rn.n1.les

cost:
340
mass:
0.2
category:
Propulsion
TechRequired:
generalRocketry
engine_data:
standard
{"isp"=>{"vac"=>350.0, "atmo"=>350.0}, "propellant_ratios"=>{"SolidFuel"=>1.0}, "max_thrust"=>400.0}
resources:
SolidFuel
100.0

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