospike Nozzle
  1400. Your Altitude of operation is: Any Altitude (0-80 km+)
  1401. Tank repressurisation would be done Autogenously
  1402. The Cooling Mechanism to be used would be Dump Cooling
  1403.  
  1404.  
  1405. Your Engine is called: DOK-962P "Gorizont"
  1406. Your Engine Cycle is: Pressure-Fed
  1407. Your Oxidizer is: AK27I: 73% HNO3 + 27% N2O4 (Nitric Acid)
  1408. Your Fuel is: N2H4 (Hydrazine)
  1409. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1410. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  1411. Tank repressurisation would be done using Inert gas
  1412. The Cooling Mechanism to be used would be Transpiration Cooling
  1413.  
  1414.  
  1415. Your Engine is called: AR-636T "Prospector"
  1416. Your Engine Cycle is: Staged Combustion (Oxidizer Rich)
  1417. Your Oxidizer is: O2 (Oxygen)
  1418. Your Fuel is: NH3 (Ammonia)
  1419. Your engine's nozzle type should be: Dual Bell Nozzle
  1420. Your Altitude of operation is: 30-80 km (High Atmosphere)
  1421. Tank repressurisation would be done Autogenously
  1422. The Cooling Mechanism to be used would be Dump Cooling
  1423.  
  1424.  
  1425. Your Engine is called: NK-896 "Nematoda"
  1426. Your Engine Cycle is: Gridded Ion Thruster
  1427. Your Propellant is: Mercury
  1428. Your engine's nozzle type should be: Electrostatic Ion Nozzle
  1429. Your Altitude of operation is: 80 km+ (Vacuum)
  1430. Tank repressurisation would be impractical and unnecessary
  1431. The Cooling Mechanism to be used would be Film Cooling
  1432.  
  1433.  
  1434. Your Engine is called: RS-160 "Oplot"
  1435. Your Engine Cycle is: Hall Effect Thruster
  1436. Your Propellant is: Magnesium
  1437. Your engine's nozzle type should be: Hall Effect Thruster Nozzle
  1438. Your Altitude of operation is: 80 km+ (Vacuum)
  1439. Tank repressurisation would be impractical and unnecessary
  1440. The Cooling Mechanism to be used would be Dump Cooling
  1441.  
  1442.  
  1443. Your Engine is called: LM10-325x "Shturn"
  1444. Your Engine Cycle is: Nuclear SaltWater
  1445. Your Propellant is: Uranium TetraBromide (UBr4) + Water (H2O)
  1446. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  1447. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1448. Your Altitude of operation is: 80 km+ (Vacuum)
  1449. Tank repressurisation would be done Autogenously
  1450. The Cooling Mechanism to be used would be Film Cooling
  1451.  
  1452.  
  1453. Your Engine is called: KRD-648 "Douglas"
  1454. Your Engine Cycle is: Cold Gas Monopropellant
  1455. Your Propellant is: Methane (CH4)
  1456. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  1457. Your Altitude of operation is: 80 km+ (Vacuum)
  1458. Tank repressurisation would be impractical and unnecessary
  1459. The Cooling Mechanism to be used would be unnecessary
  1460.  
  1461.  
  1462. Your Engine is called: AR-334s "Tellus"
  1463. Your Engine Cycle is: Gas Generator
  1464. Your Oxidizer is: ClF3 (Chlorine Trifluoride)
  1465. Your Fuel is: N2H4 (Hydrazine)
  1466. Your engine's nozzle type should be: Linear Aerospike Nozzle
  1467. Your Altitude of operation is: Any Altitude (0-80 km+)
  1468. Tank repressurisation would be done Autogenously
  1469. The Cooling Mechanism to be used would be Regenerative Cooling
  1470.  
  1471.  
  1472. Your Engine is called: KDU-38P "Odin"
  1473. Your Engine Cycle is: Full Flow Staged
  1474. Your Oxidizer is: F2 (Fluorine)
  1475. Your Fuel is: N2H4 (Hydrazine)
  1476. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  1477. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  1478. Tank repressurisation would be done using Inert gas
  1479. The Cooling Mechanism to be used would be Transpiration Cooling
  1480.  
  1481.  
  1482. Your Engine is called: CE-390U "Ithacus"
  1483. Your Engine Cycle is: Colloid Thruster
  1484. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  1485. Your engine's nozzle type should be: Capillary Emitter-Electrode Cone
  1486. Your Altitude of operation is: 80 km+ (Vacuum)
  1487. Tank repressurisation would be impractical and unnecessary
  1488. The Cooling Mechanism to be used would be Dump Cooling
  1489.  
  1490.  
  1491. Your Engine is called: DOK-913Y "Oplot"
  1492. Your Engine Cycle is: "Expander Closed" Solid Core
  1493. Your Propellant is: Nitrogen (N2)
  1494. Your Reactor's Fission Fuel is: 50% Uranium-235
  1495. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1496. Your Altitude of operation is: 80 km+ (Vacuum)
  1497. Tank repressurisation would be done using Inert gas
  1498. The Cooling Mechanism to be used would be Film Cooling
  1499.  
  1500.  
  1501. Your Engine is called: KDTU-328 "Pulsar"
  1502. Your Engine Cycle is: Expander (Open/Bleed)
  1503. Your Oxidizer is: O3 (Ozone)
  1504. Your Fuel is: CH3OH (Methanol)
  1505. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1506. Your Altitude of operation is: 30-80 km (High Atmosphere)
  1507. Tank repressurisation would be done Autogenously
  1508. The Cooling Mechanism to be used would be Dump Cooling
  1509.  
  1510.  
  1511. Your Engine is called: CE-413W "Nauka"
  1512. Your Engine Cycle is: Expander (Closed)
  1513. Your Oxidizer is: F2 (Fluorine)
  1514. Your Fuel is: C2H5OH(Ethanol) 85%
  1515. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1516. Your Altitude of operation is: 80 km+ (Vacuum)
  1517. Tank repressurisation would be done Autogenously
  1518. The Cooling Mechanism to be used would be Film Cooling
  1519.  
  1520.  
  1521. Your Engine is called: RL-547H "Astra"
  1522. Your Engine Cycle is: Dual Expander (Open/Bleed)
  1523. Your Oxidizer is: O2 (Oxygen)
  1524. Your Fuel is: H2 (Hydrogen)
  1525. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  1526. Your Altitude of operation is: 80 km+ (Vacuum)
  1527. Tank repressurisation would be done Autogenously
  1528. The Cooling Mechanism to be used would be Film Cooling
  1529.  
  1530.  
  1531. Your Engine is called: DST-901M "Agena"
  1532. Your Engine Cycle is: Staged Combustion (Fuel Rich)
  1533. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  1534. Your Fuel is: H2 (Hydrogen)
  1535. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  1536. Your Altitude of operation is: 0-10 km (Sea Level)
  1537. Tank repressurisation would be done using Inert gas
  1538. The Cooling Mechanism to be used would be Film Cooling
  1539.  
  1540.  
  1541. Your Engine is called: BE-48 "Mudrost"
  1542. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  1543. Your Propellant is: Krypton
  1544. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  1545. Your Altitude of operation is: 80 km+ (Vacuum)
  1546. Tank repressurisation would be impractical and unnecessary
  1547. The Cooling Mechanism to be used would be Regenerative Cooling
  1548.  
  1549.  
  1550. Your Engine is called: LE-849Z "Atlanta"
  1551. Your Engine Cycle is: Gas Generator
  1552. Your Oxidizer is: F2 (Fluorine)
  1553. Your Fuel is: CH3OH (Methanol)
  1554. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  1555. Your Altitude of operation is: 0-10 km (Sea Level)
  1556. Tank repressurisation would be done using Inert gas
  1557. The Cooling Mechanism to be used would be Radiative Cooling
  1558.  
  1559.  
  1560. Your Engine is called: LRE-170v "Teplokhod"
  1561. Your Engine Cycle is: Staged Combustion (Oxidizer Rich)
  1562. Your Oxidizer is: O2 (Oxygen)
  1563. Your Fuel is: C2H5OH(Ethanol) 75%
  1564. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  1565. Your Altitude of operation is: 0-10 km (Sea Level)
  1566. Tank repressurisation would be done Autogenously
  1567. The Cooling Mechanism to be used would be Regenerative Cooling
  1568.  
  1569.  
  1570. Your Engine is called: DST-523p "Cartago"
  1571. Your Engine Cycle is: Cold Gas Monopropellant
  1572. Your Propellant is: Ammonia (NH3)
  1573. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  1574. Your Altitude of operation is: 80 km+ (Vacuum)
  1575. Tank repressurisation would be impractical and unnecessary
  1576. The Cooling Mechanism to be used would be unnecessary
  1577.  
  1578.  
  1579. Your Engine is called: LRE-81D "Sturt"
  1580. Your Engine Cycle is: Dual Expander (Open/Bleed)
  1581. Your Oxidizer is: F2 (Fluorine)
  1582. Your Fuel is: H2 (Hydrogen)
  1583. Your engine's nozzle type should be: Toroidal Aerospike Nozzle
  1584. Your Altitude of operation is: Any Altitude (0-80 km+)
  1585. Tank repressurisation would be done Autogenously
  1586. The Cooling Mechanism to be used would be Film Cooling
  1587.  
  1588.  
  1589. Your Engine is called: YF-444R "Kanopus"
  1590. Your Engine Cycle is: Dual Expander (Open/Bleed)
  1591. Your Oxidizer is: O2 (Oxygen)
  1592. Your Fuel is: H2 (Hydrogen)
  1593. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  1594. Your Altitude of operation is: 0-10 km (Sea Level)
  1595. Tank repressurisation would be done Autogenously
  1596. The Cooling Mechanism to be used would be Transpiration Cooling
  1597.  
  1598.  
  1599. Your Engine is called: RL-80 "Zircon"
  1600. Your Engine Cycle is: Hall Effect Thruster
  1601. Your Propellant is: Bismuth
  1602. Your engine's nozzle type should be: Hall Effect Thruster Nozzle
  1603. Your Altitude of operation is: 80 km+ (Vacuum)
  1604. Tank repressurisation would be impractical and unnecessary
  1605. The Cooling Mechanism to be used would be Radiative Cooling
  1606.  
