File:Overall thrust to weight.png
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Overall_thrust_to_weight.png (400 × 300 pixels, file size: 4 KB, MIME type: image/png)
Graph representing rocket dry and wet mass as function of the vehicle (overall) initial thrust-to-weight ratio. There is an equivalence with the acceleration in number of G's.
File history
Yi efo/eka'e gwa ebo wo le nyangagi wuncin ye kamina wunga tinya nan
| Gwalagizhi | Nyangagi | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 20:06, 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. |
| 04:47, 1 November 2012 |  | 400 × 300 (4 KB) | Vincent (Sọ̀rọ̀ | contribs) | Graph representing rocket dry and wet mass as function of the vehicle (overall) initial thrust-to-weight ratio. There is an equivalence with the acceleration in number of G's. |
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