PART
{
// --- general parameters ---
name = SWDCSS4m
module = Part
author = TheShadow1138

// --- asset parameters ---
MODEL
{
  model = ShadowWorks/Parts/DCSS/DCSS4m
}
rescaleFactor = 1.0

// --- node definitions ---
node_stack_top = 0.0, 2.103, 0.0, 0.0, 1.0, 0.0, 2
node_stack_bottom = 0.0, -2.168, 0.0, 0.0, -1.0, 0.0, 2
node_stack_middle = 0.0, -0.503, 0.0, 0.0, -1.0, 0.0, 3




// --- Sound FX definition ---

sound_vent_medium = engage
sound_rocket_hard = running
sound_vent_soft = deactivate
sound_explosion_low = flameout

// --- editor parameters ---
TechRequired = heavierRocketry
entryCost = 4800
cost = 2000
category = FuelTank
subcategory = 0
title = Bastet Cryogenic Second Stage ("4m") SW-LT-03A
manufacturer = ShadowWorks
description = The "4m" Bastet Cryogenic Second Stage (SCSS), has an actual diameter of 2.42m, smaller than the version that was modified into the Interim Cryogenic Propulsion stage of the Amun-Ra Launcher.  Used primarily on the Bastet IV and Bastet IV Medium.

// attachment rules: stack, srfAttach, allowStack, allowSrfAttach, allowCollision
attachRules = 1,0,1,1,1

// --- standard part parameters ---
mass = 0.672	//Calculated value is 1.62 (subtracted RL-10B dry mass to get this
dragModelType = default
maximum_drag = 0.2
minimum_drag = 0.2
angularDrag = 2
crashTolerance = 12
breakingForce = 60
breakingTorque = 60
maxTemp = 2200
bulkheadProfiles = size3
stageOffset = 1
childStageOffset = 1
tags = liquid fuel oxidizer tank dcss bcss delta iv bastet shadowworks 



RESOURCE
{
 name = LiquidFuel
 amount = 500		//Original Value: 624 (ICPS)
 maxAmount = 500	//Original Value: 624
}

RESOURCE
{
 name = Oxidizer
 amount = 610		//Original Value: 763 (ICPS)
 maxAmount = 610	//Original Value: 763
}

	
}