  1607.  
  1608. Your Engine is called: RL-100U "Coeus"
  1609. Your Engine Cycle is: "Expander Bleed" Solid Core
  1610. Your Propellant is: Oxygen (O2)
  1611. Your Reactor's Fission Fuel is: 1-2% Plutonium-238
  1612. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1613. Your Altitude of operation is: 80 km+ (Vacuum)
  1614. Tank repressurisation would be done using Inert gas
  1615. The Cooling Mechanism to be used would be Radiative Cooling
  1616.  
  1617.  
  1618. Your Engine is called: MV-597A "Tellus"
  1619. Your Engine Cycle is: "Expander Open" Solid Core
  1620. Your Propellant is: Oxygen (O2)
  1621. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  1622. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1623. Your Altitude of operation is: 80 km+ (Vacuum)
  1624. Tank repressurisation would be done Autogenously
  1625. The Cooling Mechanism to be used would be Dump Cooling
  1626.  
  1627.  
  1628. Your Engine is called: DST-885z "Inertsiya"
  1629. Your Engine Cycle is: Dual Expander (Open/Bleed)
  1630. Your Oxidizer is: O2 (Oxygen)
  1631. Your Fuel is: CH4 (Methane)
  1632. Your engine's nozzle type should be: Linear Aerospike Nozzle
  1633. Your Altitude of operation is: Any Altitude (0-80 km+)
  1634. Tank repressurisation would be done Autogenously
  1635. The Cooling Mechanism to be used would be Transpiration Cooling
  1636.  
  1637.  
  1638. Your Engine is called: RS-764n "Varagian"
  1639. Your Engine Cycle is: Monopropellant (Decomposition)
  1640. Your Propellant is: N2H4 (Hydrazine)
  1641. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  1642. Your Altitude of operation is: 80 km+ (Vacuum)
  1643. Tank repressurisation would be impractical and unnecessary
  1644. The Cooling Mechanism to be used would be Radiative Cooling
  1645.  
  1646.  
  1647. Your Engine is called: KDU-587F "Galileo"
  1648. Your Engine Cycle is: Pressure-Fed
  1649. Your Oxidizer is: AK20K: 80% HNO3 + 20% N2O4 (Nitric Acid)
  1650. Your Fuel is: N2H4 (Hydrazine)
  1651. Your engine's nozzle type should be: Toroidal Aerospike Nozzle
  1652. Your Altitude of operation is: Any Altitude (0-80 km+)
  1653. Tank repressurisation would be done using Inert gas
  1654. The Cooling Mechanism to be used would be Film Cooling
  1655.  
  1656.  
  1657. Your Engine is called: AJ-34v "Pluton"
  1658. Your Engine Cycle is: Staged Combustion (Oxidizer Rich)
  1659. Your Oxidizer is: N2H4 (Hydrazine)
  1660. Your Fuel is: 50% CH6N2 + 50% N2H4 (Aerosine-50)
  1661. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  1662. Your Altitude of operation is: 0-10 km (Sea Level)
  1663. Tank repressurisation would be done Autogenously
  1664. The Cooling Mechanism to be used would be Film Cooling
  1665.  
  1666.  
  1667. Your Engine is called: MV-952 "Kronos"
  1668. Your Engine Cycle is: Expander (Closed)
  1669. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  1670. Your Fuel is: H2 (Hydrogen)
  1671. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  1672. Your Altitude of operation is: 30-80 km (High Atmosphere)
  1673. Tank repressurisation would be done Autogenously
  1674. The Cooling Mechanism to be used would be Dump Cooling
  1675.  
  1676.  
  1677. Your Engine is called: HM-648 "Foton"
  1678. Your Engine Cycle is: Expander (Open/Bleed)
  1679. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  1680. Your Fuel is: B5H9 (Pentaborane)
  1681. Your engine's nozzle type should be: Toroidal Aerospike Nozzle
  1682. Your Altitude of operation is: Any Altitude (0-80 km+)
  1683. Tank repressurisation would be done Autogenously
  1684. The Cooling Mechanism to be used would be Transpiration Cooling
  1685.  
  1686.  
  1687. Your Engine is called: NK-465Z "Oka"
  1688. Your Engine Cycle is: "Vortex Confined" Liquid Core
  1689. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Oxygen (O2) as a remass
  1690. Your Reactor's Fission Fuel is: 50% Uranium-235
  1691. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1692. Your Altitude of operation is: 80 km+ (Vacuum)
  1693. Tank repressurisation would be done Autogenously
  1694. The Cooling Mechanism to be used would be Regenerative Cooling
  1695.  
  1696.  
  1697. Your Engine is called: XS-747d "Omega"
  1698. Your Engine Cycle is: Gridded Ion Thruster
  1699. Your Propellant is: Caesium
  1700. Your engine's nozzle type should be: Electrostatic Ion Nozzle
  1701. Your Altitude of operation is: 80 km+ (Vacuum)
  1702. Tank repressurisation would be impractical and unnecessary
  1703. The Cooling Mechanism to be used would be Radiative Cooling
  1704.  
  1705.  
  1706. Your Engine is called: BE-563H "Buran"
  1707. Your Engine Cycle is: Gas Generator
  1708. Your Oxidizer is: O3 (Ozone)
  1709. Your Fuel is: B5H9 (Pentaborane)
  1710. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1711. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  1712. Tank repressurisation would be done using Inert gas
  1713. The Cooling Mechanism to be used would be Regenerative Cooling
  1714.  
  1715.  
  1716. Your Engine is called: XLR-622A "Anelida"
  1717. Your Engine Cycle is: Pressure-Fed
  1718. Your Oxidizer is: O3 (Ozone)
  1719. Your Fuel is: B5H9 (Pentaborane)
  1720. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  1721. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  1722. Tank repressurisation would be done using Inert gas
  1723. The Cooling Mechanism to be used would be Transpiration Cooling
  1724.  
  1725.  
  1726. Your Engine is called: PKA-468V "Kazbek"
  1727. Your Engine Cycle is: "Expander Closed" Pulsed Nuclear
  1728. Your Propellant is: Oxygen (O2)
  1729. Your Reactor's Fission Fuel is: 50% Uranium-235
  1730. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1731. Your Altitude of operation is: 80 km+ (Vacuum)
  1732. Tank repressurisation would be done Autogenously
  1733. The Cooling Mechanism to be used would be Regenerative Cooling
  1734.  
  1735.  
  1736. Your Engine is called: HM-336 "Delta"
  1737. Your Engine Cycle is: Nuclear SaltWater
  1738. Your Propellant is: Uranium TetraBromide (UBr4) + Water (H2O)
  1739. Your Reactor's Fission Fuel is: 50% Uranium-235
  1740. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1741. Your Altitude of operation is: 80 km+ (Vacuum)
  1742. Tank repressurisation would be done using Inert gas
  1743. The Cooling Mechanism to be used would be Film Cooling
  1744.  
  1745.  
  1746. Your Engine is called: KDTU-558U "Strela"
  1747. Your Engine Cycle is: Pressure-Fed
  1748. Your Oxidizer is: H2O2 (Hydrogen Peroxide) 95%
  1749. Your Fuel is: C2H5OH(Ethanol) 75%
  1750. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1751. Your Altitude of operation is: 80 km+ (Vacuum)
  1752. Tank repressurisation would be done using Inert gas
  1753. The Cooling Mechanism to be used would be Regenerative Cooling
  1754.  
  1755.  
  1756. Your Engine is called: MJ-563a "Cerasus"
  1757. Your Engine Cycle is: Gas Generator
  1758. Your Oxidizer is: O2 (Oxygen)
  1759. Your Fuel is: CH3OH (Methanol)
  1760. Your engine's nozzle type should be: Dual Bell Nozzle
  1761. Your Altitude of operation is: 30-80 km (High Atmosphere)
  1762. Tank repressurisation would be done Autogenously
  1763. The Cooling Mechanism to be used would be Transpiration Cooling
  1764.  
  1765.  
  1766. Your Engine is called: XLR-671D "Kratos"
  1767. Your Engine Cycle is: "Magnetohydrodynamic(MHD) vortex" Gas Core
  1768. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Oxygen (O2) as remass
  1769. Your Reactor's Fission Fuel is: 100-90% Uranium-235
  1770. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1771. Your Altitude of operation is: 80 km+ (Vacuum)
  1772. Tank repressurisation would be done using Inert gas
  1773. The Cooling Mechanism to be used would be Dump Cooling
  1774.  
  1775.  
  1776. Your Engine is called: DST-210L "Dizhou"
  1777. Your Engine Cycle is: Monopropellant (Decomposition)
  1778. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  1779. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  1780. Your Altitude of operation is: 80 km+ (Vacuum)
  1781. Tank repressurisation would be impractical and unnecessary
  1782. The Cooling Mechanism to be used would be Film Cooling
  1783.  
  1784.  
  1785. Your Engine is called: RO-419G "Gamma"
  1786. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  1787. Your Propellant is: Krypton
  1788. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  1789. Your Altitude of operation is: 80 km+ (Vacuum)
  1790. Tank repressurisation would be impractical and unnecessary
  1791. The Cooling Mechanism to be used would be Transpiration Cooling
  1792.  
  1793.  
  1794. Your Engine is called: HM-956d "Cyclero"
  1795. Your Engine Cycle is: "Expander Open" Pebble-Bed Core
  1796. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Water (H2O) as a remass
  1797. Your Reactor's Fission Fuel is: 25-8% Uranium-235
  1798. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1799. Your Altitude of operation is: 80 km+ (Vacuum)
  1800. Tank repressurisation would be done using Inert gas
  1801. The Cooling Mechanism to be used would be Radiative Cooling
  1802.  
  1803.  
  1804. Your Engine is called: NK-468l "Hornet"
  1805. Your Engine Cycle is: Dual Expander (Closed)
  1806. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  1807. Your Fuel is: H2 (Hydrogen)
  1808. Your engine's nozzle type should be: Dual Bell Nozzle
  1809. Your Altitude of operation is: 30-80 km (High Atmosphere)
  1810. Tank repressurisation would be done Autogenously
  1811. The Cooling Mechanism to be used would be Film Cooling
  1812.  
  1813.  
