ROMini.cfg

// Redo properties
@PART[*]:HAS[@RESOURCE[SolidFuel]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@mass *= 4.8 // will multiply by 0.25 later, yielding 1.2x orig mass. With 1.7x resource,
	// we get decent mass ratios.
	@MODULE,*:HAS[#name[ModuleEngine*],!PROPELLANT[IntakeAir]]
	{
		key0 = temp
		key1 = temp
		@key0 = #$atmosphereCurve/key,0$
		@key1 = #$atmosphereCurve/key,1$
		@key0 ^= :0 ::
		@key1 ^= :1 ::
		@key0 *= 1.4
		@key1 *= 1.4
		@maxThrust *= 3.4 // double the resource multiplier, divided by all-engine multiplier
		// to keep pace with fuel change alone it'd be 1.0625 x 1.6 = 1.7
		@atmosphereCurve
		{
			@key,0 = #$../key0$
			@key,0 ^= :^:0 :
			@key,1 = #$../key1$
			@key,1 ^= :^:1 :
		}
	}
	@RESOURCE[SolidFuel]
	{
		@amount *= 1.7
		@maxAmount *= 1.7
	}
}

@PART[*]:HAS[@MODULE[ModuleEngines*]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@mass *= 0.25
	@MODULE,*:HAS[#name[ModuleEngines*]]
	{
		@maxThrust *= 1 // was 1.6
	}
	@MODULE[ModuleGimbal]
	{
		//@gimbalRange *= 2 // Disabled for now, to avoid MJ twitch
	}
}
// Special case engines
// Jets
@PART[*]:HAS[@MODULE[ModuleEngine*]:HAS[@PROPELLANT[IntakeAir]]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@mass *= 3.75
	@MODULE[ModuleEngine*]:HAS[@PROPELLANT[IntakeAir]]
	{
		@maxThrust *= 0.5
		@atmosphereCurve
		{
			@key ^= :^0 ::
			@key ^= : 0 0::
			@key *= 0.75
			@key ^= :^:0 :
			@key ^= :$: 0 0:
		}
	}
}
// NTR
@PART[nuclearEngine]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@mass *= 3
	
}

// Tanks
@PART[*]:HAS[@RESOURCE[LiquidFuel]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	//@mass *= 0.2353 // will be done by rescale, uncomment if not rescaling.
	// Note, if not rescaling, LF and LFO tanks should have 0.83x resources,
	// same for Ore, and Monoprop should have 1.25x the resources to account for density diff
}

// Heat shields
@PART[*]:HAS[@MODULE[ModuleAblator]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@MODULE[ModuleAblator]
	{
		@lossConst *= 0.1
	}
}

// RESCALE
@PART[*]:HAS[#rescaleFactor[*]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@rescaleFactor *= 1.6
}
@PART[*]:HAS[~rescaleFactor[]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	rescaleFactor = 2.0
}
@PART[*]:HAS[~scale[]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	scale = 1.0
}
// This _should_ work, but scale seems to fail in 1.0.4...
//@PART[*]:HAS[@MODEL]:FOR[zROMini]:NEEDS[!RealismOverhaul]
//{
//	@MODEL,*:HAS[~scale[]]
//	{
//		scale = 1, 1, 1
//	}
//	@MODEL,*
//	{
//		scaleX = #$scale[0]$
//		scaleY = #$scale[1]$
//		scaleZ = #$scale[2]$
//		@scaleX *= #$../rescaleFactor$
//		@scaleY *= #$../rescaleFactor$
//		@scaleZ *= #$../rescaleFactor$
//		@scale = #$scaleX$,$scaleY$,$scaleZ$
//	}
//}
//@PART[*]:HAS[@MODEL]:FOR[zROMini]:NEEDS[!RealismOverhaul]
//{
//	@scale *= #$rescaleFactor$
//}
//@PART[*]:HAS[@MODEL]:FOR[zROMini]:NEEDS[!RealismOverhaul]
//{
//	@rescaleFactor = 1.0
//}
// Parachutes, special case
@PART[*]:HAS[@MODULE[ModuleDragModifier],@MODULE[ModuleParachute]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@MODULE,*:HAS[#name[ModuleDragModifier]]
	{
		@dragModifier *= 0.390625 // 1/1.6^2
	}
}

