Difference between revisions of "Template:Infobox rocket engine"
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(Started infobox for rocket engines, first iteration for bi-propellant engines) |
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| − | {|cellpadding="2" cellspacing="0" style="margin:25px 0 0 10px; border:3px solid lightsteelblue;width:250px; font-size: | + | {|cellpadding="2" cellspacing="0" style="margin:25px 0 0 10px; border:3px solid lightsteelblue;width:250px; font-size:80%; font-family:'Arial','Helvetica'; float: right; clear: right;" |
!bgcolor="lightsteelblue" colspan="2" align="center" |{{{name}}} | !bgcolor="lightsteelblue" colspan="2" align="center" |{{{name}}} | ||
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Revision as of 15:07, 17 January 2007
| {{{name}}} | |
|---|---|
| [[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}}} |