Template:Infobox/Part/reaction engine

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Revision as of 16:40, 10 February 2014 by XZise (talk | contribs) (*use fuel parameter to determine density, unit and precession; *ion engines use separate template; !defaults to empty for Isp in vacuum;)
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Maximum thrust 175 kN
Isp (1 atm) 388 s
(vacuum) 390 s
Fuel consumption (1 atm) 9.20 l/s
(vacuum) 9.15 l/s
Thrust vectoring No

{{Infobox/Part}} modules for reaction engines. Use this module directly for liquid fuel engines. It uses {{Infobox/Part/FuelConsumption}} to calculate the fuel consumption based on Isp and thrust. Other engine types:

Template:Parameter Table