File:Rocket mass.c: Difference between revisions

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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
 
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.
(No difference)

Revision as of 03:51, 7 November 2012

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 visible on the first approximations page.

File history

Yi efo/eka'e gwa ebo wo le nyangagi wuncin ye kamina wunga tinya nan

GwalagizhiDimensionsUserComment
current01:42, 12 December 2012 (21 KB)Vincent (Sọ̀rọ̀ | contribs)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 (20 KB)Vincent (Sọ̀rọ̀ | contribs)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 (14 KB)Vincent (Sọ̀rọ̀ | contribs)composite skirts, propellant venting and tank insulation (given data, not computed), mass ratio computed from delta V and Isp.
02:47, 2 November 2012 (12 KB)Vincent (Sọ̀rọ̀ | contribs)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