Author:
Ning He,Yude Liu,Hongpeng Zhang,Chunpeng Li
Reference6 articles.
1. Babuk, V.A., Vassiliev, V.A., Sviridov, V.V, 2001. Propellant Formulation Factors and Metal Agglomeration in Combustion of Aluminized Solid Rocket Propellan. Combustion Science and Technology 163,p.261-289.
2. Sun, Y., Li, S, 2006. Combustion Characteristics of Coated Nano Aluminium in Composite Propellants. Defence Science Journal 56.
3. Jianhong, Y., Jinglong, X, 2006. Calculation of TNT Equivalence of High Energy Propellant. Computer Simulation 23,P. 992-1003.
4. Clark, T., Woodley, R., De Halas, D., 1962. Gas-Graphite Systems, in “Nuclear Graphite” R. Nightingale, Editor. Academic Press, New York, p. 387.
5. Song, D., Pan, G., Wang, N, 2006. Calculational Model of Pyrotechnical Combustion Products Based on Minimum Free Energy. Journal of Projectiles, Rockets, Missiles and Guidance 1, P.61-63.
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