Solid propellant erosive burning

Author:

GODON J.1,DUTERQUE J.1,LENGELLE G.1

Affiliation:

1. ONERA, Chatillon-sous-Bagneux, France

Publisher

American Institute of Aeronautics and Astronautics

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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1. Excessive Subsurface Heat Release As a Possible Cause of the Negative Erosion Effect during Combustion of Homogeneous Solid Propellants;Combustion, Explosion, and Shock Waves;2022-12

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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