complexe chemical equilibrium and rocket performance calcultaions
Cpropep-Web is a cgi interface to Cpropep. This software is also
available as a command line program.
Cpropep is a propellant evaluation software that will let you compute
rocket motor performance in function of the propellant. It works like
the known software `propep' but is code in standard C, is in
development and is supported. There is more information about this
project on the Rocket
Workbench home page.
Cpropep can compute chemical equilibrium for a
fixed temperature and pressure points, adiabatic flame temperature,
frozen and shifting equilibrium rocket performance evaluation.
To compute an equilibrium, you just have to specify up to tree
ingredient. You have to identify them by their number. To have the
list of the code, click on `List molecule codes'. The quantity can be
in gram or in moles.
The default value are for KClO4/HTPB/Al propellant.
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