Space Shuttle Main Engine

Rocket Propulsion

0910412 / 0910512

 

NASA Chemical Equilibrium Analysis Code

Computer Program for Calculation of Complex Chemical Equilibrium
Compositions, Rocket Performance, Incident and Reflected Shocks,
and Chapman-Jouget Detonations

Sanford Gordon and Bonnie McBride
NASA Glenn Research Center
21000 Brookpark Rd.
Cleveland, OH 44135

References:
NASA SP-273, 1971
NASA RP-1311, PART I, 1994
NASA RP-1311, PART II, 1996

home and objectives

 

You can download the necessary files to run the program here:

fcea2.exe

thermo.inp

thermo.lib

trans.lib

cea2.inp

The executable is called fcea2.exe. Thermo.lib and trans.lib are libraries that are needed to run the code.  thermo.inp is a text file that contains all of the species currently available in the code.  cea2.inp is an input file with a variety of sample problems outlined.

To run the code, just click on the executable and it will open up a .dos shell.  The program will prompt you for an input data file.  Type in the file name, without an extention.  The program will generate an output file name called <filename.out>.

For more information and to download the code directly from NASA visit the NASA CEA Website:

http://www.grc.nasa.gov/WWW/CEAWeb/


Example input files from week 6 notes:

arcjetn2h4.inp       h2o2hp.inp       h2o2rocket.inp      h2o2rocket2.inp

course outline and notes

homework assignments

NASA CEA Code

rocket of the week

links and combustion research

rules and grading

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Contact  marchese@rowan.edu with questions, problems or comments.
©2005 Anthony J. Marchese.