File:Engine thrust to weight.png: Difference between revisions
From NPrize
Jump to navigationJump to search
(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)
|
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.
File history
Click on a date/time to view the file as it appeared at that time.
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. |
You cannot overwrite this file.
File usage
The following page uses this file: