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[1.8+] Real Fuels

NathanKell

By NathanKell
in KSP1 Mod Releases

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Commissar

Commissar

Posted
Posted
Just now, SpacedInvader said:

5% throttle yes, but I could swear I remember reading somewhere along the line that the engine configs for most first stage engines don't allow them to go below about 30% thrust.

irl, yes, but pretty sure you just can't cut it off completely in ksp with RF

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Starwaster

Starwaster

Posted
Posted
1 hour ago, SpacedInvader said:

The issue is that most KSP gravity turns (for me at least) end before the top of the atmosphere so after MECO, apoapse begins to decay. MJ working the way it does, it then immediately fires up the engine again assuming its got infinite relights to bump it back up to the target altitude and then 3 seconds later you've gone through 20 relights without having a second to react. Throttling probably does come into play, but to a lesser degree because I've almost never seen MJ try to reduce throttle to the point that the engines cut out before the target apoapse is reached. Ideally, MJ should have the ability to prevent engine shutdown before a certain altitude and then to either recalculate the throttle needed to arrive at MECO after leaving the atmosphere, or alternatively allow a setting for target periapse in the launch window so that once apoapse is reached, the rocket would be pitched to raise the periapse which would likely complete after departing the atmosphere. In lieu of those settings, I've been using the Gravity Turn mod which allows you to set up a proper ascent to orbit without a huge amount of coasting, though I still have removed limited relights on ascent engines specifically because MJ will still end up needing 3-5 relights somehow.

EDIT: And before you say it, I've tried many many times to build a rocket / ascent profile that doesn't have some amount of coasting through the atmosphere after MECO and I've just never been able to do it.

I almost always am using PEG so never happens for me; it keeps on with more or less constant thrust until orbit is established (scaled up Kerbin; PEG may not work so well on stock Kerbin with typical stock engine setups)

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Starwaster

Starwaster

Posted
Posted (edited)
12 minutes ago, SpacedInvader said:

PEG?

Powered Explicit Guidance.  (so PEG Guidance is redundant)

It's a guidance program that steers the rocket into orbit taking into account thrust levels and delta-V of all stages. It'll keep firing the engines at constant thrust and throttle (unless there are throttle limits such as for Q or max acceleration and minimum throttle %)

It typically kicks in after a specified pitch program (configured in the PEG ascent window) of X deg/sec over Y seconds, etc etc

Saturn used something similar called Iterative Guidance Mode (IGM)

It could even compensate for engine out situations though that's not typically something KSP players have to worry about

Edited by Starwaster
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SpacedInvader

SpacedInvader

Posted
Posted
8 minutes ago, Starwaster said:

Powered Explicit Guidance.  (so PEG Guidance is redundant)

It's a guidance program that steers the rocket into orbit taking into account thrust levels and delta-V of all stages. It'll keep firing the engines at constant thrust and throttle (unless there are throttle limits such as for Q or max acceleration and minimum throttle %)

It typically kicks in after a specified pitch program (configured in the PEG ascent window) of X deg/sec over Y seconds, etc etc)

Saturn used something similar called Iterative Guidance Mode (IGM)

It could even compensate for engine out situations though that's not typically something KSP players have to worry about

Huh... that sounds like a mod I must add to the pile...

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Starwaster

Starwaster

Posted
Posted
Just now, SpacedInvader said:

Ahh, well then that is a new feature since the last time I used MechJeb (probably a year now). I like it.

If you're using stock Kerbin then I'm not sure how PEG would work there. In theory it should but it would likely depend on the initial pitch program... I usually configure to start PEG between 60-135 seconds after launch and it wants to do shallow ascent, that being more efficient. In a stock environment that would mean going shallow at high speeds and low altitudes which means a lot of atmospheric heating. But you could give it a long pitch program and have it kick in during the upper atmosphere....

(none of that should matter for airless moons; it'll just fly shallow the whole way. Just make sure your initial pitch program is enough to clear any hills)

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SpacedInvader

SpacedInvader

Posted
Posted
Just now, Starwaster said:

If you're using stock Kerbin then I'm not sure how PEG would work there. In theory it should but it would likely depend on the initial pitch program... I usually configure to start PEG between 60-135 seconds after launch and it wants to do shallow ascent, that being more efficient. In a stock environment that would mean going shallow at high speeds and low altitudes which means a lot of atmospheric heating. But you could give it a long pitch program and have it kick in during the upper atmosphere....

