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Stockalike RF Engine Configs v3.2.6 [01/20/19][RF v12]


Raptor831
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Hello 

I come again because I'm not able to make RF stockalike work for all Tantares and Tantares LV parts. (It work fine with stock and BDB)

I'm bad at programming  and don't understand what's the matter...

I post here my logs. If someone have some time to take a look it's nice :)

https://www.dropbox.com/s/r19quhf21putru0/MMPatch.log?dl=0

https://www.dropbox.com/s/k8a58dirirxapjw/ModuleManager.log?dl=0

https://www.dropbox.com/s/nwn92ti9pjjd2e4/output_log.txt?dl=0

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There might be a little error in fix-part-categories.cfg. MM is pointing to the L at the end of third line from below.

// The game auto-sorts parts with category "Propulsion" into "Engine" if they
//  have one of the stock engine modules; otherwise "FuelTank".
// Because the auto-sort doesn't recognize ModuleEnginesRF as an engine module,
//  we need ModuleManager to do the sort for us.

@PART[*]:HAS[#category[Propulsion],@MODULE[ModuleEnginesRF]]:FOR[z_RealFuels_StockEngines] {
    @category = Engine
}

@PART[*]:HAS[#category[0],@MODULE[ModuleEnginesRF]]:FOR[z_RealFuels_StockEngines]L {
    @category = Engine
}

Do you agree?

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  • 3 weeks later...

My take on TRAIL engines, SRBs and RCS'.

@PART[trails_LR87_mod2]:FOR[RealFuels_StockEngines] //Blank Engine
{

  @mass = 0.67
  @cost = 1464
  %entryCost = 7320
  @maxTemp = 2244
  
  
  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 545
    @heatProduction = 174
    @atmosphereCurve
    {
      @key,0 = 0 320
      @key,1 = 1 288
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Kerosene
      ratio = 42.146868
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = LqdOxygen
      ratio = 57.853132
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }
  
  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 4
    origTechLevel = 4
    engineType = L
    origMass = 0.67
    configuration = Kerosene+LqdOxygen
    modded = false

    CONFIG
    {
      name = Kerosene+LqdOxygen
      maxThrust = 545
      heatProduction = 174
      PROPELLANT
      {
        name = Kerosene
        ratio = 42.14686761229314
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 57.85313238770686
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.0000
      IspV = 1.0000
      throttle = 0
      ignitions = 1
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 5.45
      }
      
      
    }
    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 545
      heatProduction = 174
      PROPELLANT
      {
        name = Aerozine50
        ratio = 45.497332914967046
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = NTO
        ratio = 54.502667085032954
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 0.9600
      IspV = 0.9500
      throttle = 0
      ignitions = 2
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 5.45
      }
      
      
    }
    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 409
      heatProduction = 174
      PROPELLANT
      {
        name = LqdHydrogen
        ratio = 76.30830964721619
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 23.69169035278381
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.3000
      IspV = 1.2700
      throttle = 0
      ignitions = 1
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 5.45
      }
      
      
    }
  }
  ignitions = 1
  ullage = true
  pressureFed = false
  IGNITOR_RESOURCE
  {
    name = ElectricCharge
    amount = 5.45
  }

  
}

@PART[trails_LR91_mod2]:FOR[RealFuels_StockEngines] //Blank Engine
{

  @mass = 0.285
  @cost = 534
  %entryCost = 2670
  @maxTemp = 1940
  
  
  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 180
    @heatProduction = 137
    @atmosphereCurve
    {
      @key,0 = 0 340
      @key,1 = 1 204
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Kerosene
      ratio = 42.146868
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = LqdOxygen
      ratio = 57.853132
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }
  
  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 4
    origTechLevel = 4
    engineType = U
    origMass = 0.285
    configuration = Kerosene+LqdOxygen
    modded = false