// Drag cube changes from rescale
@PART[*]:HAS[@DRAG_CUBE]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@DRAG_CUBE
	{
		@cube,*[1,,] *= 1.6
		@cube,*[3,,] *= 1.6
		@cube,*[4,,] *= 1.6
		@cube,*[6,,] *= 1.6
		@cube,*[7,,] *= 1.6
		@cube,*[9,,] *= 1.6
		@cube,*[10,,] *= 1.6
		@cube,*[12,,] *= 1.6
		@cube,*[13,,] *= 1.6
		@cube,*[15,,] *= 1.6
		@cube,*[16,,] *= 1.6
		@cube,*[18,,] *= 1.6
		@cube,*[19,,] *= 1.6
		@cube,*[20,,] *= 1.6
		@cube,*[21,,] *= 1.6
		@cube,*[22,,] *= 1.6
		@cube,*[23,,] *= 1.6
		@cube,*[24,,] *= 1.6
	}
}

// Stat changes from rescale
// Engines: increase by throat area
@PART[*]:HAS[@MODULE[ModuleEngines*]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@mass *= 2.56
	@MODULE,*:HAS[#name[ModuleEngines*]]
	{
		@maxThrust *= 2.56
	}
}
// SRBs: Increase from volume increase
@PART[*]:HAS[@RESOURCE[SolidFuel]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@MODULE,*:HAS[#name[ModuleEngines*]]
	{
		@maxThrust *= 1.328125 // already a factor of 2.56 from all-engines, above.
	}
	@mass *= 1.328125 // ditto
	@RESOURCE[SolidFuel]
	{
		@amount *= 3.4
		@maxAmount *= 3.4
	}
}
// Fuel tanks, lower dry mass
@PART[*]:HAS[@RESOURCE[LiquidFuel],!MODULE[ModuleCommand],!MODULE[ModuleEngines*]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@mass *= 0.8
}
// Increase volume of all tanks as appropriate
@PART[*]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@RESOURCE[Oxidizer]
	{
		@amount *= 3.4
		@maxAmount *= 3.4
	}
	@RESOURCE[LiquidFuel]
	{
		@amount *= 3.4 // should be 4.096 but this is correct for density and MR
		@maxAmount *= 3.4
	}
	@RESOURCE[MonoPropellant]
	{
		@amount *= 1.25 // higher dry fraction
		// Note: this means that volume utilization will only be 1/3 that of a regular
		// LFO tank....
		@maxAmount *= 1.25
	}
	@RESOURCE[XenonGas]
	{
		@amount *= 4
		@maxAmount *= 4
	}
	@RESOURCE[Ore]
	{
		@amount *= 3.4
		@maxAmount *= 3.4 // assume same density as LF/OX
	}
	@RESOURCE[IntakeAir]
	{
		@amount *= 4
		@maxAmount *= 4
	}
}
// decrease resource costs
@RESOURCE_DEFINITION[Oxidizer|LiquidFuel|SolidFuel|MonoPropellant|XenonGas]
{
	@unitCost *= 0.1
}
// Rescale wings
@PART[*]:HAS[@MODULE[*]:HAS[#deflectionLiftCoeff[*]]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@mass *= 2.56
	@MODULE,*:HAS[#deflectionLiftCoeff[*]]
	{
		@deflectionLiftCoeff *= 2.56
	}
}
// Catch Mk2 fuselages that have the wing modules...
@PART[*]:HAS[@MODULE[*]:HAS[#useInternalDragModel[False]]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@mass *= 0.390625 // reset mass
}
// scale up intakes
@PART[*]:HAS[@MODULE[ModuleResourceIntake]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	@mass *= 2.56
	@MODULE[ModuleResourceIntake]
	{
		@area *= 2.56
	}
}
// Handle proc fairings.
@PART[*]:HAS[@MODULE[ModuleProceduralFairing]]:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	%rescaleFactor = 1.0
	@MODEL
	{
		%scale = 1.6, 1.6, 1.6
	}
	stack_top0 = #$node_stack_top[0]$
	stack_top1 = #$node_stack_top[1]$
	stack_top2 = #$node_stack_top[2]$
	@stack_top0 *= 1.6
	@stack_top1 *= 1.6
	@stack_top2 *= 1.6
	stack_top_new = #$stack_top0$,$stack_top1$,$stack_top2$,$node_stack_top[3]$,$node_stack_top[4]$,$node_stack_top[5]$,$node_stack_top[6]$
	@node_stack_top = #$stack_top_new$
	!stack_top0 = DEL
	!stack_top1 = DEL
	!stack_top2 = DEL
	!stack_top_new = DEL
	
