Difference between revisions of "Parts/Aero/wings/structural1.cfg"
From Kerbal Space Program Wiki
< Parts
m (*update to 1.0.1;) |
m (*update to 1.0.4;) |
||
| Line 5: | Line 5: | ||
author = Porkjet | author = Porkjet | ||
rescaleFactor = 1 | rescaleFactor = 1 | ||
| − | node_attach = 0. | + | node_attach = 0.04, 0.0, 0.0, 1.0, 0.0, 0.0, 1 |
| + | CoLOffset = -0.7, -0.6, 0 | ||
| + | CoPOffset = -0.7, -0.6, 0 | ||
TechRequired = aerodynamicSystems | TechRequired = aerodynamicSystems | ||
entryCost = 6400 | entryCost = 6400 | ||
| Line 16: | Line 18: | ||
attachRules = 0,1,0,1,1 | attachRules = 0,1,0,1,1 | ||
mass = 0.1 | mass = 0.1 | ||
| − | thermalMassModifier = | + | thermalMassModifier = 8.0 // the dang things are light, so 3200 kJ/tonne-K |
// heatConductivity = 0.06 // half default | // heatConductivity = 0.06 // half default | ||
emissiveConstant = 0.95 | emissiveConstant = 0.95 | ||
| Line 24: | Line 26: | ||
angularDrag = 2 | angularDrag = 2 | ||
crashTolerance = 15 | crashTolerance = 15 | ||
| − | maxTemp = | + | maxTemp = 2400 // = 3400 |
explosionPotential = 0.1 | explosionPotential = 0.1 | ||
fuelCrossFeed = True | fuelCrossFeed = True | ||
Revision as of 12:10, 27 June 2015
PART
{
name = structuralWing
module = Part
author = Porkjet
rescaleFactor = 1
node_attach = 0.04, 0.0, 0.0, 1.0, 0.0, 0.0, 1
CoLOffset = -0.7, -0.6, 0
CoPOffset = -0.7, -0.6, 0
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 = 0.1
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
MODEL
{
model = Squad/Parts/Aero/wings/structural1
}
MODULE
{
name = ModuleLiftingSurface
useInternalDragModel = True
deflectionLiftCoeff = 1
dragAtMaxAoA = 0.3
dragAtMinAoA = 0.0
}
}
