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  1. @PART[straightslat]:NEEDS[FerramAerospaceResearch]
  2. {
  3.     @module = Part
  4.     @maximum_drag = 0
  5.     @minimum_drag = 0
  6.     @angularDrag = 0
  7.     @dragCoeff = 0
  8.     @deflectionLiftCoeff = 0
  9.     !MODULE[ModuleLiftingSurface] {}
  10.     MODULE
  11.     {
  12.         name = FARControllableSurface
  13.         MAC = 0.351
  14.         MidChordSweep = 0
  15.         maxdeflect = 45
  16.         b_2 = 1.828
  17.         TaperRatio = 1
  18.         ctrlSurfFrac = 1
  19.         transformName = straight
  20.     }
  21. }
  22.  
  23. @PART[spoilerflap]:NEEDS[FerramAerospaceResearch]
  24. {
  25.     @module = Part
  26.     @maximum_drag = 0
  27.     @minimum_drag = 0
  28.     @angularDrag = 0
  29.     @dragCoeff = 0
  30.     @deflectionLiftCoeff = 0
  31.     !MODULE[ModuleLiftingSurface] {}
  32.     MODULE
  33.     {
  34.         name = FARControllableSurface
  35.         MAC = 0.478
  36.         MidChordSweep = 0
  37.         maxdeflect = 45
  38.         b_2 = 3.53
  39.         TaperRatio = 1
  40.         ctrlSurfFrac = 1
  41.         transformName = surface
  42.     }
  43. }
  44.  
  45. @PART[kruegerflap]:NEEDS[FerramAerospaceResearch]
  46. {
  47.     @module = Part
  48.     @maximum_drag = 0
  49.     @minimum_drag = 0
  50.     @angularDrag = 0
  51.     @dragCoeff = 0
  52.     @deflectionLiftCoeff = 0
  53.     !MODULE[ModuleLiftingSurface] {}
  54.     MODULE
  55.     {
  56.         name = FARControllableSurface
  57.         MAC = 0.326
  58.         MidChordSweep = 0
  59.         maxdeflect = 30
  60.         b_2 = 1.66
  61.         TaperRatio = 1
  62.         ctrlSurfFrac = 1
  63.         transformName = flap
  64.     }
  65. }
  66.  
  67. @PART[doublefowlerflap]:NEEDS[FerramAerospaceResearch]
  68. {
  69.     @module = Part
  70.     @maximum_drag = 0
  71.     @minimum_drag = 0
  72.     @angularDrag = 0
  73.     @dragCoeff = 0
  74.     @deflectionLiftCoeff = 0
  75.     !MODULE[ModuleLiftingSurface] {}
  76.     MODULE
  77.     {
  78.         name = FARControllableSurface
  79.         MAC = 0.9
  80.         MidChordSweep = 0
  81.         maxdeflect = 30
  82.         b_2 = 3.51
  83.         TaperRatio = 1
  84.         ctrlSurfFrac = 1
  85.         transformName = slata
  86.     }
  87.     MODULE
  88.     {
  89.         name = FARControllableSurface
  90.         MAC = 0.47
  91.         MidChordSweep = 0
  92.         maxdeflect = 30
  93.         b_2 = 3.51
  94.         TaperRatio = 1
  95.         ctrlSurfFrac = 1
  96.         transformName = slatb
  97.     }
  98. }
  99.  
  100. @PART[migwing]:NEEDS[FerramAerospaceResearch]
  101. {
  102.     @module = Part
  103.     @maximum_drag = 0
  104.     @minimum_drag = 0
  105.     @angularDrag = 0
  106.     @dragCoeff = 0
  107.     @deflectionLiftCoeff = 0
  108.     !MODULE[ModuleLiftingSurface] {}
  109.     MODULE
  110.     {
  111.         name = FARControllableSurface
  112.         MAC = 1.706
  113.         MidChordSweep = 50
  114.         maxdeflect = 25
  115.         b_2 = 2.08
  116.         TaperRatio = 0.196
  117.         ctrlSurfFrac = 0.155
  118.         transformName = obj_ctrlSrf
  119.     }
  120. }
  121.  
