File:Overall thrust to weight.png: Difference between revisions

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(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.)
 
(uploaded a new version of "File:Overall thrust to weight.png": Updated with version 3 of File:Rocket_mass.c. Delta V is 8300 instead of 9000 m/s too.)
 
(No difference)

Latest revision as of 20:06, 11 December 2012

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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current20:06, 11 December 2012Thumbnail for version as of 20:06, 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.
04:47, 1 November 2012Thumbnail for version as of 04:47, 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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