Solid-propellant erosive burning
Author:
Affiliation:
1. Office National d'Etudes et de Recherches Aerospatiales, BP72, F-92322 Chatillon Cedex, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.23544
Reference25 articles.
1. A mathematical method to predict the effects of erosive burning in solid-propellant rockets
2. Experimental Investigation of Propellant Erosion
3. Model Describing the Erosive Combustion and Velocity Response of Composite Propellants
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