    CONFIG
    {
      name = Kerosene+LqdOxygen
      maxThrust = 180
      heatProduction = 137
      PROPELLANT
      {
        name = Kerosene
        ratio = 42.14686761229314
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 57.85313238770686
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.0000
      IspV = 1.0000
      throttle = 0
      ignitions = 1
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 1.8
      }
      
      
    }
    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 180
      heatProduction = 137
      PROPELLANT
      {
        name = Aerozine50
        ratio = 49.555707450444295
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = NTO
        ratio = 50.444292549555705
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 0.9600
      IspV = 0.9500
      throttle = 0
      ignitions = 4
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 1.8
      }
      
      
    }
  }
  ignitions = 1
  ullage = true
  pressureFed = false
  IGNITOR_RESOURCE
  {
    name = ElectricCharge
    amount = 1.8
  }

  
}

@PART[trails_Titan_TranstageEngine]:FOR[RealFuels_StockEngines] //Blank Engine
{

  @mass = 0.108
  @cost = 156
  %entryCost = 780
  @maxTemp = 1523
  
  
  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 36
    @heatProduction = 95
    @atmosphereCurve
    {
      @key,0 = 0 330
      @key,1 = 1 116
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Aerozine50
      ratio = 50.329747
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = NTO
      ratio = 49.670253
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }
  
  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 4
    origTechLevel = 4
    engineType = O
    origMass = 0.108
    configuration = Aerozine50+NTO
    modded = false

    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 36
      heatProduction = 95
      PROPELLANT
      {
        name = Aerozine50
        ratio = 50.32974661575842
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = NTO
        ratio = 49.67025338424158
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 0.9600
      IspV = 0.9500
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = MMH+NTO
      maxThrust = 36
      heatProduction = 95
      PROPELLANT
      {
        name = MMH
        ratio = 48.782128919391745
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = NTO
        ratio = 51.217871080608255
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 0.9600
      IspV = 0.9500
      throttle = 0
      
      
      
    }
  }
  

  
}

@PART[trails_Titan_SRB5seg]:FOR[RealFuels_StockEngines] //Blank Engine
{

  @mass = 1.2
  @cost = 1189
  %entryCost = 5945
  @maxTemp = 1800
  
  
  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 1311
    @heatProduction = 249
    @atmosphereCurve
    {
      @key,0 = 0 268
      @key,1 = 1 245
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = SolidFuel
      ratio = 100.000000
      DrawGauge = True
      
    }
    
  }
  
  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 4
    origTechLevel = 4
    engineType = S
    origMass = 1.2
    configuration = SolidFuelDecreasing
    modded = false

    CONFIG
    {
      name = SolidFuelDecreasing
      maxThrust = 1311
      heatProduction = 249
      PROPELLANT
      {
        name = SolidFuel
        ratio = 100
        DrawGauge = True
        
      }
      IspSL = 1.0000
      IspV = 1.0000
      throttle = 0
      ignitions = 1
      ullage = false
      pressureFed = false
      
      curveResource = SolidFuel
      thrustCurve
      {
        key = 0.00000 0.01000 0 0
        key = 0.00057 0.01000 0 0
        key = 0.00905 0.15000
        key = 0.02658 0.31000
        key = 0.04581 0.34000
        key = 0.06674 0.37000
        key = 0.08937 0.40000
        key = 0.11369 0.43000
        key = 0.13971 0.46000
        key = 0.16742 0.49000
        key = 0.19683 0.52000
        key = 0.22794 0.55000
        key = 0.26075 0.58000
        key = 0.29525 0.61000
        key = 0.33145 0.64000
        key = 0.36934 0.67000
        key = 0.40894 0.70000
        key = 0.45023 0.73000
        key = 0.49321 0.76000
        key = 0.53790 0.79000
        key = 0.58428 0.82000
        key = 0.63235 0.85000
        key = 0.68213 0.88000
        key = 0.73360 0.91000
        key = 0.78676 0.94000
        key = 0.84163 0.97000
        key = 0.89819 1.00000 0 0
        key = 0.95475 1.00000 0 0
        key = 1.00000 0.80000
      }
      
