Mechanism of modifying ballistic properties of propellant formulations by fast-burning inclusions

Defence Science Journal

Volumn 48, Issue 4, 1998, Pages 357-364

  Fogelzang, A E ^a   Pimenov, A Yu ^a   Denisyuk, A P ^a   Margolin, A D ^b  

^a MENDELEEV UNIVERSITY OF CHEMICAL TECHNOLOGY OF RUSSIA   (Russian Federation)

^b SEMENOV INSTITUTE OF CHEMICAL PHYSICS   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 11544257412     PISSN: 0011748X     EISSN: None     Source Type: Journal    
DOI: 10.14429/dsj.48.3962     Document Type: Article

References (8)

1. Caveny, L.H. & Pittman, C.U. (Jr.) Contribution of solid phase heat release to ammonium perchlorate composite propellant burning rate. AIAA Journal, 1968, 6 (8), 1461-67.
2. Kawamura, Kazuro. Influence of copper oxide catalysts on the burning rate of a composite propellant. J. Indus Explo Soc. Japan, 1989, 50 (5), 415-24.
3. Robson, J.H. Composite polysulshide propellants containing additives for producing extremely fast burning. USA Patent 3, 276, 926. 8 January 1953. 2p.
4. Matsubara, H. Methods of producing propellant grain adapted for single stage rockets. USA Patent 3, 300, 549. 13 April 1964. 5 p.
5. Matsubara, H. Feststofflreibsatz und Verfahren zu dessen Merstellund. German Patent 1, 287, 493. 1 October 1963, 8p.
6. Fogelzang, A.E., et al. FLAME: Database on Combustion of Explosives and Propellants. Version 2.50. Moscow, Russia, 1996.
7. Leibenzon, L.S. Natural liquid and gas flows in porous medium. Gostoptekhizdat, Moscow, 1947 (in Russian).
8. Zel'dovich, Ya. B. Theory of steady-state flame propagation limit. Zhurnal Experimentalnoi Teoreticheskoi Fiziki, 1941, 11, 159-69 (in Russian).