Template:Specific impulse: Difference between revisions
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Latest revision as of 17:15, 17 February 2023
| 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] |
Template documentation
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}}
[[Category:Template documentation pages{{#translation:}}]]
References
- ↑ 1.0 1.1 1.2 1.3 Braeunig, Robert A. (2008). "Rocket Propellants". Rocket & Space Technology.