  122. @PART[warhawkfin]:NEEDS[FerramAerospaceResearch]
  123. {
  124.     @module = Part
  125.     @maximum_drag = 0
  126.     @minimum_drag = 0
  127.     @angularDrag = 0
  128.     @dragCoeff = 0
  129.     @deflectionLiftCoeff = 0
  130.     !MODULE[ModuleLiftingSurface] {}
  131.     MODULE
  132.     {
  133.         name = FARControllableSurface
  134.         MAC = 2.19
  135.         MidChordSweep = 30
  136.         maxdeflect = 20
  137.         b_2 = 2.45
  138.         TaperRatio = 0.43
  139.         ctrlSurfFrac = 0.465
  140.         transformName = ctrlSrf
  141.     }
  142. }
  143.  
  144. @PART[wing4]:NEEDS[FerramAerospaceResearch]
  145. {
  146.     @module = Part
  147.     @maximum_drag = 0
  148.     @minimum_drag = 0
  149.     @angularDrag = 0
  150.     @dragCoeff = 0
  151.     @deflectionLiftCoeff = 0
  152.     !MODULE[ModuleLiftingSurface] {}
  153.     MODULE
  154.     {
  155.         name = FARWingAerodynamicModel
  156.         MAC = 1.06
  157.         MidChordSweep = 14
  158.         b_2 = 1.9
  159.         TaperRatio = 0.64
  160.         nonSideAttach = 0
  161.     }
  162. }
  163.  
  164. @PART[wingtip]:NEEDS[FerramAerospaceResearch]
  165. {
  166.     @module = Part
  167.     @maximum_drag = 0
  168.     @minimum_drag = 0
  169.     @angularDrag = 0
  170.     @dragCoeff = 0
  171.     @deflectionLiftCoeff = 0
  172.     !MODULE[ModuleLiftingSurface] {}
  173.     MODULE
  174.     {
  175.         name = FARWingAerodynamicModel
  176.         MAC = 0.9
  177.         MidChordSweep = -15
  178.         b_2 = 0.51
  179.         TaperRatio = 0.15
  180.         nonSideAttach = 0
  181.     }
  182. }
  183.  
  184. @PART[hanglel]:NEEDS[FerramAerospaceResearch]
  185. {
  186.     @module = Part
  187.     @maximum_drag = 0
  188.     @minimum_drag = 0
  189.     @angularDrag = 0
  190.     @dragCoeff = 0
  191.     @deflectionLiftCoeff = 0
  192.     !MODULE[ModuleLiftingSurface] {}
  193.     MODULE
  194.     {
  195.         name = FARWingAerodynamicModel
  196.         MAC = 0.26
  197.         MidChordSweep = 3.5
  198.         b_2 = 1.89
  199.         TaperRatio = 0.54
  200.         nonSideAttach = 1
  201.     }
  202. }
  203.  
  204. @PART[hangles]:NEEDS[FerramAerospaceResearch] // redo
  205. {
  206.     @module = Part
  207.     @maximum_drag = 0
  208.     @minimum_drag = 0
  209.     @angularDrag = 0
  210.     @dragCoeff = 0
  211.     @deflectionLiftCoeff = 0
  212.     !MODULE[ModuleLiftingSurface] {}
  213.     MODULE
  214.     {
  215.         name = FARWingAerodynamicModel
  216.         MAC = 0.27
  217.         MidChordSweep = 9
  218.         b_2 = 0.93
  219.         TaperRatio = 0.54
  220.         nonSideAttach = 1
  221.     }
  222. }
  223.  
