File:Final acceleration.png: Difference between revisions
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(Graph representing final acceleration and engine's thrust as function of the initial acceleration (overall thrust-to-weight ratio).) |
(uploaded a new version of "File:Final acceleration.png": Updated with version 3 of File:Rocket_mass.c. Delta V is 8300 instead of 9000 m/s too.) |
(No difference)
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Latest revision as of 20:04, 11 December 2012
Graph representing final acceleration and engine's thrust as function of the initial acceleration (overall thrust-to-weight ratio).
File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 20:04, 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. |
| 01:41, 2 November 2012 |  | 400 × 300 (5 KB) | Vincent (talk | contribs) | Graph representing final acceleration and engine's thrust as function of the initial acceleration (overall thrust-to-weight ratio). |
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