Difference between revisions of "Parts/Engine/liquidEngineLV-1 v2/liquidEngineLV-1 v2.cfg"
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Geostar1024 (talk | contribs) (update for 1.0) |
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{{Part config|LV-1 Liquid Fuel Engine|2=PART | {{Part config|LV-1 Liquid Fuel Engine|2=PART | ||
{ | { | ||
| − | name = microEngine | + | name = microEngine |
| − | module = Part | + | module = Part |
| − | author = NovaSilisko | + | author = NovaSilisko |
| − | + | mesh = model.mu | |
| − | mesh = model.mu | + | scale = 1 |
| − | scale = 1 | + | rescaleFactor = 1 |
| − | rescaleFactor = 1 | + | node_stack_top = 0.0, 0.0, 0.0, 0.0, 1.0, 0.0, 0 |
| − | + | node_stack_bottom = 0.0, -0.2816985, 0.0, 0.0, -1.0, 0.0, 0 | |
| − | node_stack_top = 0.0, 0.0, 0.0, 0.0, 1.0, 0.0, 0 | + | fx_exhaustFlame_white_tiny = 0.0, -0.2816985, 0.0, 0.0, 1.0, 0.0, running |
| − | node_stack_bottom = 0.0, -0.2816985, 0.0, 0.0, 1.0, 0.0, 0 | + | sound_vent_medium = engage |
| − | + | sound_rocket_mini = running | |
| − | fx_exhaustFlame_white_tiny = 0.0, -0.2816985, 0.0, 0.0, 1.0, 0.0, running | + | sound_vent_soft = disengage |
| − | + | sound_explosion_low = flameout | |
| − | sound_vent_medium = engage | + | TechRequired = propulsionSystems |
| − | sound_rocket_mini = running | + | entryCost = 4000 |
| − | sound_vent_soft = disengage | + | cost = 110 |
| − | sound_explosion_low = flameout | + | category = Engine |
| − | + | subcategory = 0 | |
| − | TechRequired = | + | title = LV-1 "Ant" Liquid Fuel Engine |
| − | entryCost = 4000 | + | manufacturer = Jebediah Kerman's Junkyard and Spacecraft Parts Co |
| − | cost = | + | description = What is this, an engine for ants? |
| − | category = Engine | + | attachRules = 1,0,1,0,0 |
| − | subcategory = 0 | + | mass = 0.02 |
| − | title = LV-1 Liquid Fuel Engine | + | // heatConductivity = 0.06 // half default |
| − | manufacturer = Jebediah Kerman's Junkyard and Spacecraft Parts Co | + | emissiveConstant = 0.8 // engine nozzles are good at radiating. |
| − | description = What is this, an engine for ants? | + | dragModelType = default |
| − | attachRules = 1,0,1,0,0 | + | maximum_drag = 0.2 |
| − | + | minimum_drag = 0.2 | |
| − | + | angularDrag = 2 | |
| − | dragModelType = default | + | crashTolerance = 7 |
| − | maximum_drag = 0.2 | + | maxTemp = 2000 // = 3600 |
| − | minimum_drag = 0.2 | + | bulkheadProfiles = size0 |
| − | angularDrag = 2 | + | MODULE |
| − | crashTolerance = 7 | ||
| − | maxTemp = 3600 | ||
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{ | { | ||
| − | name = LiquidFuel | + | name = ModuleEngines |
| − | + | thrustVectorTransformName = thrustTransform | |
| + | exhaustDamage = False | ||
| + | ignitionThreshold = 0.1 | ||
| + | minThrust = 0 | ||
| + | maxThrust = 0.54 | ||
| + | heatProduction = 8.095 | ||
| + | fxOffset = 0, 0, 0.02 | ||
| + | EngineType = LiquidFuel | ||
| + | PROPELLANT | ||
| + | { | ||
| + | name = LiquidFuel | ||
| + | ratio = 0.9 | ||
| + | DrawGauge = True | ||
| + | } | ||
| + | PROPELLANT | ||
| + | { | ||
| + | name = Oxidizer | ||
| + | ratio = 1.1 | ||
| + | } | ||
| + | atmosphereCurve | ||
| + | { | ||
| + | key = 0 315 | ||
| + | key = 1 85 | ||
| + | key = 3 0.001 | ||
| + | } | ||
} | } | ||
| − | + | MODULE | |
{ | { | ||
| − | name = | + | name = ModuleTestSubject |
| − | + | environments = 8 | |
| + | useStaging = False | ||
| + | useEvent = True | ||
} | } | ||
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} | } | ||
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}} | }} | ||
Revision as of 07:40, 28 April 2015
PART
{
name = microEngine
module = Part
author = NovaSilisko
mesh = model.mu
scale = 1
rescaleFactor = 1
node_stack_top = 0.0, 0.0, 0.0, 0.0, 1.0, 0.0, 0
node_stack_bottom = 0.0, -0.2816985, 0.0, 0.0, -1.0, 0.0, 0
fx_exhaustFlame_white_tiny = 0.0, -0.2816985, 0.0, 0.0, 1.0, 0.0, running
sound_vent_medium = engage
sound_rocket_mini = running
sound_vent_soft = disengage
sound_explosion_low = flameout
TechRequired = propulsionSystems
entryCost = 4000
cost = 110
category = Engine
subcategory = 0
title = LV-1 "Ant" Liquid Fuel Engine
manufacturer = Jebediah Kerman's Junkyard and Spacecraft Parts Co
description = What is this, an engine for ants?
attachRules = 1,0,1,0,0
mass = 0.02
// heatConductivity = 0.06 // half default
emissiveConstant = 0.8 // engine nozzles are good at radiating.
dragModelType = default
maximum_drag = 0.2
minimum_drag = 0.2
angularDrag = 2
crashTolerance = 7
maxTemp = 2000 // = 3600
bulkheadProfiles = size0
MODULE
{
name = ModuleEngines
thrustVectorTransformName = thrustTransform
exhaustDamage = False
ignitionThreshold = 0.1
minThrust = 0
maxThrust = 0.54
heatProduction = 8.095
fxOffset = 0, 0, 0.02
EngineType = LiquidFuel
PROPELLANT
{
name = LiquidFuel
ratio = 0.9
DrawGauge = True
}
PROPELLANT
{
name = Oxidizer
ratio = 1.1
}
atmosphereCurve
{
key = 0 315
key = 1 85
key = 3 0.001
}
}
MODULE
{
name = ModuleTestSubject
environments = 8
useStaging = False
useEvent = True
}
}