  224. @PART[vanglel]:NEEDS[FerramAerospaceResearch]
  225. {
  226.     @module = Part
  227.     @maximum_drag = 0
  228.     @minimum_drag = 0
  229.     @angularDrag = 0
  230.     @dragCoeff = 0
  231.     @deflectionLiftCoeff = 0
  232.     !MODULE[ModuleLiftingSurface] {}
  233.     MODULE
  234.     {
  235.         name = FARWingAerodynamicModel
  236.         MAC = 0.12
  237.         MidChordSweep = 4.3
  238.         b_2 = 0.94
  239.         TaperRatio = 0.44
  240.         nonSideAttach = 1
  241.     }
  242. }
  243.  
  244. @PART[vangles]:NEEDS[FerramAerospaceResearch]
  245. {
  246.     @module = Part
  247.     @maximum_drag = 0
  248.     @minimum_drag = 0
  249.     @angularDrag = 0
  250.     @dragCoeff = 0
  251.     @deflectionLiftCoeff = 0
  252.     !MODULE[ModuleLiftingSurface] {}
  253.     MODULE
  254.     {
  255.         name = FARWingAerodynamicModel
  256.         MAC = 0.10
  257.         MidChordSweep = 4
  258.         b_2 = 0.47
  259.         TaperRatio = 0.59
  260.         nonSideAttach = 1
  261.     }
  262. }
  263.  
  264.  
  265. // Wronk's config starts here
  266. //Cockpits
  267. //Mk1 Business Cockpit
  268. @PART[citationcockpit]:AFTER[FerramAerospaceResearch]
  269. {
  270.     @MODULE[GeometryPartModule]
  271.     {
  272.         %forceUseMeshes = True
  273.         %ignoreIfNoRenderer = true
  274.     }
  275. }
  276.  
  277. //Mk3S1.5 Viewer's Cockpit
  278. @PART[hueycockpit]:AFTER[FerramAerospaceResearch]
  279. {
  280.     @MODULE[GeometryPartModule]
  281.     {
  282.         %forceUseMeshes = True
  283.         %ignoreIfNoRenderer = true
  284.     }
  285. }
  286.  
  287. //Size 2 Non-Commercial Cockpit
  288. @PART[herculescockpit]:AFTER[FerramAerospaceResearch]
  289. {
  290.     @MODULE[GeometryPartModule]
  291.     {
  292.         %forceUseMeshes = True
  293.         %ignoreIfNoRenderer = true
  294.     }
  295. }
  296.  
  297. @PART[falconcocpit]:NEEDS[FerramAerospaceResearch]
  298. {
  299.     @module = Part
  300.     @maximum_drag = 0
  301.     @minimum_drag = 0
  302.     @angularDrag = 0
  303.     @dragCoeff = 0
  304.     @deflectionLiftCoeff = 0
  305.     !MODULE[ModuleLiftingSurface] {}
  306.     MODULE
  307.     {
  308.         name = FARWingAerodynamicModel
  309.         MAC = 1.45
  310.         MidChordSweep = 80
  311.         b_2 = 0.72
  312.         TaperRatio = 0.25
  313.     }
  314. }
  315.  
  316. //Misc
  317. //Size 2 Crew Cabin
  318. @PART[size2CrewCabin]:AFTER[FerramAerospaceResearch]
  319. {
  320.     @MODULE[GeometryPartModule]
  321.     {
  322.         %forceUseMeshes = True
  323.         %ignoreIfNoRenderer = true
  324.     }
  325. }
  326.  
  327.  
  328. //theonegalen's config starts here
  329. //FAT-T3R Aeroplane Main Wing
  330. @PART[bigwing]:NEEDS[FerramAerospaceResearch]
  331. {
  332.     @module = Part
  333.     @maximum_drag = 0
  334.     @minimum_drag = 0
  335.     @angularDrag = 0
  336.     @dragCoeff = 0
  337.     @deflectionLiftCoeff = 0
  338.     !MODULE[ModuleLiftingSurface] {}
  339.     MODULE
  340.     {
  341.         name = FARWingAerodynamicModel
  342.         MAC = 2.48
  343.         MidChordSweep = -4.16
  344.         b_2 = 11.060831
  345.         TaperRatio = 0.5871914171
  346.     }
  347. }
  348.  