(none of that should matter for airless moons; it'll just fly shallow the whole way. Just make sure your initial pitch program is enough to clear any hills)

Atmospheric heating is essentially the only reason I use the ascent program. On airless bodies I've usually flown either by-wire (entering pitch / roll / yaw commands into MJ) until I get the desired apoapse or I get off the ground in that manner and then use the adjust orbit programs to get the same effect. It didn't even occur to me before today that you could use the ascent program away from an atmospheric world.

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  • 1 month later...
Starwaster

Starwaster

Posted
Posted

Official updates have been released for both KSP 1.4.5 and KSP 1.5.1

This update contains new analytic improvements for tank temperature for cryogenics. Temperature will increase much more realistically during timewarp > 100 (that is, from 1000 on up)

The same issue that made analytic temp increases so slow would likely have made cooldown (whether from boiloff or external sources) also happen more slowly so that has been fixed as well and code to ensure that cooldown happens when it should happen has been put in as well. 

As soon as CKAN indexes the 1.5.1 update we'll be pushing one out for 1.6.0 as well.

For KSP 1.4.5 - https://github.com/NathanKell/ModularFuelSystem/releases/tag/rf-v12.7.2

For KSP 1.5.1 - https://github.com/NathanKell/ModularFuelSystem/releases/tag/rf-v12.7.3

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Wallygator

Wallygator

Posted
Posted

OK, so I'm slightly confused...

Considering RO is now ported to 1.4.5, is there a link for RF that is also 1.4.5?

There are so many various threads against a number of KSP versions, that frankly confuses me.

Does anyone have a link to a (KSP 1.4.5) version of RF?  

Apologies for not reading through 160 pages of posts. ;)

 

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Phineas Freak

Phineas Freak

Posted
Posted
2 hours ago, Wallygator said:

OK, so I'm slightly confused...

Considering RO is now ported to 1.4.5, is there a link for RF that is also 1.4.5?

There are so many various threads against a number of KSP versions, that frankly confuses me.

Does anyone have a link to a (KSP 1.4.5) version of RF?  

Apologies for not reading through 160 pages of posts. ;)

Approximately 4 posts above:

On 1/8/2019 at 5:52 PM, Starwaster said:

For KSP 1.4.5 - https://github.com/NathanKell/ModularFuelSystem/releases/tag/rf-v12.7.2

 

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Starwaster

Starwaster

Posted
Posted

Real Fuels for KSP 1.6.1 is in pre-release

It won't be released for CKAN indexing as Community Resource Pack hasn't been updated and I still want to use this opportunity to clear some of the outstanding issues that have been sitting around for a couple of years. 

https://github.com/NathanKell/ModularFuelSystem/releases/tag/rf-v12.7.4

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blowfish

blowfish

Posted
Posted (edited)
1 minute ago, Iso-Polaris said:

I can't find RF configs for engines from Making history expansion and latest 1.6 update , ANYWHERE. That's really annoying

Everything is community maintained.  Unlike Making History itself, no one is getting paid for this.  If you want to add it, make it yourself!

Edited by blowfish
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Iso-Polaris

Iso-Polaris

Posted
Posted
2 minutes ago, blowfish said:

Everything is community maintained.  Unlike Making History itself, no one is getting paid for this.  If you want to add it, make it yourself!

I know how to write a config. I just wonder if stockalike RF config has been abandoned.

If so, I would very much like to take over.

However I have no idea how does the liscence work and how to upload it.

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Iso-Polaris

Iso-Polaris

Posted
Posted

I've made the config for making histroy and 1.6 liquid engines myself. Can you integrate it somehow?? 

 @PART[liquidEngine3_v2]:FOR[RealFuels_StockEngines] //LV-909
{

  @mass = 0.2
  @cost = 146
  %entryCost = 730
  @maxTemp = 1450


  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 50
    @heatProduction = 88
    @atmosphereCurve
    {
      @key,0 = 0 298
      @key,1 = 1 106
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Aerozine50
      ratio = 50.173010
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = NTO
      ratio = 49.826990
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }

  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 1
    origTechLevel = 1
    engineType = O
    origMass = 0.2
    configuration = Aerozine50+NTO
    modded = false

    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 50
      heatProduction = 88
      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
      ignitions = 24
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 0.5
      }