  1814. Your Engine is called: KDTU-82E "Terrier"
  1815. Your Engine Cycle is: Dual Expander (Closed)
  1816. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  1817. Your Fuel is: H2 (Hydrogen)
  1818. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  1819. Your Altitude of operation is: 80 km+ (Vacuum)
  1820. Tank repressurisation would be done Autogenously
  1821. The Cooling Mechanism to be used would be Transpiration Cooling
  1822.  
  1823.  
  1824. Your Engine is called: BE-682C "Discoverer"
  1825. Your Engine Cycle is: "Expander Bleed" Liquid Core
  1826. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Hydrogen (H2) + Hexane (C6H14) as a remass
  1827. Your Reactor's Fission Fuel is: 25-8% Uranium-235
  1828. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1829. Your Altitude of operation is: 80 km+ (Vacuum)
  1830. Tank repressurisation would be done using Inert gas
  1831. The Cooling Mechanism to be used would be Transpiration Cooling
  1832.  
  1833.  
  1834. Your Engine is called: NK-443X "Python"
  1835. Your Engine Cycle is: Hall Effect Thruster
  1836. Your Propellant is: Iodine
  1837. Your engine's nozzle type should be: Hall Effect Thruster Nozzle
  1838. Your Altitude of operation is: 80 km+ (Vacuum)
  1839. Tank repressurisation would be impractical and unnecessary
  1840. The Cooling Mechanism to be used would be Film Cooling
  1841.  
  1842.  
  1843. Your Engine is called: KDU-213y "Gaia"
  1844. Your Engine Cycle is: Cold Gas Monopropellant
  1845. Your Propellant is: Ammonia (NH3)
  1846. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  1847. Your Altitude of operation is: 80 km+ (Vacuum)
  1848. Tank repressurisation would be impractical and unnecessary
  1849. The Cooling Mechanism to be used would be unnecessary
  1850.  
  1851.  
  1852. Your Engine is called: NK-995E "Dornier"
  1853. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  1854. Your Propellant is: Krypton
  1855. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  1856. Your Altitude of operation is: 80 km+ (Vacuum)
  1857. Tank repressurisation would be impractical and unnecessary
  1858. The Cooling Mechanism to be used would be Dump Cooling
  1859.  
  1860.  
  1861. Your Engine is called: RO-796W "Pegasus"
  1862. Your Engine Cycle is: Colloid Thruster
  1863. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  1864. Your engine's nozzle type should be: Capillary Emitter-Electrode Cone
  1865. Your Altitude of operation is: 80 km+ (Vacuum)
  1866. Tank repressurisation would be impractical and unnecessary
  1867. The Cooling Mechanism to be used would be Transpiration Cooling
  1868.  
  1869.  
  1870. Your Engine is called: RS-19k "Altaris"
  1871. Your Engine Cycle is: Expander (Closed)
  1872. Your Oxidizer is: O2 (Oxygen)
  1873. Your Fuel is: CH6N2 (MonomethylHydrazine)
  1874. Your engine's nozzle type should be: Linear Aerospike Nozzle
  1875. Your Altitude of operation is: Any Altitude (0-80 km+)
  1876. Tank repressurisation would be done Autogenously
  1877. The Cooling Mechanism to be used would be Ablative Cooling
  1878.  
  1879.  
  1880. Your Engine is called: MV-408 "Unity"
  1881. Your Engine Cycle is: Dual Expander (Open/Bleed)
  1882. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  1883. Your Fuel is: H2 (Hydrogen)
  1884. Your engine's nozzle type should be: Dual Bell Nozzle
  1885. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  1886. Tank repressurisation would be done Autogenously
  1887. The Cooling Mechanism to be used would be Regenerative Cooling
  1888.  
  1889.  
  1890. Your Engine is called: BE-632 "Voyager"
  1891. Your Engine Cycle is: MagnetoPlasmaDynamic Thruster
  1892. Your Propellant is: Xenon
  1893. Your engine's nozzle type should be: Cathode Plug Magnetic Confinement Nozzle
  1894. Your Altitude of operation is: 80 km+ (Vacuum)
  1895. Tank repressurisation would be impractical and unnecessary
  1896. The Cooling Mechanism to be used would be Regenerative Cooling
  1897.  
  1898.  
  1899. Your Engine is called: PKA-844V "Nauka"
  1900. Your Engine Cycle is: Expander (Closed)
  1901. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  1902. Your Fuel is: B2H6 (Diborane)
  1903. Your engine's nozzle type should be: Toroidal Aerospike Nozzle
  1904. Your Altitude of operation is: Any Altitude (0-80 km+)
  1905. Tank repressurisation would be done Autogenously
  1906. The Cooling Mechanism to be used would be Film Cooling
  1907.  
  1908.  
  1909. Your Engine is called: AR-931L "Themis"
  1910. Your Engine Cycle is: Monopropellant (Decomposition)
  1911. Your Propellant is: H2O2 (Hydrogen Peroxide)
  1912. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  1913. Your Altitude of operation is: 80 km+ (Vacuum)
  1914. Tank repressurisation would be impractical and unnecessary
  1915. The Cooling Mechanism to be used would be Film Cooling
  1916.  
  1917.  
  1918. Your Engine is called: YF-622R "Oberon"
  1919. Your Engine Cycle is: Electric Pump Fed
  1920. Your Oxidizer is: ClF5 (Chlorine Pentafluoride)
  1921. Your Fuel is: CH3OH (Methanol)
  1922. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  1923. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  1924. Tank repressurisation would be done using Inert gas
  1925. The Cooling Mechanism to be used would be Ablative Cooling
  1926.  
  1927.  
  1928. Your Engine is called: LRE-470l "Ascension"
  1929. Your Engine Cycle is: Cold Gas Monopropellant
  1930. Your Propellant is: Carbon Dioxide (CO2)
  1931. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  1932. Your Altitude of operation is: 80 km+ (Vacuum)
  1933. Tank repressurisation would be impractical and unnecessary
  1934. The Cooling Mechanism to be used would be unnecessary
  1935.  
  1936.  
  1937. Your Engine is called: KDU-769P "Prospero"
  1938. Your Engine Cycle is: Staged Combustion (Oxidizer Rich)
  1939. Your Oxidizer is: N2O4 (Nitrogen Tetroxide)
  1940. Your Fuel is: C2H8N2 (UnsymetricalDimethylHydrazine)
  1941. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  1942. Your Altitude of operation is: 0-10 km (Sea Level)
  1943. Tank repressurisation would be done Autogenously
  1944. The Cooling Mechanism to be used would be Radiative Cooling
  1945.  
  1946.  
  1947. Your Engine is called: CE-17N "Novo"
  1948. Your Engine Cycle is: Colloid Thruster
  1949. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  1950. Your engine's nozzle type should be: Capillary Emitter-Electrode Cone
  1951. Your Altitude of operation is: 80 km+ (Vacuum)
  1952. Tank repressurisation would be impractical and unnecessary
  1953. The Cooling Mechanism to be used would be Transpiration Cooling
  1954.  
  1955.  
  1956. Your Engine is called: LM10-912 "Tellus"
  1957. Your Engine Cycle is: Full Flow Staged
  1958. Your Oxidizer is: ClF5 (Chlorine Pentafluoride)
  1959. Your Fuel is: CH6N2 (MonomethylHydrazine)
  1960. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  1961. Your Altitude of operation is: 0-10 km (Sea Level)
  1962. Tank repressurisation would be done using Inert gas
  1963. The Cooling Mechanism to be used would be Transpiration Cooling
  1964.  
  1965.  
  1966. Your Engine is called: RL-249q "Liberty"
  1967. Your Engine Cycle is: "Expander Open" Pebble-Bed Core
  1968. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Ammonia (NH3) as a remass
  1969. Your Reactor's Fission Fuel is: 100-90% Uranium-235
  1970. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  1971. Your Altitude of operation is: 80 km+ (Vacuum)
  1972. Tank repressurisation would be done Autogenously
  1973. The Cooling Mechanism to be used would be Regenerative Cooling
  1974.  
  1975.  
  1976. Your Engine is called: PKA-977X "Voyager"
  1977. Your Engine Cycle is: Expander (Closed)
  1978. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  1979. Your Fuel is: B5H9 (Pentaborane)
  1980. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  1981. Your Altitude of operation is: 80 km+ (Vacuum)
  1982. Tank repressurisation would be done Autogenously
  1983. The Cooling Mechanism to be used would be Dump Cooling
  1984.  
  1985.  
  1986. Your Engine is called: LM10-453N "Arkon"
  1987. Your Engine Cycle is: Expander (Closed)
  1988. Your Oxidizer is: O3 (Ozone)
  1989. Your Fuel is: B2H6 (Diborane)
  1990. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  1991. Your Altitude of operation is: 80 km+ (Vacuum)
  1992. Tank repressurisation would be done Autogenously
  1993. The Cooling Mechanism to be used would be Radiative Cooling
  1994.  
  1995.  
  1996. Your Engine is called: AR-713X "Burlak"
  1997. Your Engine Cycle is: Staged Combustion (Oxidizer Rich)
  1998. Your Oxidizer is: N2H4 (Hydrazine)
  1999. Your Fuel is: 75% CH6N2 + 25% N2H4 (UH-25)
  2000. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  2001. Your Altitude of operation is: 80 km+ (Vacuum)
  2002. Tank repressurisation would be done using Inert gas
  2003. The Cooling Mechanism to be used would be Regenerative Cooling
  2004.  
  2005.  
  2006. Your Engine is called: DST-297A "Redstone"
  2007. Your Engine Cycle is: Staged Combustion (Oxidizer Rich)
  2008. Your Oxidizer is: N2O4 (Nitrogen Tetroxide)
  2009. Your Fuel is: C6H5NH2 (Aniline)
  2010. Your engine's nozzle type should be: Expanding Nozzle
  2011. Your Altitude of operation is: 80 km+ (Vacuum)
  2012. Tank repressurisation would be done using Inert gas
  2013. The Cooling Mechanism to be used would be Film Cooling
  2014.  
  2015.  
  2016. Your Engine is called: AR-1003K "Ustinov"
  2017. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  2018. Your Propellant is: Xenon
  2019. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  2020. Your Altitude of operation is: 80 km+ (Vacuum)
  2021. Tank repressurisation would be impractical and unnecessary
  2022. The Cooling Mechanism to be used would be Regenerative Cooling
  2023.  
