Development of a N2O/HTPB hybrid rocket motor
Author:
Affiliation:
1. Lockheed Martin Manned Space Systems, New Orleans, LA
2. Environmental Aeroscience Corp., Miami, FL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2803
Reference5 articles.
1. Overview of Hybrid Sounding Rocket Program
2. A standardized technique for evaluating hybrid rocket motor performance
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