File:Overall thrust to weight.png: Revision history

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11 December 2012

1 November 2012

  • curprev 04:4704:47, 1 November 2012‎ Vincent Sọ̀rọ̀ contribs‎ 175 bytes +175‎ 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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