  2024.  
  2025. Your Engine is called: RO-153T "Sokosha"
  2026. Your Engine Cycle is: Pressure-Fed
  2027. Your Oxidizer is: AK20F: 80% HNO3 + 20% N2O4 (Nitric Acid)
  2028. Your Fuel is: CH6N2 (MonomethylHydrazine)
  2029. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  2030. Your Altitude of operation is: 30-80 km (High Atmosphere)
  2031. Tank repressurisation would be done using Inert gas
  2032. The Cooling Mechanism to be used would be Transpiration Cooling
  2033.  
  2034.  
  2035. Your Engine is called: MJ-467W "Kometa"
  2036. Your Engine Cycle is: Pressure-Fed
  2037. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  2038. Your Fuel is: B5H9 (Pentaborane)
  2039. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2040. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  2041. Tank repressurisation would be done Autogenously
  2042. The Cooling Mechanism to be used would be Dump Cooling
  2043.  
  2044.  
  2045. Your Engine is called: AJ-382T "Dawn"
  2046. Your Engine Cycle is: "Expander Closed" Pulsed Nuclear
  2047. Your Propellant is: Helium (He)
  2048. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  2049. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2050. Your Altitude of operation is: 80 km+ (Vacuum)
  2051. Tank repressurisation would be done Autogenously
  2052. The Cooling Mechanism to be used would be Radiative Cooling
  2053.  
  2054.  
  2055. Your Engine is called: MV-588L "Mir"
  2056. Your Engine Cycle is: Dual Expander (Closed)
  2057. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  2058. Your Fuel is: H2 (Hydrogen)
  2059. Your engine's nozzle type should be: Linear Aerospike Nozzle
  2060. Your Altitude of operation is: Any Altitude (0-80 km+)
  2061. Tank repressurisation would be done Autogenously
  2062. The Cooling Mechanism to be used would be Dump Cooling
  2063.  
  2064.  
  2065. Your Engine is called: RD-746Y "Nexus"
  2066. Your Engine Cycle is: Gas Generator
  2067. Your Oxidizer is: AK27I: 73% HNO3 + 27% N2O4 (Nitric Acid)
  2068. Your Fuel is: C2H5OH(Ethanol) 85%
  2069. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  2070. Your Altitude of operation is: 30-80 km (High Atmosphere)
  2071. Tank repressurisation would be done Autogenously
  2072. The Cooling Mechanism to be used would be Film Cooling
  2073.  
  2074.  
  2075. Your Engine is called: RD-548o "Strela"
  2076. Your Engine Cycle is: Full Flow Staged
  2077. Your Oxidizer is: N2H4 (Hydrazine)
  2078. Your Fuel is: B5H9 (Pentaborane)
  2079. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  2080. Your Altitude of operation is: 0-10 km (Sea Level)
  2081. Tank repressurisation would be done using Inert gas
  2082. The Cooling Mechanism to be used would be Ablative Cooling
  2083.  
  2084.  
  2085. Your Engine is called: LE-74A "Hephaestus"
  2086. Your Engine Cycle is: Electric Pump Fed
  2087. Your Oxidizer is: AK27I: 73% HNO3 + 27% N2O4 (Nitric Acid)
  2088. Your Fuel is: CH6N2 (MonomethylHydrazine)
  2089. Your engine's nozzle type should be: Dual Bell Nozzle
  2090. Your Altitude of operation is: 30-80 km (High Atmosphere)
  2091. Tank repressurisation would be done using Inert gas
  2092. The Cooling Mechanism to be used would be Regenerative Cooling
  2093.  
  2094.  
  2095. Your Engine is called: TQ-307i "Surveyor"
  2096. Your Engine Cycle is: Dual Expander (Closed)
  2097. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  2098. Your Fuel is: H2 (Hydrogen)
  2099. Your engine's nozzle type should be: Dual Bell Nozzle
  2100. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  2101. Tank repressurisation would be done Autogenously
  2102. The Cooling Mechanism to be used would be Ablative Cooling
  2103.  
  2104.  
  2105. Your Engine is called: LE-173i "Atlantis"
  2106. Your Engine Cycle is: Pressure-Fed
  2107. Your Oxidizer is: N2H4 (Hydrazine)
  2108. Your Fuel is: B5H9 (Pentaborane)
  2109. Your engine's nozzle type should be: Expanding Nozzle
  2110. Your Altitude of operation is: 80 km+ (Vacuum)
  2111. Tank repressurisation would be done Autogenously
  2112. The Cooling Mechanism to be used would be Radiative Cooling
  2113.  
  2114.  
  2115. Your Engine is called: XLR-249C "Slava"
  2116. Your Engine Cycle is: Hall Effect Thruster
  2117. Your Propellant is: Iodine
  2118. Your engine's nozzle type should be: Hall Effect Thruster Nozzle
  2119. Your Altitude of operation is: 80 km+ (Vacuum)
  2120. Tank repressurisation would be impractical and unnecessary
  2121. The Cooling Mechanism to be used would be Dump Cooling
  2122.  
  2123.  
  2124. Your Engine is called: KDU-383J "Beta"
  2125. Your Engine Cycle is: Pressure-Fed
  2126. Your Oxidizer is: N2O4 (Nitrogen Tetroxide)
  2127. Your Fuel is: C2H8N2 (UnsymmetricalDimethylHydrazine)
  2128. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  2129. Your Altitude of operation is: 0-10 km (Sea Level)
  2130. Tank repressurisation would be done Autogenously
  2131. The Cooling Mechanism to be used would be Dump Cooling
  2132.  
  2133.  
  2134. Your Engine is called: RS-361T "Kapustin"
  2135. Your Engine Cycle is: Staged Combustion (Oxidizer Rich)
  2136. Your Oxidizer is: O2 (Oxygen)
  2137. Your Fuel is: CH6N2 (MonomethylHydrazine)
  2138. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  2139. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  2140. Tank repressurisation would be done Autogenously
  2141. The Cooling Mechanism to be used would be Ablative Cooling
  2142.  
  2143.  
  2144. Your Engine is called: AR-192 "Argus"
  2145. Your Engine Cycle is: "Expander Open" Pebble-Bed Core
  2146. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Ammonia (NH3) as a remass
  2147. Your Reactor's Fission Fuel is: 50% Uranium-235
  2148. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2149. Your Altitude of operation is: 80 km+ (Vacuum)
  2150. Tank repressurisation would be done using Inert gas
  2151. The Cooling Mechanism to be used would be Regenerative Cooling
  2152.  
  2153.  
  2154. Your Engine is called: TQ-176 "Atlas"
  2155. Your Engine Cycle is: MagnetoPlasmaDynamic Thruster
  2156. Your Propellant is: Neon
  2157. Your engine's nozzle type should be: Cathode Plug Magnetic Confinement Nozzle
  2158. Your Altitude of operation is: 80 km+ (Vacuum)
  2159. Tank repressurisation would be impractical and unnecessary
  2160. The Cooling Mechanism to be used would be Dump Cooling
  2161.  
  2162.  
  2163. Your Engine is called: RL-948V "Zarya"
  2164. Your Engine Cycle is: Dual Expander (Closed)
  2165. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  2166. Your Fuel is: H2 (Hydrogen)
  2167. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  2168. Your Altitude of operation is: 80 km+ (Vacuum)
  2169. Tank repressurisation would be done Autogenously
  2170. The Cooling Mechanism to be used would be Radiative Cooling
  2171.  
  2172.  
  2173. Your Engine is called: AJ-434b "Kazbek"
  2174. Your Engine Cycle is: "Expander Open" Pulsed Nuclear
  2175. Your Propellant is: Hydrogen (H)
  2176. Your Reactor's Fission Fuel is: 50% Uranium-235
  2177. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2178. Your Altitude of operation is: 80 km+ (Vacuum)
  2179. Tank repressurisation would be done Autogenously
  2180. The Cooling Mechanism to be used would be Radiative Cooling
  2181.  
  2182.  
  2183. Your Engine is called: XLR-577K "Ekran"
  2184. Your Engine Cycle is: Combustion Tap Off
  2185. Your Oxidizer is: N2O4 (Nitrogen Tetroxide)
  2186. Your Fuel is: B2H6 (Diborane)
  2187. Your engine's nozzle type should be: Toroidal Aerospike Nozzle
  2188. Your Altitude of operation is: Any Altitude (0-80 km+)
  2189. Tank repressurisation would be done Autogenously
  2190. The Cooling Mechanism to be used would be Film Cooling
  2191.  
  2192.  
  2193. Your Engine is called: AJ-514l "Vulcan"
  2194. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  2195. Your Propellant is: Argon
  2196. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  2197. Your Altitude of operation is: 80 km+ (Vacuum)
  2198. Tank repressurisation would be impractical and unnecessary
  2199. The Cooling Mechanism to be used would be Film Cooling
  2200.  
  2201.  
  2202. Your Engine is called: AR-307p "Stimuls"
  2203. Your Engine Cycle is: Gas Generator
  2204. Your Oxidizer is: ClF5 (Chlorine Pentafluoride)
  2205. Your Fuel is: CH3OH (Methanol)
  2206. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  2207. Your Altitude of operation is: 0-10 km (Sea Level)
  2208. Tank repressurisation would be done Autogenously
  2209. The Cooling Mechanism to be used would be Ablative Cooling
  2210.  
  2211.  
  2212. Your Engine is called: LE-950D "Oko"
  2213. Your Engine Cycle is: "Expander Closed" Pebble-Bed Core
  2214. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Nitrogen (N2) as a remass
  2215. Your Reactor's Fission Fuel is: 25-8% Uranium-235
  2216. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2217. Your Altitude of operation is: 80 km+ (Vacuum)
  2218. Tank repressurisation would be done using Inert gas
  2219. The Cooling Mechanism to be used would be Dump Cooling
  2220.  
  2221.  
  2222. Your Engine is called: KDU-916S "Condor"
  2223. Your Engine Cycle is: "Expander Bleed" Liquid Core
  2224. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Hydrogen (H2) + Hexane (C6H14) as a remass
  2225. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  2226. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2227. Your Altitude of operation is: 80 km+ (Vacuum)
  2228. Tank repressurisation would be done using Inert gas
  2229. The Cooling Mechanism to be used would be Dump Cooling
  2230.  
