Solid propellant erosive burning
Author:
Affiliation:
1. ONERA, Chatillon-sous-Bagneux, France
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-2031
Reference40 articles.
1. 1000 2000 3000 4000 5000 6000 70
2. 1-AluminizedAPICTPB13MPa,11mmlsl 2 -90pmAPICTPB 15MPa,10mmls) 3- 5pm APICTPB 16MPa,27mmls) i g .3 Measured erosive burning on composite
3. 2500-2350-2200
4. -+ 19oo.z ?!2175061450 c 1600-'8
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2. Erosive Burning Model Predictions and Laboratory Test Data: A Retrospective;AIAA Propulsion and Energy 2020 Forum;2020-08-17
3. Solid-Propellant Rocket Motors;Powered Flight;2012
4. Parametric Evaluation of Solid Rocket Motor Internal Ballistics;46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2010-07-25
5. Model for Prediction of Negative and Positive Erosive Burning;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09
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