Template:Infobox rocket engine
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{{{name}}} | |
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[[Image:{{{pic1_file}}}|240px]] | |
{{{pic1_text}}} | |
Overview | |
Vacuum thrust | {{{thrust_vac}}} |
Sealevel thrust | {{{thrust_sl}}} |
specific impulse (vac) | {{{isp_vac}}} |
Fuel | {{{fuel}}} |
Oxidizer | {{{oxidizer}}} |
Cycle | {{{cycle}}} |
First flight | {{{first_flight_date}}} |
Entered service | {{{service_date}}} |
Manufacturer | {{{manufacturer}}} |
Dimensions | |
Length | {{{length}}} |
Width | {{{width}}} |
Dry mass | {{{dry_mass}}} |
Power head | |
Chamber pressure | {{{pc}}} |
Chamber temperature | {{{tc}}} |
Fuel flow rate | {{{dmf}}} |
Oxidizer flow rate | {{{dmo}}} |