Difference between revisions of "Parts/Aero/wings/structural1.cfg"
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< Parts
m (XZise moved page Parts/SPP/Wings/structural1.cfg to Parts/Structural/structuralWing/part.cfg without leaving a redirect: merge with old part config) |
m (Update config) |
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{{Part config|Structural Wing Type A|2=PART | {{Part config|Structural Wing Type A|2=PART | ||
{ | { | ||
| − | + | name = structuralWing | |
| − | name = structuralWing | + | module = Part |
| − | module = Part | + | author = Porkjet |
| − | author = Porkjet | + | rescaleFactor = 1 |
| − | + | node_attach = 0.04, 0.0, 0.0, 1.0, 0.0, 0.0, 1 | |
| − | MODEL | + | CoMOffset = -0.7, -0.6, 0 |
| − | { | + | CoLOffset = -0.7, -0.6, 0 |
| − | + | CoPOffset = -0.7, -0.6, 0 | |
| + | TechRequired = supersonicFlight | ||
| + | entryCost = 6400 | ||
| + | cost = 500 | ||
| + | category = Aero | ||
| + | subcategory = 0 | ||
| + | title = #autoLOC_500268 //#autoLOC_500268 = Structural Wing Type A | ||
| + | manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division | ||
| + | description = #autoLOC_500269 //#autoLOC_500269 = This wing has been constructed out of surplus wing components. Comes complete with "like new" finish. Intended uses include very large canards, and leading edges of larger delta wings. | ||
| + | attachRules = 0,1,0,1,1 | ||
| + | mass = 0.1 | ||
| + | thermalMassModifier = 8.0 // the dang things are light, so 3200 kJ/tonne-K | ||
| + | // heatConductivity = 0.06 // half default | ||
| + | emissiveConstant = 0.95 | ||
| + | dragModelType = none | ||
| + | maximum_drag = 0.02 | ||
| + | minimum_drag = 0.02 | ||
| + | angularDrag = 2 | ||
| + | crashTolerance = 15 | ||
| + | maxTemp = 2400 // = 3400 | ||
| + | explosionPotential = 0.1 | ||
| + | fuelCrossFeed = True | ||
| + | bulkheadProfiles = srf | ||
| + | tags = #autoLOC_500270 //#autoLOC_500270 = aero aircraft fligh foil lift plane swept | ||
| + | MODEL | ||
| + | { | ||
| + | model = Squad/Parts/Aero/wings/structural1 | ||
| + | } | ||
| + | MODULE | ||
| + | { | ||
| + | name = ModuleLiftingSurface | ||
| + | useInternalDragModel = True | ||
| + | deflectionLiftCoeff = 1 | ||
| + | dragAtMaxAoA = 0.3 | ||
| + | dragAtMinAoA = 0.0 | ||
| + | } | ||
| + | MODULE | ||
| + | { | ||
| + | name = ModuleCargoPart | ||
| + | packedVolume = -1 | ||
| + | } | ||
} | } | ||
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}} | }} | ||
Latest revision as of 11:00, 13 October 2024
PART
{
name = structuralWing
module = Part
author = Porkjet
rescaleFactor = 1
node_attach = 0.04, 0.0, 0.0, 1.0, 0.0, 0.0, 1
CoMOffset = -0.7, -0.6, 0
CoLOffset = -0.7, -0.6, 0
CoPOffset = -0.7, -0.6, 0
TechRequired = supersonicFlight
entryCost = 6400
cost = 500
category = Aero
subcategory = 0
title = #autoLOC_500268 //#autoLOC_500268 = Structural Wing Type A
manufacturer = #autoLOC_501624 //#autoLOC_501624 = C7 Aerospace Division
description = #autoLOC_500269 //#autoLOC_500269 = This wing has been constructed out of surplus wing components. Comes complete with "like new" finish. Intended uses include very large canards, and leading edges of larger delta wings.
attachRules = 0,1,0,1,1
mass = 0.1
thermalMassModifier = 8.0 // the dang things are light, so 3200 kJ/tonne-K
// heatConductivity = 0.06 // half default
emissiveConstant = 0.95
dragModelType = none
maximum_drag = 0.02
minimum_drag = 0.02
angularDrag = 2
crashTolerance = 15
maxTemp = 2400 // = 3400
explosionPotential = 0.1
fuelCrossFeed = True
bulkheadProfiles = srf
tags = #autoLOC_500270 //#autoLOC_500270 = aero aircraft fligh foil lift plane swept
MODEL
{
model = Squad/Parts/Aero/wings/structural1
}
MODULE
{
name = ModuleLiftingSurface
useInternalDragModel = True
deflectionLiftCoeff = 1
dragAtMaxAoA = 0.3
dragAtMinAoA = 0.0
}
MODULE
{
name = ModuleCargoPart
packedVolume = -1
}
}
