This part is from AIES Aerospace
cost:
200
mass:
0.035
category:
Propulsion
TechRequired:
fuelSystems
engine_data:
standard
{"isp"=>{"vac"=>290.0, "atmo"=>220.0}, "propellant_ratios"=>{"LiquidFuel"=>0.9, "Oxidizer"=>1.1}, "max_thrust"=>3.0}
