Difference between revisions of "Parts/Aero/wings/structural1.cfg"
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< Parts
m (BobBot moved page Parts/SPP/Wings/structural1.cfg to Parts/Aero/wings/structural1.cfg without leaving a redirect: Renamed part configuration file after update.) |
m (*update to 1.0;) |
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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 = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1 | |
| − | + | TechRequired = aerodynamicSystems | |
| − | + | entryCost = 6400 | |
| − | + | cost = 500 | |
| − | + | category = Aero | |
| − | + | subcategory = 0 | |
| − | + | title = Structural Wing Type A | |
| − | rescaleFactor = 1 | + | manufacturer = C7 Aerospace Division |
| − | + | description = 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 | |
| − | node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1 | + | mass = 0.05 |
| − | + | thermalMassModifier = 4.0 // the dang things are light, so 3200 kJ/tonne-K | |
| − | + | // heatConductivity = 0.06 // half default | |
| − | TechRequired = aerodynamicSystems | + | emissiveConstant = 0.95 |
| − | entryCost = 6400 | + | dragModelType = none |
| − | cost = 500 | + | maximum_drag = 0.02 |
| − | category = Aero | + | minimum_drag = 0.02 |
| − | subcategory = 0 | + | angularDrag = 2 |
| − | title = Structural Wing Type A | + | crashTolerance = 15 |
| − | manufacturer = C7 Aerospace Division | + | maxTemp = 2000 // = 3400 |
| − | description = 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. | + | explosionPotential = 0.1 |
| − | + | fuelCrossFeed = True | |
| − | + | bulkheadProfiles = srf | |
| − | attachRules = 0,1,0,1,1 | + | MODEL |
| − | + | { | |
| − | + | model = Squad/Parts/Aero/wings/structural1 | |
| − | // | + | } |
| − | + | MODULE | |
| − | dragModelType = | + | { |
| − | maximum_drag = 0.02 | + | name = ModuleLiftingSurface |
| − | minimum_drag = 0.02 | + | useInternalDragModel = True |
| − | angularDrag = 2 | + | deflectionLiftCoeff = 1 |
| − | crashTolerance = 15 | + | dragAtMaxAoA = 0.3 |
| − | maxTemp = 3400 | + | dragAtMinAoA = 0.0 |
| − | explosionPotential = 0.1 | + | } |
| − | fuelCrossFeed = True | ||
| − | |||
| − | MODULE | ||
| − | { | ||
| − | |||
| − | |||
| − | |||
| − | |||
| − | |||
| − | } | ||
| − | |||
} | } | ||
}} | }} | ||
Revision as of 10:40, 29 April 2015
PART
{
name = structuralWing
module = Part
author = Porkjet
rescaleFactor = 1
node_attach = 0.0, 0.0, 0.0, 1.0, 0.0, 0.0, 1
TechRequired = aerodynamicSystems
entryCost = 6400
cost = 500
category = Aero
subcategory = 0
title = Structural Wing Type A
manufacturer = C7 Aerospace Division
description = 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 = 0.05
thermalMassModifier = 4.0 // 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 = 2000 // = 3400
explosionPotential = 0.1
fuelCrossFeed = True
bulkheadProfiles = srf
MODEL
{
model = Squad/Parts/Aero/wings/structural1
}
MODULE
{
name = ModuleLiftingSurface
useInternalDragModel = True
deflectionLiftCoeff = 1
dragAtMaxAoA = 0.3
dragAtMinAoA = 0.0
}
}
