@PART[km_ssme_rs25s]:FOR[RealFuels_StockEngines] //RX-25s
{

  @mass = 1.66
  @cost = 2724
  %entryCost = 8620
  @maxTemp = 3275

  !mesh = DELETE
	MODEL
	{
		model = Klockheed_Martian_SSE/Parts/Ssme-s/model
		scale = 1.68, 1.68, 1.68
		rotation = 0, 0, 0
	}
	%scale = 1.0
	%rescaleFactor = 1.0



  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 675
    @heatProduction = 171
    @atmosphereCurve
    {
      @key,0 = 0 434
      @key,1 = 1 365
    }
    !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 = L+
    origMass = 1.66
    configuration = LqdHydrogen+LqdOxygen
    modded = false

    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 675
      heatProduction = 171
      PROPELLANT
      {
        name = LqdHydrogen
        ratio = 72.85613945469638
        DrawGauge = True
        %ResourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 27.143860545303625
        %ResourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.3000
      IspV = 1.2700
      throttle = 0
      ModuleEngineIgnitor
      {
        ignitionsAvailable = 1
        autoIgnitionTemperature = 800
        ignitorType = Electric
        useUllageSimulation = true
        IGNITOR_RESOURCE
        {
          name = ElectricCharge
          amount = 5
        }
      }


    }
    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 875
      heatProduction = 171
      PROPELLANT
      {
        name = Aerozine50
        ratio = 50.17301038062284
        DrawGauge = True
        %ResourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = NTO
        ratio = 49.82698961937716
        %ResourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 0.9600
      IspV = 0.9500
      throttle = 0
      ModuleEngineIgnitor
      {
        ignitionsAvailable = 2
        autoIgnitionTemperature = 800
        ignitorType = Electric
        useUllageSimulation = true
        IGNITOR_RESOURCE
        {
          name = ElectricCharge
          amount = 5
        }
      }


    }
    CONFIG
    {
      name = Kerosene+LqdOxygen
      maxThrust = 875
      heatProduction = 171
      PROPELLANT
      {
        name = Kerosene
        ratio = 36.699903505950466
        DrawGauge = True
        %ResourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 63.300096494049534
        %ResourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.0000
      IspV = 1.0000
      throttle = 0
      ModuleEngineIgnitor
      {
        ignitionsAvailable = 1
        autoIgnitionTemperature = 800
        ignitorType = Electric
        useUllageSimulation = true
        IGNITOR_RESOURCE
        {
          name = ElectricCharge
          amount = 5
        }
      }


    }
  }
  !MODULE[ModuleEngineIgnitor] {}
  ModuleEngineIgnitor
  {
    ignitionsAvailable = 1
    autoIgnitionTemperature = 800
    ignitorType = Electric
    useUllageSimulation = true
    IGNITOR_RESOURCE
    {
      name = ElectricCharge
      amount = 5
    }
  }


}
@PART[km_ssme_rs25ss]:FOR[RealFuels_StockEngines] //RX-25ss Straight
{

  @mass = 1.525
  @cost = 2394
  %entryCost = 6970
  @maxTemp = 3279

  !mesh = DELETE
	MODEL
	{
		model = Klockheed_Martian_SSE/Parts/Ssme-s-Straight/model
		scale = 1.94, 1.94, 1.94
		rotation = 0, 0, 0
	}
	%scale = 1.0
	%rescaleFactor = 1.0

  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 675
    @heatProduction = 172
    @atmosphereCurve
    {
      @key,0 = 0 434
      @key,1 = 1 365
    }
    !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 = L+
    origMass = 1.525
    configuration = LqdHydrogen+LqdOxygen
    modded = false

    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 675
      heatProduction = 172
      PROPELLANT
      {
        name = LqdHydrogen
        ratio = 72.85613945469638
        DrawGauge = True
        %ResourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 27.143860545303625
        %ResourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.3000
      IspV = 1.2700
      throttle = 0
      ModuleEngineIgnitor
      {
        ignitionsAvailable = 1
        autoIgnitionTemperature = 800
        ignitorType = Electric
        useUllageSimulation = true
        IGNITOR_RESOURCE
        {
          name = ElectricCharge
          amount = 4
        }
      }


    }
    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 875
      heatProduction = 172
      PROPELLANT
      {
        name = Aerozine50
        ratio = 50.17301038062284
        DrawGauge = True
        %ResourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = NTO
        ratio = 49.82698961937716
        %ResourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 0.9600
      IspV = 0.9500
      throttle = 0
      ModuleEngineIgnitor
      {
        ignitionsAvailable = 2
        autoIgnitionTemperature = 800
        ignitorType = Electric
        useUllageSimulation = true
        IGNITOR_RESOURCE
        {
          name = ElectricCharge
          amount = 4
        }
      }


    }
    CONFIG
    {
      name = Kerosene+LqdOxygen
      maxThrust = 875
      heatProduction = 172
      PROPELLANT
      {
        name = Kerosene
        ratio = 36.699903505950466
        DrawGauge = True
        %ResourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 63.300096494049534
        %ResourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.0000
      IspV = 1.0000
      throttle = 0
      ModuleEngineIgnitor
      {
        ignitionsAvailable = 1
        autoIgnitionTemperature = 800
        ignitorType = Electric
        useUllageSimulation = true
        IGNITOR_RESOURCE
        {
          name = ElectricCharge
          amount = 4
        }
      }


    }
  }
  !MODULE[ModuleEngineIgnitor] {}
  ModuleEngineIgnitor
  {
    ignitionsAvailable = 1
    autoIgnitionTemperature = 800
    ignitorType = Electric
    useUllageSimulation = true
    IGNITOR_RESOURCE
    {
      name = ElectricCharge
      amount = 4
    }
  }


}