bluedog.LunarOrbiter.Propulsion

This part is from Bluedog DB

cost:
165
mass:
0.02425
TechRequired:
basicScience
engine_data:
standard
{"isp"=>{"vac"=>240.0, "atmo"=>180.0}, "propellant_ratios"=>{"MonoPropellant"=>0.9}, "max_thrust"=>0.75}
resources:
MonoPropellant
22.0

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