    }
  }
  ignitions = 1
  ullage = false
  pressureFed = false
  

  
}

@PART[Janus_RCS_A]:FOR[RealFuels_StockEngines] //Blank Engine
{

  @mass = 0.125
  @cost = 91
  %entryCost = 455
  
  
  
  @MODULE[ModuleRCS*]
  {
    @name = ModuleRCS
    @thrusterPower = 0.3
    @heatProduction = 13
    @atmosphereCurve
    {
      @key,0 = 0 300
      @key,1 = 1 109
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Hydrazine
      ratio = 100.000000
      DrawGauge = True
      %resourceFlowMode = STAGE_PRIORITY_FLOW
    }
    
  }
  
  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleRCS
    techLevel = 2
    origTechLevel = 2
    engineType = L
    origMass = 0.125
    configuration = Hydrazine
    modded = false

    CONFIG
    {
      name = Hydrazine
      thrusterPower = 0.3
      heatProduction = 13
      PROPELLANT
      {
        name = Hydrazine
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.2740
      IspV = 0.7200
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = HTP
      thrusterPower = 0.27
      heatProduction = 13
      PROPELLANT
      {
        name = HTP
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.1770
      IspV = 0.4650
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = MMH+NTO
      thrusterPower = 0.3
      heatProduction = 13
      PROPELLANT
      {
        name = MMH
        ratio = 50.73477956613017
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      PROPELLANT
      {
        name = NTO
        ratio = 49.26522043386983
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.9600
      IspV = 0.9500
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = Nitrogen
      thrusterPower = 0.081
      heatProduction = 13
      PROPELLANT
      {
        name = Nitrogen
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.1001
      IspV = 0.1950
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = NitrousOxide
      thrusterPower = 0.285
      heatProduction = 13
      PROPELLANT
      {
        name = NitrousOxide
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.2000
      IspV = 0.5250
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = UDMH+NTO
      thrusterPower = 0.3
      heatProduction = 13
      PROPELLANT
      {
        name = UDMH
        ratio = 47.82321899736148
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      PROPELLANT
      {
        name = NTO
        ratio = 52.17678100263852
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.9500
      IspV = 0.9500
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = Aerozine50+NTO
      thrusterPower = 0.3
      heatProduction = 13
      PROPELLANT
      {
        name = Aerozine50
        ratio = 48.65771812080538
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      PROPELLANT
      {
        name = NTO
        ratio = 51.34228187919462
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.9600
      IspV = 0.9500
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = Helium
      thrusterPower = 0.004
      heatProduction = 13
      PROPELLANT
      {
        name = Helium
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.2030
      IspV = 0.4530
      throttle = 0
      
      
      
    }
  }
  

  
}

@PART[Janus_RCS_B]:FOR[RealFuels_StockEngines] //Blank Engine
{

  @mass = 0.035
  @cost = 90
  %entryCost = 450
  
  
  
  @MODULE[ModuleRCS*]
  {
    @name = ModuleRCS
    @thrusterPower = 1
    @heatProduction = 43
    @atmosphereCurve
    {
      @key,0 = 0 325
      @key,1 = 1 118
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Hydrazine
      ratio = 100.000000
      DrawGauge = True
      %resourceFlowMode = STAGE_PRIORITY_FLOW
    }
    
  }
  
  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleRCS
    techLevel = 4
    origTechLevel = 4
    engineType = L
    origMass = 0.035
    configuration = Hydrazine
    modded = false

