Investigation of Liquid Breakup Process in Solid Rocket Motor
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Published:2023
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Page:11
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Container-title:Proceeding of 10th International Symposium on Turbulence, Heat and Mass Transfer, THMT-23, Rome, Italy, 11-15 September 2023
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Reference16 articles.
1. Xiao, Y., Amano, R., 2006, 'Aluminized Composite Solid Propellant Particle Path in The Combustion Chamber of A Solid Rocket Motor,' WIT Transactions on Engineering Sciences, 52, pp. 153-164. 2. Rapp, D., 1990, 'High Energy-Density Liquid Rocket Fuel Performance,' in 26th Joint Propulsion Conference, Orlando, FL, USA, pp. 1967-1968. 3. Amano, R. S., Yen, YH, and Hamman, Michael L., 2014, 'Solid-Fuel Rocket Motor Efficiency Improvement Scheme,' Novel Combustion Concepts for Sustainable Energy Development. Springer, New Delhi. 4. Thakre, P., Yang, V., 2009, 'Chemical erosion of refractory-metal nozzle inserts in solid-propellant rocket motors,' Journal of Propulsion and Power, 25(1), pp. 40-50. 5. Wong, E., 1968, 'Solid rocket nozzle design summary,' In 4th Propulsion Joint Specialist Conference, pp. 654-655.
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