File:Mass ratio.png: Difference between revisions
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Graph representing rocket dry and wet mass as function of the mass ratio (fixed by Isp and Delta V). |
uploaded a new version of "File:Mass ratio.png": Updated with version 3 of File:Rocket_mass.c. Delta V is 8300 instead of 9000 m/s too, and overall thrust-to-weight ratio is 2.5 instead of 1.25. |
(No difference)
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Latest revision as of 20:09, 11 December 2012
Graph representing rocket dry and wet mass as function of the mass ratio (fixed by Isp and Delta V).
File history
Yi efo/eka'e gwa ebo wo le nyangagi wuncin ye kamina wunga tinya nan
| Gwalagizhi | Nyangagi | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 20:09, 11 December 2012 |  | 400 × 300 (4 KB) | Vincent (Sọ̀rọ̀ | contribs) | Updated with version 3 of File:Rocket_mass.c. Delta V is 8300 instead of 9000 m/s too, and overall thrust-to-weight ratio is 2.5 instead of 1.25. |
| 04:44, 1 November 2012 |  | 400 × 300 (4 KB) | Vincent (Sọ̀rọ̀ | contribs) | Graph representing rocket dry and wet mass as function of the mass ratio (fixed by Isp and Delta V). |
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