File:Isp.png: Difference between revisions
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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.
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Date/Time | Thumbnail | Dimensions | User | Comment | |
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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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