  349. //FATwings
  350. @PART[fatwing0]:NEEDS[FerramAerospaceResearch]
  351. {
  352.     @module = Part
  353.     @maximum_drag = 0
  354.     @minimum_drag = 0
  355.     @angularDrag = 0
  356.     @dragCoeff = 0
  357.     @deflectionLiftCoeff = 0
  358.     !MODULE[ModuleLiftingSurface] {}
  359.     MODULE
  360.     {
  361.         name = FARWingAerodynamicModel
  362.         MAC = 1
  363.         MidChordSweep = 0
  364.         b_2 = 3.5
  365.         TaperRatio = 1
  366.     }
  367. }
  368.  
  369. @PART[fatwing1]:NEEDS[FerramAerospaceResearch]
  370. {
  371.     @module = Part
  372.     @maximum_drag = 0
  373.     @minimum_drag = 0
  374.     @angularDrag = 0
  375.     @dragCoeff = 0
  376.     @deflectionLiftCoeff = 0
  377.     !MODULE[ModuleLiftingSurface] {}
  378.     MODULE
  379.     {
  380.         name = FARWingAerodynamicModel
  381.         MAC = 3.5
  382.         MidChordSweep = 0
  383.         b_2 = 1
  384.         TaperRatio = 1
  385.     }
  386. }
  387.  
  388. @PART[fatwing2]:NEEDS[FerramAerospaceResearch]
  389. {
  390.     @module = Part
  391.     @maximum_drag = 0
  392.     @minimum_drag = 0
  393.     @angularDrag = 0
  394.     @dragCoeff = 0
  395.     @deflectionLiftCoeff = 0
  396.     !MODULE[ModuleLiftingSurface] {}
  397.     MODULE
  398.     {
  399.         name = FARWingAerodynamicModel
  400.         MAC = 0.5
  401.         MidChordSweep = 8
  402.         b_2 = 3.5
  403.         TaperRatio = 1
  404.     }
  405. }
  406.  
  407. @PART[fatwing3]:NEEDS[FerramAerospaceResearch]
  408. {
  409.     @module = Part
  410.     @maximum_drag = 0
  411.     @minimum_drag = 0
  412.     @angularDrag = 0
  413.     @dragCoeff = 0
  414.     @deflectionLiftCoeff = 0
  415.     !MODULE[ModuleLiftingSurface] {}
  416.     MODULE
  417.     {
  418.         name = FARWingAerodynamicModel
  419.         MAC = 1.75
  420.         MidChordSweep = 36.75
  421.         b_2 = 1
  422.         TaperRatio = 0
  423.     }
  424. }
  425.  
  426. @PART[fatwing4]:NEEDS[FerramAerospaceResearch]
  427. {
  428.     @module = Part
  429.     @maximum_drag = 0
  430.     @minimum_drag = 0
  431.     @angularDrag = 0
  432.     @dragCoeff = 0
  433.     @deflectionLiftCoeff = 0
  434.     !MODULE[ModuleLiftingSurface] {}
  435.     MODULE
  436.     {
  437.         name = FARWingAerodynamicModel
  438.         MAC = 3.5
  439.         MidChordSweep = 0
  440.         b_2 = 0.5
  441.         TaperRatio = 1
  442.     }
  443. }
  444.  
  445. @PART[fatwing5]:NEEDS[FerramAerospaceResearch]
  446. {
  447.     @module = Part
  448.     @maximum_drag = 0
  449.     @minimum_drag = 0
  450.     @angularDrag = 0
  451.     @dragCoeff = 0
  452.     @deflectionLiftCoeff = 0
  453.     !MODULE[ModuleLiftingSurface] {}
  454.     MODULE
  455.     {
  456.         name = FARWingAerodynamicModel
  457.         MAC = 1.75
  458.         MidChordSweep = 40
  459.         b_2 = 0.5
  460.         TaperRatio = 0
  461.     }
  462. }
  463.  
