File:Rocket mass.c: Revision history

12 December 2012

• curprev 01:4201:42, 12 December 2012‎ Vincent Sọ̀rọ̀ contribs‎ 3,436 bytes 0‎ 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

11 December 2012

• curprev 13:3213:32, 11 December 2012‎ Vincent Sọ̀rọ̀ contribs‎ 3,436 bytes +552‎ v3 update
• curprev 13:2613:26, 11 December 2012‎ Vincent Sọ̀rọ̀ contribs‎ 2,884 bytes 0‎ 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.
• curprev 03:3603:36, 11 December 2012‎ Vincent Sọ̀rọ̀ contribs‎ 2,884 bytes +77‎ Adding the picture and few details

9 November 2012

• curprev 01:4501:45, 9 November 2012‎ Vincent Sọ̀rọ̀ contribs‎ 2,807 bytes +185‎ include images for tank model

7 November 2012

• curprev 18:4918:49, 7 November 2012‎ Vincent Sọ̀rọ̀ contribs‎ 2,622 bytes +392‎ →‎Features: mass ratio stuff
• curprev 18:2918:29, 7 November 2012‎ Vincent Sọ̀rọ̀ contribs‎ 2,230 bytes +1,873‎ documentation
• curprev 03:5103:51, 7 November 2012‎ Vincent Sọ̀rọ̀ contribs‎ 357 bytes 0‎ 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.

2 November 2012

• curprev 02:4702:47, 2 November 2012‎ Vincent Sọ̀rọ̀ contribs‎ 357 bytes +357‎ 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