Solid rocket nozzle design summary
Author:
Affiliation:
1. AEROJET-GENERAL CORP., SACRAMENTO, CALIF.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1968-655
Reference29 articles.
1. Exhaust Nozzle Contour for Optimum Thrust
2. Correlation of performance of conical and contoured nozzles for gas-particle flow.
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