Development and testing of a vortex-driven, high-regression rate hybrid rocket engine
Author:
Affiliation:
1. Orbital Technologies Corp., Madison, WI
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3507
Reference4 articles.
1. Experimental investigation of a vortex-driven high-regression rate hybrid rocket engine
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