Advanced liquid rocket engine transient model-Reference-Cited by-同舟云学术

Advanced liquid rocket engine transient model

Published:1990-07-16 Issue: Volume: Page:
ISSN:
Container-title:26th Joint Propulsion Conference
language:
Short-container-title:

Author:

RUTH E.¹,AHN H.¹,BAKER R.¹,BROSMER M.¹

Affiliation:

1. Aerospace Corp., ElSegundo, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1990-2299

Reference8 articles.

1. Schuman, M. D., Webber W. T., Ervin, J., Taniguchi, M., and Wong, E. Y. C. "Transient Performance Program," Vol.1,AirForce Rocket Propnlsion Laboratory, Final Report AFRPLTR-80-22,1981.

2. Gordon, S. and McBride, B. J. "Computer Program for Calculation of Complex Chemical Equilibrium Compositions, Rocket Performance, Incident and Reflected Shocks, and Chapman-Jouguet Detonations,`` NASA Lewis Research Center, NASA SP-273, 1971.

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