File:Engine thrust to weight.png

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Engine_thrust_to_weight.png(400 × 300 pixels, file size: 4 KB, MIME type: image/png)

Graph representing rocket dry and wet mass as function of the engine's thrust-to-weight ratio.

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current22:08, 11 December 2012Thumbnail for version as of 22:08, 11 December 2012400 × 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.
06:45, 1 November 2012Thumbnail for version as of 06:45, 1 November 2012400 × 300 (4 KB)Vincent (talk | contribs)Graph representing rocket dry and wet mass as function of the engine's thrust-to-weight ratio.
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