    CONFIG
    {
      name = Hydrazine
      thrusterPower = 1
      heatProduction = 43
      PROPELLANT
      {
        name = Hydrazine
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.2740
      IspV = 0.7200
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = HTP
      thrusterPower = 0.9
      heatProduction = 43
      PROPELLANT
      {
        name = HTP
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.1770
      IspV = 0.4650
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = MMH+NTO
      thrusterPower = 1
      heatProduction = 43
      PROPELLANT
      {
        name = MMH
        ratio = 50.73477956613017
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      PROPELLANT
      {
        name = NTO
        ratio = 49.26522043386983
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.9600
      IspV = 0.9500
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = Nitrogen
      thrusterPower = 0.27
      heatProduction = 43
      PROPELLANT
      {
        name = Nitrogen
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.1001
      IspV = 0.1950
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = NitrousOxide
      thrusterPower = 0.95
      heatProduction = 43
      PROPELLANT
      {
        name = NitrousOxide
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.2000
      IspV = 0.5250
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = UDMH+NTO
      thrusterPower = 1
      heatProduction = 43
      PROPELLANT
      {
        name = UDMH
        ratio = 47.82321899736148
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      PROPELLANT
      {
        name = NTO
        ratio = 52.17678100263852
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.9500
      IspV = 0.9500
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = Aerozine50+NTO
      thrusterPower = 1
      heatProduction = 43
      PROPELLANT
      {
        name = Aerozine50
        ratio = 48.65771812080538
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      PROPELLANT
      {
        name = NTO
        ratio = 51.34228187919462
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.9600
      IspV = 0.9500
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = Helium
      thrusterPower = 0.013
      heatProduction = 43
      PROPELLANT
      {
        name = Helium
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.2030
      IspV = 0.4530
      throttle = 0
      
      
      
    }
  }


}

@PART[Janus_Service_A]:FOR[RealFuels_StockEngines] //Blank Engine
{

  @MODULE[ModuleRCS*]
  {
    @name = ModuleRCS
    @thrusterPower = 1
    @heatProduction = 43
    @atmosphereCurve
    {
      @key,0 = 0 325
      @key,1 = 1 118
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Hydrazine
      ratio = 100.000000
      DrawGauge = True
      %resourceFlowMode = STAGE_PRIORITY_FLOW
    }
    
  }
  
  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleRCS
    techLevel = 4
    origTechLevel = 4
    engineType = L
    origMass = 0.035
    configuration = Hydrazine
    modded = false

    CONFIG
    {
      name = Hydrazine
      thrusterPower = 1
      heatProduction = 43
      PROPELLANT
      {
        name = Hydrazine
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.2740
      IspV = 0.7200
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = HTP
      thrusterPower = 0.9
      heatProduction = 43
      PROPELLANT
      {
        name = HTP
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.1770
      IspV = 0.4650
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = MMH+NTO
      thrusterPower = 1
      heatProduction = 43
      PROPELLANT
      {
        name = MMH
        ratio = 50.73477956613017
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      PROPELLANT
      {
        name = NTO
        ratio = 49.26522043386983
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.9600
      IspV = 0.9500
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = Nitrogen
      thrusterPower = 0.27
      heatProduction = 43
      PROPELLANT
      {
        name = Nitrogen
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.1001
      IspV = 0.1950
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = NitrousOxide
      thrusterPower = 0.95
      heatProduction = 43
      PROPELLANT
      {
        name = NitrousOxide
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.2000
      IspV = 0.5250
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = UDMH+NTO
      thrusterPower = 1
      heatProduction = 43
      PROPELLANT
      {
        name = UDMH
        ratio = 47.82321899736148
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      PROPELLANT
      {
        name = NTO
        ratio = 52.17678100263852
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.9500
      IspV = 0.9500
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = Aerozine50+NTO
      thrusterPower = 1
      heatProduction = 43
      PROPELLANT
      {
        name = Aerozine50
        ratio = 48.65771812080538
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      PROPELLANT
      {
        name = NTO
        ratio = 51.34228187919462
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.9600
      IspV = 0.9500
      throttle = 0
      
      
      
    }
    CONFIG
    {
      name = Helium
      thrusterPower = 0.013
      heatProduction = 43
      PROPELLANT
      {
        name = Helium
        ratio = 100
        DrawGauge = True
        %resourceFlowMode = STAGE_PRIORITY_FLOW
      }
      IspSL = 0.2030
      IspV = 0.4530
      throttle = 0
      
      
      
    }
  }
  

  
}

As all engines are modeled after Titan rocket family engines, I made configs that resemble the originals.

