Charge Geometry and Ballistic Parameters for Solid Propellant Rocket Motors
Author:
Affiliation:
1. U. S. Naval Ordnance Test Station, Inyokern, China Lake, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.6440
Reference3 articles.
1. Theory of Steady Flow with Mass Addition Applied to Solid Propellant Rocket Motors
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