File:DeltaV.png: Difference between revisions
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Graph representing rocket dry and wet mass as function of the Delta V. Done with version 3 of File:Rocket_mass.c, overall thrust-to-weight ratio is 2.5 and Isp is 340s. |
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Latest revision as of 20:53, 11 December 2012
Graph representing rocket dry and wet mass as function of the Delta V. Done with version 3 of File:Rocket mass.c, overall thrust-to-weight ratio is 2.5 and Isp is 340s.
File history
Yi efo/eka'e gwa ebo wo le nyangagi wuncin ye kamina wunga tinya nan
| Gwalagizhi | Nyangagi | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 20:53, 11 December 2012 |  | 400 × 300 (4 KB) | Vincent (Sọ̀rọ̀ | contribs) | Graph representing rocket dry and wet mass as function of the Delta V. Done with version 3 of File:Rocket_mass.c, overall thrust-to-weight ratio is 2.5 and Isp is 340s. |
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