File:Overall thrust to weight.png

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Overall_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 vehicle (overall) initial thrust-to-weight ratio. There is an equivalence with the acceleration in number of G's.

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current22:06, 11 December 2012Thumbnail for version as of 22:06, 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.
06:47, 1 November 2012Thumbnail for version as of 06:47, 1 November 2012400 × 300 (4 KB)Vincent (talk | contribs)Graph representing rocket dry and wet mass as function of the vehicle (overall) initial thrust-to-weight ratio. There is an equivalence with the acceleration in number of G's.
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