  2231.  
  2232. Your Engine is called: RO-146Q "Portal"
  2233. Your Engine Cycle is: Electric Pump Fed
  2234. Your Oxidizer is: ClF5 (Chlorine Pentafluoride)
  2235. Your Fuel is: C2H5OH(Ethanol) 85%
  2236. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  2237. Your Altitude of operation is: 80 km+ (Vacuum)
  2238. Tank repressurisation would be done Autogenously
  2239. The Cooling Mechanism to be used would be Radiative Cooling
  2240.  
  2241.  
  2242. Your Engine is called: MV-114N "Radon"
  2243. Your Engine Cycle is: Full Flow Staged
  2244. Your Oxidizer is: N2H4 (Hydrazine)
  2245. Your Fuel is: B5H9 (Pentaborane)
  2246. Your engine's nozzle type should be: Expanding Nozzle
  2247. Your Altitude of operation is: 80 km+ (Vacuum)
  2248. Tank repressurisation would be done Autogenously
  2249. The Cooling Mechanism to be used would be Dump Cooling
  2250.  
  2251.  
  2252. Your Engine is called: MV-586y "Kobra"
  2253. Your Engine Cycle is: Dual Expander (Open/Bleed)
  2254. Your Oxidizer is: O2 (Oxygen)
  2255. Your Fuel is: H2 (Hydrogen)
  2256. Your engine's nozzle type should be: Dual Bell Nozzle
  2257. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  2258. Tank repressurisation would be done Autogenously
  2259. The Cooling Mechanism to be used would be Regenerative Cooling
  2260.  
  2261.  
  2262. Your Engine is called: LE-316V "Ceres"
  2263. Your Engine Cycle is: Staged Combustion (Fuel Rich)
  2264. Your Oxidizer is: O3 (Ozone)
  2265. Your Fuel is: H2 (Hydrogen)
  2266. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  2267. Your Altitude of operation is: 80 km+ (Vacuum)
  2268. Tank repressurisation would be done using Inert gas
  2269. The Cooling Mechanism to be used would be Transpiration Cooling
  2270.  
  2271.  
  2272. Your Engine is called: KDTU-629F "Prometheus"
  2273. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  2274. Your Propellant is: Argon
  2275. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  2276. Your Altitude of operation is: 80 km+ (Vacuum)
  2277. Tank repressurisation would be impractical and unnecessary
  2278. The Cooling Mechanism to be used would be Transpiration Cooling
  2279.  
  2280.  
  2281. Your Engine is called: RO-701r "Proxima"
  2282. Your Engine Cycle is: "Expander Closed" Pulsed Nuclear
  2283. Your Propellant is: Ammonia (NH3)
  2284. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  2285. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2286. Your Altitude of operation is: 80 km+ (Vacuum)
  2287. Tank repressurisation would be done Autogenously
  2288. The Cooling Mechanism to be used would be Film Cooling
  2289.  
  2290.  
  2291. Your Engine is called: MV-712 "Vesper"
  2292. Your Engine Cycle is: Combustion Tap Off
  2293. Your Oxidizer is: N2O4 (Nitrogen Tetroxide)
  2294. Your Fuel is: C2H5OH(Ethanol) 75%
  2295. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2296. Your Altitude of operation is: 30-80 km (High Atmosphere)
  2297. Tank repressurisation would be done Autogenously
  2298. The Cooling Mechanism to be used would be Ablative Cooling
  2299.  
  2300.  
  2301. Your Engine is called: KDU-1009z "Altaris"
  2302. Your Engine Cycle is: Full Flow Staged
  2303. Your Oxidizer is: O3 (Ozone)
  2304. Your Fuel is: H2 (Hydrogen)
  2305. Your engine's nozzle type should be: Dual Bell Nozzle
  2306. Your Altitude of operation is: 30-80 km (High Atmosphere)
  2307. Tank repressurisation would be done using Inert gas
  2308. The Cooling Mechanism to be used would be Dump Cooling
  2309.  
  2310.  
  2311. Your Engine is called: MJ-830C "Vodopad"
  2312. Your Engine Cycle is: Dual Expander (Closed)
  2313. Your Oxidizer is: F2 (Fluorine)
  2314. Your Fuel is: H2 (Hydrogen)
  2315. Your engine's nozzle type should be: Toroidal Aerospike Nozzle
  2316. Your Altitude of operation is: Any Altitude (0-80 km+)
  2317. Tank repressurisation would be done Autogenously
  2318. The Cooling Mechanism to be used would be Film Cooling
  2319.  
  2320.  
  2321. Your Engine is called: RD-531k "Dynetics"
  2322. Your Engine Cycle is: Colloid Thruster
  2323. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  2324. Your engine's nozzle type should be: Capillary Emitter-Electrode Cone
  2325. Your Altitude of operation is: 80 km+ (Vacuum)
  2326. Tank repressurisation would be impractical and unnecessary
  2327. The Cooling Mechanism to be used would be Regenerative Cooling
  2328.  
  2329.  
  2330. Your Engine is called: RS-131r "Ekspress"
  2331. Your Engine Cycle is: Hall Effect Thruster
  2332. Your Propellant is: Xenon
  2333. Your engine's nozzle type should be: Hall Effect Thruster Nozzle
  2334. Your Altitude of operation is: 80 km+ (Vacuum)
  2335. Tank repressurisation would be impractical and unnecessary
  2336. The Cooling Mechanism to be used would be Film Cooling
  2337.  
  2338.  
  2339. Your Engine is called: AR-632 "Fram"
  2340. Your Engine Cycle is: Cold Gas Monopropellant
  2341. Your Propellant is: Hydrogen (H2)
  2342. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  2343. Your Altitude of operation is: 80 km+ (Vacuum)
  2344. Tank repressurisation would be impractical and unnecessary
  2345. The Cooling Mechanism to be used would be unnecessary
  2346.  
  2347.  
  2348. Your Engine is called: BE-326U "Aeonian"
  2349. Your Engine Cycle is: Monopropellant (Decomposition)
  2350. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  2351. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  2352. Your Altitude of operation is: 80 km+ (Vacuum)
  2353. Tank repressurisation would be impractical and unnecessary
  2354. The Cooling Mechanism to be used would be Dump Cooling
  2355.  
  2356.  
  2357. Your Engine is called: LE-552 "Lunokhod"
  2358. Your Engine Cycle is: "Expander Closed" Pebble-Bed Core
  2359. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Water (H2O) as a remass
  2360. Your Reactor's Fission Fuel is: 50% Uranium-235
  2361. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2362. Your Altitude of operation is: 80 km+ (Vacuum)
  2363. Tank repressurisation would be done Autogenously
  2364. The Cooling Mechanism to be used would be Dump Cooling
  2365.  
  2366.  
  2367. Your Engine is called: XLR-273A "Dreadnought"
  2368. Your Engine Cycle is: MagnetoPlasmaDynamic Thruster
  2369. Your Propellant is: Xenon
  2370. Your engine's nozzle type should be: Cathode Plug Magnetic Confinement Nozzle
  2371. Your Altitude of operation is: 80 km+ (Vacuum)
  2372. Tank repressurisation would be impractical and unnecessary
  2373. The Cooling Mechanism to be used would be Dump Cooling
  2374.  
  2375.  
  2376. Your Engine is called: LM10-684C "Nautilus"
  2377. Your Engine Cycle is: Combustion Tap Off
  2378. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  2379. Your Fuel is: CH6N2 (MonomethylHydrazine)
  2380. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  2381. Your Altitude of operation is: 0-10 km (Sea Level)
  2382. Tank repressurisation would be done Autogenously
  2383. The Cooling Mechanism to be used would be Regenerative Cooling
  2384.  
  2385.  
  2386. Your Engine is called: RS-661G "Prospector"
  2387. Your Engine Cycle is: MagnetoPlasmaDynamic Thruster
  2388. Your Propellant is: Hydrogen
  2389. Your engine's nozzle type should be: Cathode Plug Magnetic Confinement Nozzle
  2390. Your Altitude of operation is: 80 km+ (Vacuum)
  2391. Tank repressurisation would be impractical and unnecessary
  2392. The Cooling Mechanism to be used would be Regenerative Cooling
  2393.  
  2394.  
  2395. Your Engine is called: LRE-60u "Agena"
  2396. Your Engine Cycle is: Dual Expander (Closed)
  2397. Your Oxidizer is: O2 (Oxygen)
  2398. Your Fuel is: CH4 (Methane)
  2399. Your engine's nozzle type should be: Expansion-Deflection Nozzle
  2400. Your Altitude of operation is: Any Altitude (0-80 km+)
  2401. Tank repressurisation would be done Autogenously
  2402. The Cooling Mechanism to be used would be Radiative Cooling
  2403.  
  2404.  
  2405. Your Engine is called: PKA-446f "Ulysses"
  2406. Your Engine Cycle is: MagnetoPlasmaDynamic Thruster
  2407. Your Propellant is: Neon
  2408. Your engine's nozzle type should be: Cathode Plug Magnetic Confinement Nozzle
  2409. Your Altitude of operation is: 80 km+ (Vacuum)
  2410. Tank repressurisation would be impractical and unnecessary
  2411. The Cooling Mechanism to be used would be Radiative Cooling
  2412.  
  2413.  
  2414. Your Engine is called: XLR-196a "Connestoga"
  2415. Your Engine Cycle is: Cold Gas Monopropellant
  2416. Your Propellant is: Ammonia (NH3)
  2417. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  2418. Your Altitude of operation is: 80 km+ (Vacuum)
  2419. Tank repressurisation would be impractical and unnecessary
  2420. The Cooling Mechanism to be used would be unnecessary
  2421.  
  2422.  
  2423. Your Engine is called: LM10-702X "Eagle"
  2424. Your Engine Cycle is: Gas Generator
  2425. Your Oxidizer is: O2 (Oxygen)
  2426. Your Fuel is: N2H4 (Hydrazine)
  2427. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2428. Your Altitude of operation is: 30-80 km (High Atmosphere)
  2429. Tank repressurisation would be done using Inert gas
  2430. The Cooling Mechanism to be used would be Regenerative Cooling
  2431.  