	stack_bottom0 = #$node_stack_bottom[0]$
	stack_bottom1 = #$node_stack_bottom[1]$
	stack_bottom2 = #$node_stack_bottom[2]$
	@stack_bottom0 *= 1.6
	@stack_bottom1 *= 1.6
	@stack_bottom2 *= 1.6
	stack_bottom_new = #$stack_bottom0$,$stack_bottom1$,$stack_bottom2$,$node_stack_bottom[3]$,$node_stack_bottom[4]$,$node_stack_bottom[5]$,$node_stack_bottom[6]$
	@node_stack_bottom = #$stack_bottom_new$
	!stack_bottom0 = DEL
	!stack_bottom1 = DEL
	!stack_bottom2 = DEL
	!stack_bottom_new = DEL
	
	@MODULE[ModuleProceduralFairing]
	{
		@baseRadius *= 1.6
		@maxRadius *= 1.6
		//@capRadius *= 1.6
		@snapThreshold *= 1.6
		
		//@xSectionHeightMin = 0.2
		@xSectionHeightMax *= 2
		
		//edgeSlide = 0.15
		//edgeWarp = 0
		//noseTip = 0.7
		
		@UnitAreaMass = 0.0075
		@UnitAreaCost = 6
	}
}

// Physics
@PHYSICSGLOBALS:FOR[zROMini]:NEEDS[!RealismOverhaul]
{
	// AeroFX
	@aeroFXScalar = 0.003
	@aeroFXDensityExponent = 0.5
	@aeroFXStartThermalFX = 2.5
	@aeroFXFullThermalFX = 3.5
	@aeroFXExponent = 3.5
	
	// CONSTANTS
	@spaceTemperature = 4
	@solarLuminosityAtHome = 1360
	@solarInsolationAtHome = 0.15
	@standardSpecificHeatCapacity = 800
	@internalHeatProductionFactor = 0.025
	@aerodynamicHeatProductionFactor = 1.0
	
	// CONVECTION
	// Convection areas
	@fullConvectionAreaMin = -0.1
	@fullToCrossSectionLerpStart = 0.8
	@fullToCrossSectionLerpEnd = 1.5
	
	// Newtonian-To-Hypersonic transition
	@machConvectionStart = 2
	@machConvectionEnd = 4.0
	@machConvectionExponent = 3
	@convectionFactorSplashed = 5000
	
	// Turbulent convection (total guesses)
	@turbulentConvectionStart = 100
	@turbulentConvectionEnd = 400
	@turbulentConvectionMult = 25
	
	// Newtonian Convection
	@newtonianConvectionFactorBase = 4.0
	@newtonianConvectionFactorTotal = 1.0
	@newtonianDensityExponent = 0.5
	@newtonianVelocityExponent = 1.0
	
	// Hypersonic Convection
	@convectionDensityExponent = 0.5
	@convectionVelocityExponent = 3.0
	@convectionFactor = 1.1
	@machTemperatureScalar = 7.5 // ~6000 at 7.3km/sec
	@machTemperatureVelocityExponent = 0.75
	
	// CONDUCTION
	@conductionFactor = 5
	@skinSkinConductionFactor = 0.06
	@skinInteralConductionFactor = 0.25
	@shieldedConductionFactor = 0.01
	
	// RADIATION
	@partEmissivityExponent = 4
	@radiationFactor = 1
}

// ENGINE RADIAL ATTACH
@PART[*]:HAS[@MODULE[ModuleEngines*],~node_attach[],#node_stack_top[*]]:FINAL
{
	node_attach = #$node_stack_top$
}
@PART[*]:HAS[#node_attach[*],#attachRules[1,0,1,0,0]]:FINAL
{
	@attachRules = 1,1,1,0,0
}
@PART[*]:HAS[#node_attach[*],#attachRules[1,0,1,1,0]]:FINAL
{
	@attachRules = 1,1,1,1,0
}