This part is from ProjectEOC
cost:
200
mass:
0.1
category:
Structural
TechRequired:
heavyAerodynamics
engine_data:
standard
{"isp"=>{"vac"=>154.0, "atmo"=>118.0}, "propellant_ratios"=>{"SolidFuel"=>1.0}, "max_thrust"=>500.0}
resources:
SolidFuel
2.0