  2432.  
  2433. Your Engine is called: KDTU-145l "Horizon"
  2434. Your Engine Cycle is: Staged Combustion (Oxidizer Rich)
  2435. Your Oxidizer is: N2O4 (Nitrogen Tetroxide)
  2436. Your Fuel is: 75% CH6N2 + 25% N2H4 (UH-25)
  2437. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  2438. Your Altitude of operation is: 0-10 km (Sea Level)
  2439. Tank repressurisation would be done using Inert gas
  2440. The Cooling Mechanism to be used would be Regenerative Cooling
  2441.  
  2442.  
  2443. Your Engine is called: TQ-89s "Magellan"
  2444. Your Engine Cycle is: Expander (Open/Bleed)
  2445. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  2446. Your Fuel is: C12H24 (Kerosene)
  2447. Your engine's nozzle type should be: Expanding Nozzle
  2448. Your Altitude of operation is: 80 km+ (Vacuum)
  2449. Tank repressurisation would be done Autogenously
  2450. The Cooling Mechanism to be used would be Ablative Cooling
  2451.  
  2452.  
  2453. Your Engine is called: AJ-391E "Kronos"
  2454. Your Engine Cycle is: Cold Gas Monopropellant
  2455. Your Propellant is: Carbon Dioxide (CO2)
  2456. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  2457. Your Altitude of operation is: 80 km+ (Vacuum)
  2458. Tank repressurisation would be impractical and unnecessary
  2459. The Cooling Mechanism to be used would be unnecessary
  2460.  
  2461.  
  2462. Your Engine is called: RS-559x "Dawn"
  2463. Your Engine Cycle is: "Vortex Confined" Liquid Core
  2464. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Water (H2O) as a remass
  2465. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  2466. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2467. Your Altitude of operation is: 80 km+ (Vacuum)
  2468. Tank repressurisation would be done Autogenously
  2469. The Cooling Mechanism to be used would be Transpiration Cooling
  2470.  
  2471.  
  2472. Your Engine is called: KRD-106V "Skiph"
  2473. Your Engine Cycle is: Cold Gas Monopropellant
  2474. Your Propellant is: Carbon Dioxide (CO2)
  2475. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  2476. Your Altitude of operation is: 80 km+ (Vacuum)
  2477. Tank repressurisation would be impractical and unnecessary
  2478. The Cooling Mechanism to be used would be unnecessary
  2479.  
  2480.  
  2481. Your Engine is called: BE-527T "Aurora"
  2482. Your Engine Cycle is: Full Flow Staged
  2483. Your Oxidizer is: ClF5 (Chlorine Pentafluoride)
  2484. Your Fuel is: C2H5OH(Ethanol) 85%
  2485. Your engine's nozzle type should be: Dual Bell Nozzle
  2486. Your Altitude of operation is: 30-80 km (High Atmosphere)
  2487. Tank repressurisation would be done Autogenously
  2488. The Cooling Mechanism to be used would be Film Cooling
  2489.  
  2490.  
  2491. Your Engine is called: BE-644H "Pluton"
  2492. Your Engine Cycle is: "Magnetohydrodynamic(MHD) vortex" Gas Core
  2493. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Water (H2O) as remass
  2494. Your Reactor's Fission Fuel is: 100-90% Uranium-235
  2495. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2496. Your Altitude of operation is: 80 km+ (Vacuum)
  2497. Tank repressurisation would be done using Inert gas
  2498. The Cooling Mechanism to be used would be Film Cooling
  2499.  
  2500.  
  2501. Your Engine is called: LM10-560 "Ariane"
  2502. Your Engine Cycle is: Full Flow Staged
  2503. Your Oxidizer is: ClF3 (Chlorine Trifluoride)
  2504. Your Fuel is: N2H4 (Hydrazine)
  2505. Your engine's nozzle type should be: Linear Aerospike Nozzle
  2506. Your Altitude of operation is: Any Altitude (0-80 km+)
  2507. Tank repressurisation would be done Autogenously
  2508. The Cooling Mechanism to be used would be Film Cooling
  2509.  
  2510.  
  2511. Your Engine is called: CE-594m "Heimdall"
  2512. Your Engine Cycle is: Gas Generator
  2513. Your Oxidizer is: H2O2 (Hydrogen Peroxide) 95%
  2514. Your Fuel is: C2H8N2 (UnsymmetricalDimethylHydrazine)
  2515. Your engine's nozzle type should be: Expansion-Deflection Nozzle
  2516. Your Altitude of operation is: Any Altitude (0-80 km+)
  2517. Tank repressurisation would be done using Inert gas
  2518. The Cooling Mechanism to be used would be Dump Cooling
  2519.  
  2520.  
  2521. Your Engine is called: YF-115S "Olympia"
  2522. Your Engine Cycle is: Combustion Tap Off
  2523. Your Oxidizer is: N2H4 (Hydrazine)
  2524. Your Fuel is: H2 (Hydrogen)
  2525. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  2526. Your Altitude of operation is: 0-10 km (Sea Level)
  2527. Tank repressurisation would be done using Inert gas
  2528. The Cooling Mechanism to be used would be Regenerative Cooling
  2529.  
  2530.  
  2531. Your Engine is called: BE-781Y "Voyager"
  2532. Your Engine Cycle is: Staged Combustion (Fuel Rich)
  2533. Your Oxidizer is: F2 (Fluorine)
  2534. Your Fuel is: NH3 (Ammonia)
  2535. Your engine's nozzle type should be: Dual Bell Nozzle
  2536. Your Altitude of operation is: 30-80 km (High Atmosphere)
  2537. Tank repressurisation would be done Autogenously
  2538. The Cooling Mechanism to be used would be Radiative Cooling
  2539.  
  2540.  
  2541. Your Engine is called: RO-612H "Irtysh"
  2542. Your Engine Cycle is: Full Flow Staged
  2543. Your Oxidizer is: N2O4 (Nitrogen Tetroxide)
  2544. Your Fuel is: 75% CH6N2 + 25% N2H4 (UH-25)
  2545. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  2546. Your Altitude of operation is: 30-80 km (High Atmosphere)
  2547. Tank repressurisation would be done Autogenously
  2548. The Cooling Mechanism to be used would be Ablative Cooling
  2549.  
  2550.  
  2551. Your Engine is called: MV-803U "Phoenix"
  2552. Your Engine Cycle is: Expander (Closed)
  2553. Your Oxidizer is: O3 (Ozone)
  2554. Your Fuel is: B2H6 (Diborane)
  2555. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  2556. Your Altitude of operation is: 80 km+ (Vacuum)
  2557. Tank repressurisation would be done Autogenously
  2558. The Cooling Mechanism to be used would be Radiative Cooling
  2559.  
  2560.  
  2561. Your Engine is called: LE-503Q "Almaz"
  2562. Your Engine Cycle is: Electric Pump Fed
  2563. Your Oxidizer is: H2O2 (Hydrogen Peroxide) 95%
  2564. Your Fuel is: 75% CH6N2 + 25% N2H4 (UH-25)
  2565. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  2566. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  2567. Tank repressurisation would be done Autogenously
  2568. The Cooling Mechanism to be used would be Dump Cooling
  2569.  
  2570.  
  2571. Your Engine is called: YF-797F "Salyut"
  2572. Your Engine Cycle is: Electric Pump Fed
  2573. Your Oxidizer is: ClF5 (Chlorine Pentafluoride)
  2574. Your Fuel is: N2H4 (Hydrazine)
  2575. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  2576. Your Altitude of operation is: 30-80 km (High Atmosphere)
  2577. Tank repressurisation would be done Autogenously
  2578. The Cooling Mechanism to be used would be Dump Cooling
  2579.  
  2580.  
  2581. Your Engine is called: DOK-370L "Mariner"
  2582. Your Engine Cycle is: Pressure-Fed
  2583. Your Oxidizer is: O2 (Oxygen)
  2584. Your Fuel is: B5H9 (Pentaborane)
  2585. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  2586. Your Altitude of operation is: 0-10 km (Sea Level)
  2587. Tank repressurisation would be done Autogenously
  2588. The Cooling Mechanism to be used would be Regenerative Cooling
  2589.  
  2590.  
  2591. Your Engine is called: DOK-724R "Vega"
  2592. Your Engine Cycle is: Electric Pump Fed
  2593. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  2594. Your Fuel is: CH3OH (Methanol)
  2595. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  2596. Your Altitude of operation is: 0-10 km (Sea Level)
  2597. Tank repressurisation would be done Autogenously
  2598. The Cooling Mechanism to be used would be Transpiration Cooling
  2599.  
  2600.  
  2601. Your Engine is called: RD-703I "Kronos"
  2602. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  2603. Your Propellant is: Argon
  2604. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  2605. Your Altitude of operation is: 80 km+ (Vacuum)
  2606. Tank repressurisation would be impractical and unnecessary
  2607. The Cooling Mechanism to be used would be Film Cooling
  2608.  
  2609.  
  2610. Your Engine is called: XLR-623N "Eridanus"
  2611. Your Engine Cycle is: Gridded Ion Thruster
  2612. Your Propellant is: Caesium
  2613. Your engine's nozzle type should be: Electrostatic Ion Nozzle
  2614. Your Altitude of operation is: 80 km+ (Vacuum)
  2615. Tank repressurisation would be impractical and unnecessary
  2616. The Cooling Mechanism to be used would be Dump Cooling
  2617.  
  2618.  
  2619. Your Engine is called: KDU-253F "Bastion"
  2620. Your Engine Cycle is: MagnetoPlasmaDynamic Thruster
  2621. Your Propellant is: Hydrogen
  2622. Your engine's nozzle type should be: Cathode Plug Magnetic Confinement Nozzle
  2623. Your Altitude of operation is: 80 km+ (Vacuum)
  2624. Tank repressurisation would be impractical and unnecessary
  2625. The Cooling Mechanism to be used would be Transpiration Cooling
  2626.  
  2627.  
  2628. Your Engine is called: MJ-759A "Ikar"
  2629. Your Engine Cycle is: Monopropellant (Decomposition)
  2630. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  2631. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  2632. Your Altitude of operation is: 80 km+ (Vacuum)
  2633. Tank repressurisation would be impractical and unnecessary
  2634. The Cooling Mechanism to be used would be Radiative Cooling
  2635.  
