Difference between revisions of "Template:Infobox/Part/reaction engine"

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(Created page with "<noinclude>{{Infobox/Part/preview|</noinclude>{{Infobox/Line|{{Infobox/Part/Dict|Maximum thrust}}|{{{thrust<noinclude>|175</noinclude>}}} kN}} {{Infobox/Part/ISP|{{{isp-a...")
(No difference)

Revision as of 16:26, 10 February 2014

Maximum thrust 175 kN
Isp (1 atm) 388 s
(vacuum) 390 s

Template:Infobox/Part/FuelConsumption

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