File:Isp.png: Difference between revisions
From NPrize
Jump to navigationJump to search
m fix link |
uploaded a new version of "File:Isp.png": starting at 280 instead of 270 |
(No difference)
| |
Latest revision as of 20:59, 11 December 2012
Graph representing rocket dry and wet mass as function of the Isp. This is clearly exponential on the left because a too low Isp means that orbit cannot be reached, the mass ratio gets too high. Done with version 3 of File:Rocket mass.c. Delta V is 8300 m/s, overall thrust-to-weight ratio is 2.5.
File history
Yi efo/eka'e gwa ebo wo le nyangagi wuncin ye kamina wunga tinya nan
| Gwalagizhi | Nyangagi | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 20:59, 11 December 2012 |  | 400 × 300 (3 KB) | Vincent (Sọ̀rọ̀ | contribs) | starting at 280 instead of 270 |
| 20:52, 11 December 2012 |  | 400 × 300 (3 KB) | Vincent (Sọ̀rọ̀ | contribs) | Graph representing rocket dry and wet mass as function of the Isp. This is clearly exponential on the left because a too low Isp means that orbit cannot be reached, the mass ratio gets too high. Done with version 3 of File:Rocket_mass.c. Delta V is 8300 m |
You cannot overwrite this file.
File usage
The following page uses this file:
