An RL10A-3-3A rocket engine model using the Rocket Engine Transient Simulator (ROCETS) software
Author:
Affiliation:
1. Sverdrup Technology, Inc., Brook Park, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-2357
Reference16 articles.
1. Modeling Space Engines,AIAAPapcr 91-3556, September 1991.
2. Macmillan Company 1956.
3. Bartz,D.R., A SimplifiedEquutionforRupid Estimation ofRocket Nozzle Convective Heat Transfer Coefficients,JetPropulsionVo 1.27, pp.29-51, 1957.
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