  2636.  
  2637. Your Engine is called: LRE-914W "Astra"
  2638. Your Engine Cycle is: Gridded Ion Thruster
  2639. Your Propellant is: Xenon
  2640. Your engine's nozzle type should be: Electrostatic Ion Nozzle
  2641. Your Altitude of operation is: 80 km+ (Vacuum)
  2642. Tank repressurisation would be impractical and unnecessary
  2643. The Cooling Mechanism to be used would be Film Cooling
  2644.  
  2645.  
  2646. Your Engine is called: DST-387T "Philae"
  2647. Your Engine Cycle is: Colloid Thruster
  2648. Your Propellant is: NH2OH+NO3 (Hydroxylammonium nitrate)
  2649. Your engine's nozzle type should be: Capillary Emitter-Electrode Cone
  2650. Your Altitude of operation is: 80 km+ (Vacuum)
  2651. Tank repressurisation would be impractical and unnecessary
  2652. The Cooling Mechanism to be used would be Dump Cooling
  2653.  
  2654.  
  2655. Your Engine is called: RL-92v "Sputnik"
  2656. Your Engine Cycle is: Gas Generator
  2657. Your Oxidizer is: AK27P: 73% HNO3 + 27% N2O4 (Nitric Acid)
  2658. Your Fuel is: CH6N2 (MonomethylHydrazine)
  2659. Your engine's nozzle type should be: Expansion-Deflection Nozzle
  2660. Your Altitude of operation is: Any Altitude (0-80 km+)
  2661. Tank repressurisation would be done using Inert gas
  2662. The Cooling Mechanism to be used would be Dump Cooling
  2663.  
  2664.  
  2665. Your Engine is called: MJ-531X "Spartacus"
  2666. Your Engine Cycle is: Electric Pump Fed
  2667. Your Oxidizer is: N2O4 (Nitrogen Tetroxide)
  2668. Your Fuel is: N2H4 (Hydrazine)
  2669. Your engine's nozzle type should be: Linear Aerospike Nozzle
  2670. Your Altitude of operation is: Any Altitude (0-80 km+)
  2671. Tank repressurisation would be done using Inert gas
  2672. The Cooling Mechanism to be used would be Film Cooling
  2673.  
  2674.  
  2675. Your Engine is called: XS-218B "Cheget"
  2676. Your Engine Cycle is: Electric Pump Fed
  2677. Your Oxidizer is: AK27I: 73% HNO3 + 27% N2O4 (Nitric Acid)
  2678. Your Fuel is: N2H4 (Hydrazine)
  2679. Your engine's nozzle type should be: Expansion-Deflection Nozzle
  2680. Your Altitude of operation is: Any Altitude (0-80 km+)
  2681. Tank repressurisation would be done Autogenously
  2682. The Cooling Mechanism to be used would be Dump Cooling
  2683.  
  2684.  
  2685. Your Engine is called: AR-135E "Uragan"
  2686. Your Engine Cycle is: "Expander Closed" Pebble-Bed Core
  2687. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Carbon Monoxide (CO) as a remass
  2688. Your Reactor's Fission Fuel is: 100-90% Uranium-235
  2689. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2690. Your Altitude of operation is: 80 km+ (Vacuum)
  2691. Tank repressurisation would be done using Inert gas
  2692. The Cooling Mechanism to be used would be Transpiration Cooling
  2693.  
  2694.  
  2695. Your Engine is called: CE-257F "Quaoar"
  2696. Your Engine Cycle is: Nuclear SaltWater
  2697. Your Propellant is: Uranium TetraBromide (UBr4) + Water (H2O)
  2698. Your Reactor's Fission Fuel is: 50% Uranium-235
  2699. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2700. Your Altitude of operation is: 80 km+ (Vacuum)
  2701. Tank repressurisation would be done Autogenously
  2702. The Cooling Mechanism to be used would be Dump Cooling
  2703.  
  2704.  
  2705. Your Engine is called: MV-261b "Jubilance"
  2706. Your Engine Cycle is: Staged Combustion (Fuel Rich)
  2707. Your Oxidizer is: F2 (Fluorine)
  2708. Your Fuel is: N2H4 (Hydrazine)
  2709. Your engine's nozzle type should be: Dual Bell Nozzle
  2710. Your Altitude of operation is: 30-80 km (High Atmosphere)
  2711. Tank repressurisation would be done using Inert gas
  2712. The Cooling Mechanism to be used would be Radiative Cooling
  2713.  
  2714.  
  2715. Your Engine is called: MV-948F "Mir"
  2716. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  2717. Your Propellant is: Krypton
  2718. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  2719. Your Altitude of operation is: 80 km+ (Vacuum)
  2720. Tank repressurisation would be impractical and unnecessary
  2721. The Cooling Mechanism to be used would be Transpiration Cooling
  2722.  
  2723.  
  2724. Your Engine is called: R-460r "Argosy"
  2725. Your Engine Cycle is: Full Flow Staged
  2726. Your Oxidizer is: AK20K: 80% HNO3 + 20% N2O4 (Nitric Acid)
  2727. Your Fuel is: CH3OH (Methanol)
  2728. Your engine's nozzle type should be: Dual Bell Nozzle
  2729. Your Altitude of operation is: 30-80 km (High Atmosphere)
  2730. Tank repressurisation would be done Autogenously
  2731. The Cooling Mechanism to be used would be Ablative Cooling
  2732.  
  2733.  
  2734. Your Engine is called: PKA-134V "Svir"
  2735. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  2736. Your Propellant is: Krypton
  2737. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  2738. Your Altitude of operation is: 80 km+ (Vacuum)
  2739. Tank repressurisation would be impractical and unnecessary
  2740. The Cooling Mechanism to be used would be Transpiration Cooling
  2741.  
  2742.  
  2743. Your Engine is called: LE-909a "Cyclero"
  2744. Your Engine Cycle is: Dual Expander (Closed)
  2745. Your Oxidizer is: F2 (Fluorine)
  2746. Your Fuel is: H2 (Hydrogen)
  2747. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  2748. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  2749. Tank repressurisation would be done Autogenously
  2750. The Cooling Mechanism to be used would be Dump Cooling
  2751.  
  2752.  
  2753. Your Engine is called: YF-19w "Varagian"
  2754. Your Engine Cycle is: "Expander Closed" Pebble-Bed Core
  2755. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Oxygen (O2) as a remass
  2756. Your Reactor's Fission Fuel is: 25-8% Uranium-235
  2757. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2758. Your Altitude of operation is: 80 km+ (Vacuum)
  2759. Tank repressurisation would be done using Inert gas
  2760. The Cooling Mechanism to be used would be Radiative Cooling
  2761.  
  2762.  
  2763. Your Engine is called: HM-547M "Kratos"
  2764. Your Engine Cycle is: Expander (Open/Bleed)
  2765. Your Oxidizer is: O3 (Ozone)
  2766. Your Fuel is: C12H24 (Kerosene)
  2767. Your engine's nozzle type should be: Expansion-Deflection Nozzle
  2768. Your Altitude of operation is: Any Altitude (0-80 km+)
  2769. Tank repressurisation would be done Autogenously
  2770. The Cooling Mechanism to be used would be Radiative Cooling
  2771.  
  2772.  
  2773. Your Engine is called: MV-352 "Tsygan"
  2774. Your Engine Cycle is: "Expander Bleed" Liquid Core
  2775. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Hydrogen (H2) as a remass
  2776. Your Reactor's Fission Fuel is: 1-2% Uranium-235
  2777. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2778. Your Altitude of operation is: 80 km+ (Vacuum)
  2779. Tank repressurisation would be done using Inert gas
  2780. The Cooling Mechanism to be used would be Regenerative Cooling
  2781.  
  2782.  
  2783. Your Engine is called: R-858G "Bastion"
  2784. Your Engine Cycle is: Electric Pump Fed
  2785. Your Oxidizer is: AK20F: 80% HNO3 + 20% N2O4 (Nitric Acid)
  2786. Your Fuel is: N2H4 (Hydrazine)
  2787. Your engine's nozzle type should be: De Laval Cone (Without Nozzle Extension)
  2788. Your Altitude of operation is: 0-10 km (Sea Level)
  2789. Tank repressurisation would be done Autogenously
  2790. The Cooling Mechanism to be used would be Dump Cooling
  2791.  
  2792.  
  2793. Your Engine is called: LM10-193B "Shenzhou"
  2794. Your Engine Cycle is: Hall Effect Thruster
  2795. Your Propellant is: Xenon
  2796. Your engine's nozzle type should be: Hall Effect Thruster Nozzle
  2797. Your Altitude of operation is: 80 km+ (Vacuum)
  2798. Tank repressurisation would be impractical and unnecessary
  2799. The Cooling Mechanism to be used would be Regenerative Cooling
  2800.  
  2801.  
  2802. Your Engine is called: XLR-14L "Skiph"
  2803. Your Engine Cycle is: Nuclear SaltWater
  2804. Your Propellant is: Uranium TetraBromide (UBr4) + Water (H2O)
  2805. Your Reactor's Fission Fuel is: 50% Uranium-235
  2806. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2807. Your Altitude of operation is: 80 km+ (Vacuum)
  2808. Tank repressurisation would be done using Inert gas
  2809. The Cooling Mechanism to be used would be Regenerative Cooling
  2810.  
  2811.  
  2812. Your Engine is called: PKA-498N "Zenit"
  2813. Your Engine Cycle is: Dual Expander (Open/Bleed)
  2814. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  2815. Your Fuel is: H2 (Hydrogen)
  2816. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  2817. Your Altitude of operation is: 0-10 km (Sea Level)
  2818. Tank repressurisation would be done Autogenously
  2819. The Cooling Mechanism to be used would be Radiative Cooling
  2820.  
  2821.  
  2822. Your Engine is called: LM10-247n "Kometa"
  2823. Your Engine Cycle is: Expander (Closed)
  2824. Your Oxidizer is: F2 (Fluorine)
  2825. Your Fuel is: NH3 (Ammonia)
  2826. Your engine's nozzle type should be: Toroidal Aerospike Nozzle
  2827. Your Altitude of operation is: Any Altitude (0-80 km+)
  2828. Tank repressurisation would be done Autogenously
  2829. The Cooling Mechanism to be used would be Radiative Cooling
  2830.  
