rn.dnepr1.rd264

cost:
400
mass:
1.25
category:
Propulsion
TechRequired:
start
engine_data:
standard
{"isp"=>{"vac"=>300.0, "atmo"=>280.0}, "propellant_ratios"=>{"LiquidFuel"=>0.9, "Oxidizer"=>1.1}, "max_thrust"=>475.0}

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