rn.dnepr1.ts

cost:
2000
mass:
0.65
category:
Propulsion
TechRequired:
basicRocketry
engine_data:
standard
{"isp"=>{"vac"=>345.0, "atmo"=>290.0}, "propellant_ratios"=>{"LiquidFuel"=>0.9, "Oxidizer"=>1.1}, "max_thrust"=>30.0}
resources:
ElectricCharge
200.0
LiquidFuel
45.0
Oxidizer
55.0

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