Difference between revisions of "Template:Infobox rocket engine"
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{|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;" | {|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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|colspan="2" align="center"|[[Image:{{{pic1_file|Nopic.png}}}|240px]] | |colspan="2" align="center"|[[Image:{{{pic1_file|Nopic.png}}}|240px]] |
Revision as of 15:21, 17 January 2007
{{{name}}} | |
---|---|
Overview | |
Vacuum thrust | {{{thrust_vac}}} |
Sealevel thrust | N/A |
specific impulse (vac) | {{{isp_vac}}} |
Fuel | Unknown |
Oxidizer | Unknown |
Cycle | Unknown |
First flight | Unknown |
Entered service | Unknown |
Manufacturer | Unknown |
Dimensions | |
Length | Unknown |
Width | Unknown |
Dry mass | Unknown |
Power head | |
Chamber pressure | Unknown |
Chamber temperature | Unknown |
Fuel flow rate | Unknown |
Oxidizer flow rate | Unknown |