.. RocketCEA documentation master file
You can adapt this file completely to your liking, but it should at least
contain the root `toctree` directive.
.. include:: ../README.rst
See NASA CEA Documentation:
`CEA User Manual (NASA RP-1311).pdf <./_static/CEA_User_Manual_(NASA_RP-1311).pdf>`_
and
`CEA Methodology (NASA RP-1311).pdf <./_static/CEA_Methodology_(NASA_RP-1311).pdf>`_
.. note::
For those interested in using **RocketCEA** to design rocket thrusters,
there are two companion projects
`RocketIsp `_ and
`RocketProps `_.
`RocketIsp `_ uses a simplified JANNAF
approach to calculate delivered specific impulse (Isp) for liquid rocket thrust chambers.
`RocketProps `_
calculates the various liquid propellant properties required to analyse
a liquid propellant thrust chamber.
.. note::
On Windows, 32 bit python 3.8 and above are not supported.
As of this writing (10/5/2021) 64 bit python 3.10 requires Unofficial Binaries
to install numpy, scipy and matplotlib.
RocketCEA
=========
Contents:
.. toctree::
:maxdepth: 2
quickstart
installgfortran
std_examples
traditional_example
simple_examples
finite_area_comb
comb_species
engine_mr
propellant_select
propellants
new_propellants
plot_examples
ambient_isp
hydrazine_mono
temperature_adjust
cea_tdk_rpa
parasol_example
functions
copyright
authors
history
Indices and tables
==================
* :ref:`genindex`
* :ref:`modindex`
* :ref:`search`