Propellant Effects on SRM Upper Stage Internal Ballistics and Performance with Nozzle Erosion Characterization
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American Institute of Aeronautics and Astronautics
Reference27 articles.
1. 1Bianchi, D., Nasuti, F., and Onofri, M. “Radius of Curvature Effects on Throat Thermochemical Erosion in Solid Rocket Motors,” AIAA 2012-533, Jan. 2012, 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Nashville.
2. 2Cavallini, E., Bianchi, D., Favini, B., DiGiacinto, M., andSerraglia, F. “InternalBallisticsModelingofHighPerformance SRMs with Coupled Nozzle Erosion Characterization,” AIAA 2011-5799, July 2011, 47thAIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 31July- 3 August2011, San Diego, CA.
3. 3Lenoir,J.M.andRobillard,G.“AMathematicalMethodtoPredicttheEffectsoftheErosiveBurninginSolidPropellant Rockets,” Proc. of the Sixth Symposium on Combustion, 1957, pp.663-667, New York.
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