JLV-675 "Pallas" - modeled after LR87 main engine. I configured it to use LOX/RP1 with 1 ignition, NTO/A50 with 2 ignitions and LOX/LOH with 1 ignition. 

JLV-250 "Lelantos" - modeled after LR91 upper stage engine.  I configured it to use LOX/RP1 with 1 ignition, NTO/A50 with 4 ignitions.

JLV-T-51 "Metis" - modeled after AJ10 orbital engine. Only 36 kN of thrust despite being 1.875 m and double nozzled, but I left it like this. Comes with an integrated 700 l tank. I configured it as either NTO/A50 or NTO/MMH pressure fed engine with unlimited ignitions and no ullage (allows for a bit of cheating but low thrust will make it useless on a ship with huge tanks filled with fuel anyway). 

RCS' can use a typical selection of monopropellants and hypergols. 

Edited by JebIsDeadBaby
Added config for Service Module RCS
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  • 4 months later...
  • 2 weeks later...
On 4/4/2020 at 4:07 PM, New Horizons said:

Is there a continuation of this work? Some engines do not have a plume while using this.

Check my answer on the previous page, some engines got newer models a while back with the 1.7 release and the plume was lost, I made an updated config file. Might still not work with the new part models they included with the 1.9 update though.

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  • 3 weeks later...

Is there a way to make Real Fuels work nicely with parts that use B9 Part Switcher to add/remove tanks?

Specifically, I'm looking at the LV-601-4 Orbital Maneuvering Engine Cluster from Near Future Spacecraft, which originally runs on MonoProp, and has variants with or without inbuilt MonoProp tanks.

(The probe tanks from Near Future Exploration present with a related problem, as they use variants with different fuels, but since this just switches content it seems to be reasonably easy to work around, by just letting Real Fuels do the switching and degrade the variants to mere optics.)

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  • 2 weeks later...
1 hour ago, FabioofSpace said:

have a question. Why is this mod making Hydrolox cheaper than Hypergolics? Is there any reasons for that?

You mean like price per unit? I’m not aware that RFStockalike changes any prices on fuels. 

For me it makes sense that LqdHydrogen is far cheaper, it’s easier to get and/or produce than these dangerous nasty self igniting chemicals.

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On 5/19/2020 at 11:31 PM, FabioofSpace said:

I have a question. Why is this mod making Hydrolox cheaper than Hypergolics? Is there any reasons for that?

 

On 5/20/2020 at 1:35 AM, ValiZockt said:

You mean like price per unit? I’m not aware that RFStockalike changes any prices on fuels. 

For me it makes sense that LqdHydrogen is far cheaper, it’s easier to get and/or produce than these dangerous nasty self igniting chemicals.

Liquid hydrogen is not cheaper. It must be refrigerated down to cryogenic temperatures (20K)

prices come from the CRP mod and have been through strenuous vetting by the RO community using 1960s  prices and inflation values  

 

 

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  • 3 months later...

Hi Everyone,

                    I have a question; does anyone know how to (globally) edit the engine dry mass in this mod?

I'm playing with RF-stock in RSS, and I really need to have low engine masses, this mod doesn't touch the engines' masses-because they remain their stock values.

So, I downloaded SMURFF to solve this problem, but apparently it doesn't work alongside RealFuels-Stock.

How do I edit the engines masses so to make them to closer to reality? I don't want to play with RO (it's great but too hard for me), but to really enjoy a RSS playthrough, I need low part masses.Any help would be appreciated.

BTW, I really love the mod, it's the perfect blend of realism and playability.(IMO)

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