eb05416991
Taken from sources in CVS at:
https://sourceforge.net/projects/rocketworkbench/
Sources extracted in two steps:
1. Pull entire project tree into a subdir "rwb" via "rsync":
rsync -a a.cvs.sourceforge.net::cvsroot/rocketworkbench/ rwb/.
2. Export sources:
export CVSROOT=$(pwd)/rwb
SUBDIRS="analyser cpropep cpropep-web CVSROOT data libcompat libcpropep libnum libsimulation libthermo prop rocketworkbench rockflight"
mkdir rwbx; cd rwbx
cvs export -D now ${SUBDIRS}
After this (and some backups for safety), the directory content was
added to a Git repo:
git init .
git add *
15 lines
403 B
Plaintext
15 lines
403 B
Plaintext
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Propellant
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+oxidant 686 Oxygene
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+fuel 673 Octane
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+o/f 2.55 O/F ratio
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Parameter
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+chamber_pressure 500 psi The chamber pressure
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+thrust 30000 N The thrust we are looking for
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+L* 45 in The characteristic chamber length
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+Dc/Dt 2.34 Chamber diameter / Throat diameter
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+theta 20 deg Convergent half angle
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+r_rt 1.5
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