@PART[RSBengineJ2]:FOR[RealFuels_StockEngines] //J-2 Cryogenic Engine
{

  @mass = 1.7881
  @cost = 45000
  %entryCost = 275000
  @maxTemp = 2300


  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 1033.1
    @heatProduction = 150
    @atmosphereCurve
    {
      @key,0 = 0 421
      @key,1 = 1 300
      @key,1 = 12 0.001
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = LqdHydrogen
      ratio = 72.856139
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = LqdOxygen
      ratio = 27.143861
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }

  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 6
    origTechLevel = 6
    engineType = U
    origMass = 1.7881
    configuration = LqdHydrogen+LqdOxygen
    modded = false

    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 1033.1
      heatProduction = 150
      PROPELLANT
      {
        name = LqdHydrogen
        ratio = 72.85613945469638
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 27.143860545303625
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 0.95238
      IspV = 1.2028
      throttle = 0
      ModuleEngineIgnitor
      {
        ignitionsAvailable = 2
        useUllageSimulation = true
        autoIgnitionTemperature = 800
        ignitorType = Electric
        IGNITOR_RESOURCE
        {
          name = ElectricCharge
          amount = 58
        }
      }
    }
  }
  !MODULE[ModuleEngineIgnitor] {}
  ModuleEngineIgnitor
  {
    ignitionsAvailable = 2
    autoIgnitionTemperature = 800
    useUllageSimulation = true

  }
}


@PART[RSBengineRL10B2]:FOR[RealFuels_StockEngines] //RL10B-2 Cryogenic Engine
{

  @MODULE[ModuleEngine*]
  {
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = LqdHydrogen
      ratio = 72.856139
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = LqdOxygen
      ratio = 27.143861
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }

  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 6
    origTechLevel = 6
    engineType = U
    origMass = 0.277
    configuration = LqdHydrogen+LqdOxygen
    modded = false

    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 110
      heatProduction = 150
      PROPELLANT
      {
        name = LqdHydrogen
        ratio = 72.85613945469638
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 27.143860545303625
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 0.95238
      IspV = 1.33
      throttle = 0
      ModuleEngineIgnitor
      {
        ignitionsAvailable = 2
        useUllageSimulation = true
        autoIgnitionTemperature = 800
        ignitorType = Electric
        IGNITOR_RESOURCE
        {
          name = ElectricCharge
          amount = 58
        }
      }
    }
  }
  !MODULE[ModuleEngineIgnitor] {}
  ModuleEngineIgnitor
  {
    ignitionsAvailable = 2
    autoIgnitionTemperature = 800
    useUllageSimulation = true

  }
}

@PART[RSBengineRS25]:FOR[RealFuels_StockEngines] //RS-25 Space Shuttle Main Engine
{

  @MODULE[ModuleEngine*]
  {
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = LqdHydrogen
      ratio = 72.856139
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = LqdOxygen
      ratio = 27.143861
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }

  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 6
    origTechLevel = 6
    engineType = U
    origMass = 3.39
    configuration = LqdHydrogen+LqdOxygen
    modded = false

    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 2279
      heatProduction = 192
      PROPELLANT
      {
        name = LqdHydrogen
        ratio = 72.85613945469638
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 27.143860545303625
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.74285
      IspV = 1.292285
      throttle = 0
      ModuleEngineIgnitor
      {
        ignitionsAvailable = 1
        useUllageSimulation = true
        autoIgnitionTemperature = 800
        ignitorType = Electric
        IGNITOR_RESOURCE
        {
          name = ElectricCharge
          amount = 58
        }
      }
    }
  }
  !MODULE[ModuleEngineIgnitor] {}
  ModuleEngineIgnitor
  {
    ignitionsAvailable = 1
    autoIgnitionTemperature = 800
    useUllageSimulation = true

  }
}