  464. @PART[fatwing6]:NEEDS[FerramAerospaceResearch]
  465. {
  466.     @module = Part
  467.     @maximum_drag = 0
  468.     @minimum_drag = 0
  469.     @angularDrag = 0
  470.     @dragCoeff = 0
  471.     @deflectionLiftCoeff = 0
  472.     !MODULE[ModuleLiftingSurface] {}
  473.     MODULE
  474.     {
  475.         name = FARWingAerodynamicModel
  476.         MAC = 0.25
  477.         MidChordSweep = -4.1
  478.         b_2 = 3.5
  479.         TaperRatio = 0
  480.     }
  481. }
  482.  
  483. //Small APP Wings
  484. @PART[smallwingConnector1]:NEEDS[FerramAerospaceResearch]
  485. {
  486.     @module = Part
  487.     @maximum_drag = 0
  488.     @minimum_drag = 0
  489.     @angularDrag = 0
  490.     @dragCoeff = 0
  491.     @deflectionLiftCoeff = 0
  492.     !MODULE[ModuleLiftingSurface] {}
  493.     MODULE
  494.     {
  495.         name = FARWingAerodynamicModel
  496.         MAC = 1.14
  497.         MidChordSweep = 0
  498.         b_2 = 0.96
  499.         TaperRatio = 1
  500.     }
  501. }
  502.  
  503. @PART[smallwingConnector2]:NEEDS[FerramAerospaceResearch]
  504. {
  505.     @module = Part
  506.     @maximum_drag = 0
  507.     @minimum_drag = 0
  508.     @angularDrag = 0
  509.     @dragCoeff = 0
  510.     @deflectionLiftCoeff = 0
  511.     !MODULE[ModuleLiftingSurface] {}
  512.     MODULE
  513.     {
  514.         name = FARWingAerodynamicModel
  515.         MAC = 1.87
  516.         MidChordSweep = 0
  517.         b_2 = 0.67
  518.         TaperRatio = 1
  519.     }
  520. }
  521.  
  522. @PART[smallwingConnector3]:NEEDS[FerramAerospaceResearch]
  523. {
  524.     @module = Part
  525.     @maximum_drag = 0
  526.     @minimum_drag = 0
  527.     @angularDrag = 0
  528.     @dragCoeff = 0
  529.     @deflectionLiftCoeff = 0
  530.     !MODULE[ModuleLiftingSurface] {}
  531.     MODULE
  532.     {
  533.         name = FARWingAerodynamicModel
  534.         MAC = 0.67
  535.         MidChordSweep = 0
  536.         b_2 = 1.87
  537.         TaperRatio = 1
  538.     }
  539. }
  540.  
  541. @PART[smallwingConnector4]:NEEDS[FerramAerospaceResearch]
  542. {
  543.     @module = Part
  544.     @maximum_drag = 0
  545.     @minimum_drag = 0
  546.     @angularDrag = 0
  547.     @dragCoeff = 0
  548.     @deflectionLiftCoeff = 0
  549.     !MODULE[ModuleLiftingSurface] {}
  550.     MODULE
  551.     {
  552.         name = FARWingAerodynamicModel
  553.         MAC = 0.71
  554.         MidChordSweep = -7
  555.         b_2 = 1.87
  556.         TaperRatio = .48
  557.     }
  558. }
  559.  
  560. @PART[smallwingConnector5]:NEEDS[FerramAerospaceResearch]
  561. {
  562.     @module = Part
  563.     @maximum_drag = 0
  564.     @minimum_drag = 0
  565.     @angularDrag = 0
  566.     @dragCoeff = 0
  567.     @deflectionLiftCoeff = 0
  568.     !MODULE[ModuleLiftingSurface] {}
  569.     MODULE
  570.     {
  571.         name = FARWingAerodynamicModel
  572.         MAC = 0.34
  573.         MidChordSweep = 7
  574.         b_2 = 1.87
  575.         TaperRatio = 0
  576.     }
  577. }
  578.  
