Template:Specific impulse
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Revision as of 23:11, 7 April 2021 by imported>Jworkorg (import)
Rocket | Propellants | Isp, vacuum (s) |
---|---|---|
Space shuttle liquid engines |
LOX/LH2 | 453[1] |
Space shuttle solid motors |
APCP | 268[1] |
Space shuttle OMS |
NTO/MMH | 313[1] |
Saturn V stage 1 |
LOX/RP-1 | 304[1] |
![](/wiki/images/thumb/4/43/Test_Template_Info-Icon_-_Version_%282%29.svg/50px-Test_Template_Info-Icon_-_Version_%282%29.svg.png)
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.
Usage
{{specific impulse}}
or
{{specific impulse|align=left, right, or center}}
References
- ↑ 1.0 1.1 1.2 1.3 Braeunig, Robert A. (2008). "Rocket Propellants". http://www.braeunig.us/space/propel.htm.