rn.thor.altair.e2

This part is from US Rockets

cost:
700
mass:
0.36
category:
Engine
TechRequired:
generalRocketry
engine_data:
standard
{"isp"=>{"vac"=>250.0, "atmo"=>230.0}, "propellant_ratios"=>{"SolidFuel"=>1.0}, "max_thrust"=>14.0}
resources:
SolidFuel
26.5

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