  579. @PART[smallwingConnector6]:NEEDS[FerramAerospaceResearch]
  580. {
  581.     @module = Part
  582.     @maximum_drag = 0
  583.     @minimum_drag = 0
  584.     @angularDrag = 0
  585.     @dragCoeff = 0
  586.     @deflectionLiftCoeff = 0
  587.     !MODULE[ModuleLiftingSurface] {}
  588.     MODULE
  589.     {
  590.         name = FARWingAerodynamicModel
  591.         MAC = 0.935
  592.         MidChordSweep = 38
  593.         b_2 = 0.68
  594.         TaperRatio = 0
  595.     }
  596. }
  597.  
  598. @PART[smallwingConnectortip]:NEEDS[FerramAerospaceResearch]
  599. {
  600.     @module = Part
  601.     @maximum_drag = 0
  602.     @minimum_drag = 0
  603.     @angularDrag = 0
  604.     @dragCoeff = 0
  605.     @deflectionLiftCoeff = 0
  606.     !MODULE[ModuleLiftingSurface] {}
  607.     MODULE
  608.     {
  609.         name = FARWingAerodynamicModel
  610.         MAC = 0.935
  611.         MidChordSweep = 36.91
  612.         b_2 = 0.58
  613.         TaperRatio = 0.3568965517
  614.     }
  615. }
  616.  
  617. //CONTROL SURFACES
  618.  
  619. //Round-Deluxe Winglet
  620. @PART[roundwinglet]:NEEDS[FerramAerospaceResearch]
  621. {
  622.     @module = Part
  623.     @maximum_drag = 0
  624.     @minimum_drag = 0
  625.     @angularDrag = 0
  626.     @dragCoeff = 0
  627.     @deflectionLiftCoeff = 0
  628.     @ctrlSurfaceRange = 0
  629.     @ctrlSurfaceArea = 0
  630.     !MODULE[ModuleControlSurface] {}
  631.     MODULE
  632.     {
  633.         name = FARControllableSurface
  634.         MAC = 0.98
  635.         MidChordSweep = 11.14
  636.         maxdeflect = 20
  637.         b_2 = 1.36
  638.         TaperRatio = 0.661
  639.         ctrlSurfFrac = 0.45
  640.         transformName = obj_ctrlSrf
  641.     }
  642. }
  643.  
  644. @PART[elevon2b]:NEEDS[FerramAerospaceResearch]
  645. {
  646.     @module = Part
  647.     @maximum_drag = 0
  648.     @minimum_drag = 0
  649.     @angularDrag = 0
  650.     @dragCoeff = 0
  651.     @deflectionLiftCoeff = 0
  652.     @ctrlSurfaceRange = 0
  653.     @ctrlSurfaceArea = 0
  654.     !MODULE[ModuleControlSurface] {}
  655.     MODULE
  656.     {
  657.         name = FARControllableSurface
  658.         MAC = 0.75
  659.         MidChordSweep = 0
  660.         maxdeflect = 20
  661.         b_2 = 1.825
  662.         nonSideAttach = 1
  663.         TaperRatio = 0
  664.         ctrlSurfFrac = 1
  665.         transformName = ctrlSrf
  666.     }
  667. }
  668.  
  669. @PART[hlfSrf]:NEEDS[FerramAerospaceResearch]
  670. {
  671.     @module = Part
  672.     @maximum_drag = 0
  673.     @minimum_drag = 0
  674.     @angularDrag = 0
  675.     @dragCoeff = 0
  676.     @deflectionLiftCoeff = 0
  677.     @ctrlSurfaceRange = 0
  678.     @ctrlSurfaceArea = 0
  679.     !MODULE[ModuleControlSurface] {}
  680.     MODULE
  681.     {
  682.         name = FARControllableSurface
  683.         MAC = 0.525
  684.         MidChordSweep = 0
  685.         maxdeflect = 20
  686.         b_2 = 0.9125
  687.         nonSideAttach = 1
  688.         TaperRatio = 0
  689.         ctrlSurfFrac = 1
  690.         transformName = elevon
  691.     }
  692. }
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