File:Rocket mass.c

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Revision as of 03:47, 2 November 2012 by Vincent (talk | 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 )
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Rocket_mass.c(file size: 21 KB, MIME type: text/x-c)
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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 visible on the first approximations page.

File history

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Date/TimeDimensionsUserComment
current02:42, 12 December 2012 (21 KB)Vincent (talk | 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.
14:26, 11 December 2012 (20 KB)Vincent (talk | 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.
04:51, 7 November 2012 (14 KB)Vincent (talk | contribs)composite skirts, propellant venting and tank insulation (given data, not computed), mass ratio computed from delta V and Isp.
03:47, 2 November 2012 (12 KB)Vincent (talk | 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
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