File:Isp.png

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Isp.png(400 × 300 pixels, file size: 3 KB, MIME type: image/png)

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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current22:59, 11 December 2012Thumbnail for version as of 22:59, 11 December 2012400 × 300 (3 KB)Vincent (talk | contribs)starting at 280 instead of 270
22:52, 11 December 2012Thumbnail for version as of 22:52, 11 December 2012400 × 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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