    }
    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 38
      heatProduction = 88
      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 = 24
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 0.5
      }


    }
  }
  ignitions = 24
  ullage = true
  pressureFed = false
  IGNITOR_RESOURCE
  {
    name = ElectricCharge
    amount = 0.5
  }


}

 @PART[liquidEngineMini_v2]:FOR[RealFuels_StockEngines] //48-7S
{

  @mass = 0.045
  @cost = 145
  %entryCost = 725
  @maxTemp = 2082


  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 30
    @heatProduction = 166
    @atmosphereCurve
    {
      @key,0 = 0 319
      @key,1 = 1 262
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Kerosene
      ratio = 37.694087
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = LqdOxygen
      ratio = 62.305913
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }

  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 3
    origTechLevel = 3
    engineType = L+
    origMass = 0.045
    configuration = Kerosene+LqdOxygen
    modded = false

    CONFIG
    {
      name = Kerosene+LqdOxygen
      maxThrust = 30
      heatProduction = 166
      PROPELLANT
      {
        name = Kerosene
        ratio = 37.69408655434424
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 62.30591344565576
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.0000
      IspV = 1.0000
      throttle = 0
      ignitions = 2
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 0.3
      }


    }
    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 30
      heatProduction = 166
      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
      ignitions = 4
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 0.3
      }


    }
    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 23
      heatProduction = 166
      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 = 2
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 0.3
      }


    }
  }
  ignitions = 2
  ullage = true
  pressureFed = false
  IGNITOR_RESOURCE
  {
    name = ElectricCharge
    amount = 0.3
  }


}

@PART[liquidEngine2-2_v2]:FOR[RealFuels_StockEngines] //Poodle
{

  @mass = 0.67
  @cost = 573
  %entryCost = 2865
  @maxTemp = 1516


  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 220
    @heatProduction = 94
    @atmosphereCurve
    {
      @key,0 = 0 330
      @key,1 = 1 116
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Aerozine50
      ratio = 50.173010
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = NTO
      ratio = 49.826990
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }

  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 4
    origTechLevel = 4
    engineType = O
    origMass = 0.67
    configuration = Aerozine50+NTO
    modded = false

    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 220
      heatProduction = 94
      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
      ignitions = 24
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 2.2
      }


    }
    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 165
      heatProduction = 94
      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 = 24
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 2.2
      }


    }
  }
  ignitions = 24
  ullage = true
  pressureFed = false
  IGNITOR_RESOURCE
  {
    name = ElectricCharge
    amount = 2.2
  }

}

@PART[LiquidEngineLV-TX87]:FOR[RealFuels_StockEngines]
{

  @mass = 0.66
  @cost = 800
  %entryCost = 5120
  @maxTemp = 2266


  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 400
    @heatProduction = 150
    @atmosphereCurve
    {
      @key,0 = 0 322
      @key,1 = 1 281
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Kerosene
      ratio = 37.694087
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = LqdOxygen
      ratio = 62.305913
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }

  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 6
    origTechLevel = 6
    engineType = L+
    origMass = 0.66
    configuration = Kerosene+LqdOxygen
    modded = false

    CONFIG
    {
      name = Kerosene+LqdOxygen
      maxThrust = 400
      heatProduction = 150
      PROPELLANT
      {
        name = Kerosene
        ratio = 37.69408655434424
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 62.30591344565576
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.0000
      IspV = 0.9415
      throttle = 0
      ignitions = 1
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 8
      }


    }
    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 400
      heatProduction = 150
      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 = 0.8944
      throttle = 0
      ignitions = 2
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 8
      }


    }
    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 300
      heatProduction = 150
      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 = 1.1957
      throttle = 0
      ignitions = 1
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 8
      }


    }
  }
  ignitions = 1
  ullage = true
  pressureFed = false
  IGNITOR_RESOURCE
  {
    name = ElectricCharge
    amount = 8
  }


}

@PART[LiquidEngineKE-1]:FOR[RealFuels_StockEngines]
{

  @mass = 1.5
  @cost = 3200
  %entryCost = 21250
  @maxTemp = 2266


  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 1880
    @heatProduction = 170
    @atmosphereCurve
    {
      @key,0 = 0 332
      @key,1 = 1 283
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Kerosene
      ratio = 37.694087
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = LqdOxygen
      ratio = 62.305913
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }

  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 6
    origTechLevel = 6
    engineType = L+
    origMass = 1.5
    configuration = Kerosene+LqdOxygen
    modded = false

    CONFIG
    {
      name = Kerosene+LqdOxygen
      maxThrust = 1880
      heatProduction = 160
      PROPELLANT
      {
        name = Kerosene
        ratio = 37.69408655434424
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 62.30591344565576
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.05
      IspV = 0.97
      throttle = 0
      ignitions = 1
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 15
      }


    }
    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 1350
      heatProduction = 160
      PROPELLANT
      {
        name = Aerozine50
        ratio = 50.17301038062284
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = NTO
        ratio = 49.82698961937716
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.008
      IspV = 0.9215
      throttle = 0
      ignitions = 2
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 15
      }


    }
    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 1015
      heatProduction = 160
      PROPELLANT
      {
        name = LqdHydrogen
        ratio = 76.30830964721619
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 23.69169035278381
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.365
      IspV = 1.2319
      throttle = 0
      ignitions = 1
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 15
      }


    }
  }
  ignitions = 1
  ullage = true
  pressureFed = false
  IGNITOR_RESOURCE
  {
    name = ElectricCharge
    amount = 15
  }


}

@PART[LiquidEngineLV-T91]:FOR[RealFuels_StockEngines]
{

  @mass = 0.4
  @cost = 350
  %entryCost = 2455
  @maxTemp = 1516


  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 120
    @heatProduction = 94
    @atmosphereCurve
    {
      @key,0 = 0 325
      @key,1 = 1 110
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Aerozine50
      ratio = 50.173010
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = NTO
      ratio = 49.826990
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }

  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 4
    origTechLevel = 4
    engineType = O
    origMass = 0.4
    configuration = Aerozine50+NTO
    modded = false

    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 120
      heatProduction = 94
      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 = 0.931
      throttle = 0
      ignitions = 24
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 2.2
      }


    }
    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 90
      heatProduction = 94
      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 = 1.2446
      throttle = 0
      ignitions = 24
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 2.2
      }


    }
  }
  ignitions = 24
  ullage = true
  pressureFed = false
  IGNITOR_RESOURCE
  {
    name = ElectricCharge
    amount = 2.2
  }


}

@PART[LiquidEngineRE-I2]:FOR[RealFuels_StockEngines]
{

  @mass = 0.53
  @cost = 920
  %entryCost = 7050
  @maxTemp = 1948


  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 300
    @heatProduction = 138
    @atmosphereCurve
    {
      @key,0 = 0 350
      @key,1 = 1 211
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Kerosene
      ratio = 37.694087
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = LqdOxygen
      ratio = 62.305913
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }

  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 5
    origTechLevel = 5
    engineType = U
    origMass = 0.53
    configuration = Kerosene+LqdOxygen
    modded = false

    CONFIG
    {
      name = Kerosene+LqdOxygen
      maxThrust = 300
      heatProduction = 138
      PROPELLANT
      {
        name = Kerosene
        ratio = 37.69408655434424
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 62.30591344565576
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.015
      IspV = 1.015
      throttle = 0
      ignitions = 1
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 4.5
      }


    }
    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 300
      heatProduction = 138
      PROPELLANT
      {
        name = Aerozine50
        ratio = 50.17301038062284
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = NTO
        ratio = 49.82698961937716
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 0.9744
      IspV = 0.9643
      throttle = 0
      ignitions = 4
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 4.5
      }


    }
    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 225
      heatProduction = 138
      PROPELLANT
      {
        name = LqdHydrogen
        ratio = 76.30830964721619
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 23.69169035278381
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.3195
      IspV = 1.2891
      throttle = 0
      ignitions = 1
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 4.5
      }


    }
  }
  ignitions = 1
  ullage = true
  pressureFed = false
  IGNITOR_RESOURCE
  {
    name = ElectricCharge
    amount = 4.5
  }


}

@PART[LiquidEngineRE-J10]:FOR[RealFuels_StockEngines]
{

  @mass = 1.1
  @cost = 1200
  %entryCost = 10000
  @maxTemp = 1516


  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 340
    @heatProduction = 110
    @atmosphereCurve
    {
      @key,0 = 0 351
      @key,1 = 1 122
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Aerozine50
      ratio = 50.173010
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = NTO
      ratio = 49.826990
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }

  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 5
    origTechLevel = 5
    engineType = O
    origMass = 1.1
    configuration = Aerozine50+NTO
    modded = false

    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 340
      heatProduction = 110
      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
      ignitions = 24
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 2.2
      }


    }
    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 255
      heatProduction = 110
      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 = 24
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 2.2
      }


    }
  }
  ignitions = 24
  ullage = true
  pressureFed = false
  IGNITOR_RESOURCE
  {
    name = ElectricCharge
    amount = 2.2
  }


}

@PART[LiquidEngineRK-7]:FOR[RealFuels_StockEngines]
{

  @mass = 0.4
  @cost = 440
  %entryCost = 3500
  @maxTemp = 2266


  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 350
    @heatProduction = 140
    @atmosphereCurve
    {
      @key,0 = 0 256
      @key,1 = 1 231
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Kerosene
      ratio = 37.694087
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = LqdOxygen
      ratio = 62.305913
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }

  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 3
    origTechLevel = 3
    engineType = L
    origMass = 0.4
    configuration = Kerosene+LqdOxygen
    modded = false

    CONFIG
    {
      name = Kerosene+LqdOxygen
      maxThrust = 350
      heatProduction = 140
      PROPELLANT
      {
        name = Kerosene
        ratio = 37.69408655434424
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 62.30591344565576
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.0000
      IspV = 1.0000
      throttle = 0
      ignitions = 1
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 1.5
      }


    }
    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 350
      heatProduction = 140
      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
      ignitions = 2
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 1.5
      }


    }
    
  }
  ignitions = 1
  ullage = true
  pressureFed = false
  IGNITOR_RESOURCE
  {
    name = ElectricCharge
    amount = 1.5
  }


}

@PART[LiquidEngineRV-1]:FOR[RealFuels_StockEngines] 
{

  @mass = 0.06
  @cost = 300
  %entryCost = 2000
  @maxTemp = 2082


  @MODULE[ModuleEngine*]
  {
    @name = ModuleEnginesRF
    @maxThrust = 45
    @heatProduction = 166
    @atmosphereCurve
    {
      @key,0 = 0 310
      @key,1 = 1 254
    }
    !PROPELLANT[LiquidFuel] {}
    !PROPELLANT[Oxidizer] {}
    !PROPELLANT[MonoPropellant] {}
    PROPELLANT
    {
      name = Kerosene
      ratio = 37.694087
      DrawGauge = True
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
    PROPELLANT
    {
      name = LqdOxygen
      ratio = 62.305913
      %resourceFlowMode = STACK_PRIORITY_SEARCH
    }
  }

  MODULE
  {
    name = ModuleEngineConfigs
    type = ModuleEnginesRF
    techLevel = 3
    origTechLevel = 3
    engineType = L+
    origMass = 0.06
    configuration = Kerosene+LqdOxygen
    modded = false

    CONFIG
    {
      name = Kerosene+LqdOxygen
      maxThrust = 45
      heatProduction = 166
      PROPELLANT
      {
        name = Kerosene
        ratio = 37.69408655434424
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 62.30591344565576
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 0.97
      IspV = 0.97
      throttle = 0
      ignitions = 2
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 0.3
      }


    }
    CONFIG
    {
      name = Aerozine50+NTO
      maxThrust = 45
      heatProduction = 166
      PROPELLANT
      {
        name = Aerozine50
        ratio = 50.17301038062284
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = NTO
        ratio = 49.82698961937716
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 0.9312
      IspV = 0.9215
      throttle = 0
      ignitions = 4
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 0.3
      }


    }
    CONFIG
    {
      name = LqdHydrogen+LqdOxygen
      maxThrust = 34
      heatProduction = 166
      PROPELLANT
      {
        name = LqdHydrogen
        ratio = 76.30830964721619
        DrawGauge = True
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      PROPELLANT
      {
        name = LqdOxygen
        ratio = 23.69169035278381
        %resourceFlowMode = STACK_PRIORITY_SEARCH
      }
      IspSL = 1.261
      IspV = 1.2319
      throttle = 0
      ignitions = 2
      ullage = true
      pressureFed = false
      IGNITOR_RESOURCE
      {
        name = ElectricCharge
        amount = 0.3
      }


    }
  }
  ignitions = 2
  ullage = true
  pressureFed = false
  IGNITOR_RESOURCE
  {
    name = ElectricCharge
    amount = 0.3
  }


}

 

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