File:Isp.png: Difference between revisions
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(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) |
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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. | 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. | ||
Revision as of 20:54, 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.
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 20:59, 11 December 2012 |  | 400 × 300 (3 KB) | Vincent (talk | contribs) | starting at 280 instead of 270 |
| 20:52, 11 December 2012 |  | 400 × 300 (3 KB) | Vincent (talk | 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 |
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