File:Engine thrust to weight.png: Difference between revisions
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(Graph representing rocket dry and wet mass as function of the engine's thrust-to-weight ratio.) |
(uploaded a new version of "File:Engine thrust to weight.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 20:08, 11 December 2012
Graph representing rocket dry and wet mass as function of the engine's thrust-to-weight ratio.
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 20:08, 11 December 2012 |  | 400 × 300 (4 KB) | Vincent (talk | 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. |
| 04:45, 1 November 2012 |  | 400 × 300 (4 KB) | Vincent (talk | contribs) | Graph representing rocket dry and wet mass as function of the engine's thrust-to-weight ratio. |
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