Template:Infobox/Part/reaction engine

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Maximum thrust 175 kN
Isp (1 atm) 388 s
(vacuum) 390 s
Fuel consumption (1 atm) 35.69 l/s
(vacuum) 35.69 l/s
Thrust vectoring No

{{Infobox/Part}} modules for reaction engines. Use this module directly for liquid fuel engines and ion engines. For solid rocket boosters the {{Infobox/Part/solid fuel engine}} should be used. It uses {{Infobox/Part/FuelConsumption}} to calculate the fuel consumption based on Isp and thrust.

Template:Parameter Table