rn.dnepr1.ejector.cap

cost:
9000
mass:
0.01
category:
Propulsion
TechRequired:
veryHeavyRocketry
engine_data:
standard
{"isp"=>{"vac"=>105.0, "atmo"=>105.0}, "propellant_ratios"=>{"SolidFuel"=>1.0}, "max_thrust"=>5300.0}
resources:
SolidFuel
445.0

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