  2831.  
  2832. Your Engine is called: XLR-787G "Sever"
  2833. Your Engine Cycle is: "Expander Closed" Pulsed Nuclear
  2834. Your Propellant is: Water (H2O)
  2835. Your Reactor's Fission Fuel is: 50% Plutonium-238
  2836. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2837. Your Altitude of operation is: 80 km+ (Vacuum)
  2838. Tank repressurisation would be done using Inert gas
  2839. The Cooling Mechanism to be used would be Regenerative Cooling
  2840.  
  2841.  
  2842. Your Engine is called: KDTU-379U "Skiph"
  2843. Your Engine Cycle is: Staged Combustion (Fuel Rich)
  2844. Your Oxidizer is: O3 (Ozone)
  2845. Your Fuel is: H2 (Hydrogen)
  2846. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  2847. Your Altitude of operation is: 0-10 km (Sea Level)
  2848. Tank repressurisation would be done using Inert gas
  2849. The Cooling Mechanism to be used would be Radiative Cooling
  2850.  
  2851.  
  2852. Your Engine is called: RD-222E "Almaz"
  2853. Your Engine Cycle is: Combustion Tap Off
  2854. Your Oxidizer is: O3 (Ozone)
  2855. Your Fuel is: 50% CH6N2 + 50% N2H4 (Aerosine-50)
  2856. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  2857. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  2858. Tank repressurisation would be done using Inert gas
  2859. The Cooling Mechanism to be used would be Ablative Cooling
  2860.  
  2861.  
  2862. Your Engine is called: AJ-222H "Tetrapoda"
  2863. Your Engine Cycle is: Combustion Tap Off
  2864. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  2865. Your Fuel is: 50% CH6N2 + 50% N2H4 (Aerosine-50)
  2866. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  2867. Your Altitude of operation is: 80 km+ (Vacuum)
  2868. Tank repressurisation would be done using Inert gas
  2869. The Cooling Mechanism to be used would be Regenerative Cooling
  2870.  
  2871.  
  2872. Your Engine is called: XLR-663N "Salyut"
  2873. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  2874. Your Propellant is: Argon
  2875. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  2876. Your Altitude of operation is: 80 km+ (Vacuum)
  2877. Tank repressurisation would be impractical and unnecessary
  2878. The Cooling Mechanism to be used would be Regenerative Cooling
  2879.  
  2880.  
  2881. Your Engine is called: KDTU-137B "Kosmos"
  2882. Your Engine Cycle is: MagnetoPlasmaDynamic Thruster
  2883. Your Propellant is: Hydrazine
  2884. Your engine's nozzle type should be: Cathode Plug Magnetic Confinement Nozzle
  2885. Your Altitude of operation is: 80 km+ (Vacuum)
  2886. Tank repressurisation would be impractical and unnecessary
  2887. The Cooling Mechanism to be used would be Transpiration Cooling
  2888.  
  2889.  
  2890. Your Engine is called: PKA-555W "Athena"
  2891. Your Engine Cycle is: "Expander Open" Solid Core
  2892. Your Propellant is: Hydrogen (H2)
  2893. Your Reactor's Fission Fuel is: 100-90% Plutonium-238
  2894. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2895. Your Altitude of operation is: 80 km+ (Vacuum)
  2896. Tank repressurisation would be done Autogenously
  2897. The Cooling Mechanism to be used would be Regenerative Cooling
  2898.  
  2899.  
  2900. Your Engine is called: KDTU-435d "Onatchesko"
  2901. Your Engine Cycle is: Combustion Tap Off
  2902. Your Oxidizer is: F2 (Fluorine)
  2903. Your Fuel is: CH3OH (Methanol)
  2904. Your engine's nozzle type should be: Toroidal Aerospike Nozzle
  2905. Your Altitude of operation is: Any Altitude (0-80 km+)
  2906. Tank repressurisation would be done using Inert gas
  2907. The Cooling Mechanism to be used would be Dump Cooling
  2908.  
  2909.  
  2910. Your Engine is called: YF-722E "Twitch"
  2911. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  2912. Your Propellant is: Krypton
  2913. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  2914. Your Altitude of operation is: 80 km+ (Vacuum)
  2915. Tank repressurisation would be impractical and unnecessary
  2916. The Cooling Mechanism to be used would be Transpiration Cooling
  2917.  
  2918.  
  2919. Your Engine is called: LE-221v "Poisk"
  2920. Your Engine Cycle is: "Vortex Confined" Pebble-Bed Core
  2921. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Hydrogen (H2) + Hexane (C6H14) as a remass
  2922. Your Reactor's Fission Fuel is: 50% Uranium-235
  2923. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2924. Your Altitude of operation is: 80 km+ (Vacuum)
  2925. Tank repressurisation would be done using Inert gas
  2926. The Cooling Mechanism to be used would be Film Cooling
  2927.  
  2928.  
  2929. Your Engine is called: RD-137D "Horizon"
  2930. Your Engine Cycle is: Electric Pump Fed
  2931. Your Oxidizer is: F2 (Fluorine) + O2 (Oxygen)
  2932. Your Fuel is: B5H9 (Pentaborane)
  2933. Your engine's nozzle type should be: Toroidal Aerospike Nozzle
  2934. Your Altitude of operation is: Any Altitude (0-80 km+)
  2935. Tank repressurisation would be done Autogenously
  2936. The Cooling Mechanism to be used would be Regenerative Cooling
  2937.  
  2938.  
  2939. Your Engine is called: BE-954W "Artyom"
  2940. Your Engine Cycle is: "Expander Bleed" Pebble-Bed Core
  2941. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Carbon Monoxide (CO) as a remass
  2942. Your Reactor's Fission Fuel is: 50% Uranium-235
  2943. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2944. Your Altitude of operation is: 80 km+ (Vacuum)
  2945. Tank repressurisation would be done Autogenously
  2946. The Cooling Mechanism to be used would be Film Cooling
  2947.  
  2948.  
  2949. Your Engine is called: DOK-639N "Hyperion"
  2950. Your Engine Cycle is: "Wheel Flow" Gas Core
  2951. Your Propellant is: Uranium HexaFluoride Salt (UF6) and Hydrogen (H2) as remass
  2952. Your Reactor's Fission Fuel is: 100-90% Uranium-235
  2953. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2954. Your Altitude of operation is: 80 km+ (Vacuum)
  2955. Tank repressurisation would be done Autogenously
  2956. The Cooling Mechanism to be used would be Dump Cooling
  2957.  
  2958.  
  2959. Your Engine is called: AR-829A "Zarya"
  2960. Your Engine Cycle is: Nuclear SaltWater
  2961. Your Propellant is: Uranium TetraBromide (UBr4) + Water (H2O)
  2962. Your Reactor's Fission Fuel is: 25-8% Uranium-235
  2963. Your engine's nozzle type should be: De Laval Bell (With Nozzle Extension)
  2964. Your Altitude of operation is: 80 km+ (Vacuum)
  2965. Tank repressurisation would be done Autogenously
  2966. The Cooling Mechanism to be used would be Transpiration Cooling
  2967.  
  2968.  
  2969. Your Engine is called: NK-622K "Kondor"
  2970. Your Engine Cycle is: MagnetoPlasmaDynamic Thruster
  2971. Your Propellant is: Argon
  2972. Your engine's nozzle type should be: Cathode Plug Magnetic Confinement Nozzle
  2973. Your Altitude of operation is: 80 km+ (Vacuum)
  2974. Tank repressurisation would be impractical and unnecessary
  2975. The Cooling Mechanism to be used would be Radiative Cooling
  2976.  
  2977.  
  2978. Your Engine is called: KDTU-672 "Perseverence"
  2979. Your Engine Cycle is: Staged Combustion (Fuel Rich)
  2980. Your Oxidizer is: F2 (Fluorine)
  2981. Your Fuel is: N2H4 (Hydrazine)
  2982. Your engine's nozzle type should be: De Laval Bell (Without Nozzle Extension)
  2983. Your Altitude of operation is: 20-30 km (Medium Atmosphere)
  2984. Tank repressurisation would be done using Inert gas
  2985. The Cooling Mechanism to be used would be Regenerative Cooling
  2986.  
  2987.  
  2988. Your Engine is called: PKA-665Y "Zephyr"
  2989. Your Engine Cycle is: Staged Combustion (Oxidizer Rich)
  2990. Your Oxidizer is: N2O4 (Nitrogen Tetroxide)
  2991. Your Fuel is: 50% CH6N2 + 50% N2H4 (Aerosine-50)
  2992. Your engine's nozzle type should be: De Laval Cone (With Nozzle Extension)
  2993. Your Altitude of operation is: 80 km+ (Vacuum)
  2994. Tank repressurisation would be done using Inert gas
  2995. The Cooling Mechanism to be used would be Ablative Cooling
  2996.  
  2997.  
  2998. Your Engine is called: AJ-639F "Eagle"
  2999. Your Engine Cycle is: Hall Effect Thruster
  3000. Your Propellant is: Zinc
  3001. Your engine's nozzle type should be: Hall Effect Thruster Nozzle
  3002. Your Altitude of operation is: 80 km+ (Vacuum)
  3003. Tank repressurisation would be impractical and unnecessary
  3004. The Cooling Mechanism to be used would be Film Cooling
  3005.  
  3006.  
  3007. Your Engine is called: LM10-701n "Resurs"
  3008. Your Engine Cycle is: Variable Specific Impulse Magnetoplasma Rocket (VASIMR)
  3009. Your Propellant is: Krypton
  3010. Your engine's nozzle type should be: VASIMR Magnetic Confinement Nozzle
  3011. Your Altitude of operation is: 80 km+ (Vacuum)
  3012. Tank repressurisation would be impractical and unnecessary
  3013. The Cooling Mechanism to be used would be Transpiration Cooling
Tags: data informational output
Advertisement
Add Comment
Please, Sign In to add comment
Public Pastes
We use cookies for various purposes including analytics. By continuing to use Pastebin, you agree to our use of cookies as described in the Cookies Policy.  OK, I Understand
Not a member of Pastebin yet?
Sign Up, it unlocks many cool features!