Design and optimization of variable thrust hybrid rocket motors for sounding rockets

Author:

Rao DaLin,Cai GuoBiao,Zhu Hao,Tian Hui

Publisher

Springer Science and Business Media LLC

Subject

General Engineering,General Materials Science

Reference23 articles.

1. Chiaverini M J, Harting G C, Lu Y C, et al. Pyrolysis behavior of hybrid rocket solid fuels under rapid heating conditions. AIAA Paper 97-3078, 1997

2. Marxman G A, Gilbert M. Turbulent boundary layer combustion in the hybrid rocket. Ninth International Symposium on Combustion. New York: Academic Press, 1963. 371–383

3. Marxman G A. Boundary layer combustion in propulsion. Proceedings of the Eleventh (International) Symposium on Combustion. Pittsburgh, PA: Combustion Inst, 1967. 269–289

4. Marxman G A. Combustion in the turbulent boundary layer on a vaporizing surface. Tenth (International) Symposium on Combustion. Pittsburgh: Combustion Inst, 1965. 1337–1349

5. Smoot L D, Price C F. Regression rates of nonmetallized hybrid fuel systems. AIAA J, 1965, 3(8): 1408–1413

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