https://www.vigyanwiki.in/index.php?action=history&feed=atom&title=Template%3ASpecific_impulseTemplate:Specific impulse - Revision history2026-06-09T09:43:12ZRevision history for this page on the wikiMediaWiki 1.39.3https://www.vigyanwiki.in/index.php?title=Template:Specific_impulse&diff=88586&oldid=prevIndicwiki: 1 revision imported from :alpha:Template:Specific_impulse2023-02-17T11:45:54Z<p>1 revision imported from <a href="https://alpha.indicwiki.in/index.php?title=Template:Specific_impulse" class="extiw" title="alpha:Template:Specific impulse">alpha:Template:Specific_impulse</a></p>
<table style="background-color: #fff; color: #202122;" data-mw="interface">
<tr class="diff-title" lang="en-GB">
<td colspan="1" style="background-color: #fff; color: #202122; text-align: center;">← Older revision</td>
<td colspan="1" style="background-color: #fff; color: #202122; text-align: center;">Revision as of 17:15, 17 February 2023</td>
</tr><tr><td colspan="2" class="diff-notice" lang="en-GB"><div class="mw-diff-empty">(No difference)</div>
</td></tr></table>Indicwikihttps://www.vigyanwiki.in/index.php?title=Template:Specific_impulse&diff=88585&oldid=prevalpha>Indicwiki: Created page with "<!-- this is a short table intended for use in rocket, rocket engine etc. of the performance of common propellant mixes. It's intended to have only about 10 entries at most; i..."2023-01-26T16:55:40Z<p>Created page with "<!-- this is a short table intended for use in rocket, rocket engine etc. of the performance of common propellant mixes. It's intended to have only about 10 entries at most; i..."</p>
<p><b>New page</b></p><div><!-- this is a short table intended for use in rocket, rocket engine etc. of the performance of common propellant mixes. It's intended to have only about 10 entries at most; it is NOT a complete list. Table has been edited to include actual vacuum performance of rocket engines instead of theoretical maximum Isp.<br />
-->{| class="wikitable" style="text-align:center; {{#switch:{{{align|}}}<br />
| left = float: left; clear:left; margin-right:1em<br />
| right = float:right; clear:right; margin-left:1em <br />
| center = margin:0.5em auto<br />
}}"<br />
|+ [[Specific impulse|''I''<sub>sp</sub>]] in vacuum of various rockets<br />
|-<br />
! Rocket<br />
! Propellants<br />
! ''I''<sub>sp</sub>, vacuum (s)<br />
|-<br />
! [[Space Shuttle main engine|Space Shuttle<br/>liquid engines]]<br />
| [[Liquid oxygen|LOX]]/[[liquid hydrogen|LH<sub>2</sub>]]<br />
| 453<ref name="spec_impulse">{{cite web |url=http://www.braeunig.us/space/propel.htm |first=Robert A. |last=Braeunig |title=Rocket Propellants |website=Rocket & Space Technology |date=2008}}</ref><br />
|-<br />
! [[Space Shuttle Solid Rocket Booster|Space Shuttle<br/>solid motors]]<br />
| [[Ammonium perchlorate composite propellant|APCP]]<br />
| 268<ref name="spec_impulse"/><br />
|-<br />
! [[Space Shuttle Orbital Maneuvering System|Space Shuttle<br/>OMS]]<br />
| [[Nitrogen tetroxide|NTO]]/[[monomethylhydrazine|MMH]]<br />
| 313<ref name="spec_impulse"/><br />
|-<br />
! [[S-IC|Saturn V<br/>stage 1]]<br />
| [[Liquid oxygen|LOX]]/[[rocket propellant-1|RP-1]]<br />
| 304<ref name="spec_impulse"/><br />
|}<noinclude><br />
{{documentation|content=<br />
This is a short table intended for use in rocket, rocket engine, etc. of the performance of common propellant mixes. It's intended to have only about 10 entries at most; it is NOT a complete list. Table has been edited to include actual vacuum performance of rocket engines instead of theoretical maximum Isp.<br />
<br />
== Usage ==<br />
:{{tld|specific impulse}}<br />
or<br />
:{{tld|specific impulse|align{{=}}left, right, or center}}<br />
<br />
}}<br />
{{Template reference list}}<br />
</noinclude></div>alpha>Indicwiki