Solid Propellant Grain Design
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Publisher
Elsevier
Reference24 articles.
1. DELANOY G. and LOUBERE, B., A physical method for predicting thrust imbalance of solid rocket motor pairs for a satellite launcher AIAA 87–1740, AIAA/ASEE/SAE/ASME 23rd Joint Propulsion Conference, 1987.
2. LEROUX, A. Y., RIBEREAU, D. and NAMAH, G., Numerical model for propellant grain burning. Conference on mathematical modeling of combustion and related topics. Ecole Centrale de Lyon, 1987.
3. Erosive burning of solid Propellants;RAZDAN;Fundamentals of solid Propellant, Combustion Progress in Astronautics and Aeronautics,1984
4. DELANNOY, G., Prediction of antitank solid propellant rocket internal ballistics. AIAA-84–1355. AIAA/SAE/ASME 20th Joint Propulsion Conference, 1984.
5. PHILIPPE, A. and TCHEPIDJIAN, P., Prediction of longitudinal combustion instabilities in axisymmetrical propellant grains. AIAA-84–1358. AIAA/SAE/ASME 20th Joint Propulsion Conference, 1984.
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