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Combined display of all available logs of NPrize. You can narrow down the view by selecting a log type, the username (case-sensitive), or the affected page (also case-sensitive).
- 01:42, 12 December 2012 Vincent Sọ̀rọ̀ contribs uploaded a new version of File:Rocket mass.c (clarification about the propellant mass. vehicle_wet_mass is the dry mass + the burnt propellant mass, but it doesn't include the propellant taken aboard and evaporated during the ascent. The output indicates the ground value now. This is still version 3.)
- 13:26, 11 December 2012 Vincent Sọ̀rọ̀ contribs uploaded a new version of File:Rocket mass.c (Refining the model: better structure, more realistic fairing, adding forgotten pipes and valves, tanks alignment on outer shell, composite skirts for non-structural or soft tanks.)
- 03:51, 7 November 2012 Vincent Sọ̀rọ̀ contribs uploaded a new version of File:Rocket mass.c (composite skirts, propellant venting and tank insulation (given data, not computed), mass ratio computed from delta V and Isp.)
- 02:47, 2 November 2012 Vincent Sọ̀rọ̀ contribs uploaded File:Rocket mass.c (Program that iterates to compute an SSTO rocket's dry and wet mass (and other parameters). Compile with gcc -O2 -Wall rocket_mass.c -o rocket_mass -lm for normal use, and add -DMAKE_GRAPH after gcc on the command line if you want to create graph data as )
