Effect of RDX and HMX on the efficiency of catalysts for double-base propellant combustion

Combustion, Explosion and Shock Waves

Volumn 37, Issue 2, 2001, Pages 190-196

  Denisyuk, A P ^a   Shepelev, Yu G ^a   Rusin, D L ^a   Shumskii, I V ^a  

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

Author keywords

[No Author keywords available]

Indexed keywords

EID: 23044525355     PISSN: 00105082     EISSN: None     Source Type: Journal    
DOI: 10.1023/A:1017561827203     Document Type: Article

References (11)

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2. G. Lengelle and A. Bizot, "Combustion des differents propergols solides," Memorial de l'Artillerie Francaise, 60, No. 232, 157-211 (1986).
3. A. A. Zenin, S. V. Finyakov, and V. M. Puchkov, et al., "Influence of HMX on the combustion mechanism of double-base propellants," Fiz. Goreniya Vzryva, 32, No. 3, 42-52 (1996).
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5. "The fundamental study of HMX composite propellent and its practical application," in: Scientific and Technical Aerospace Reports "STAR," No. 86-20582 (NALTR-875), National Aerospace Lab., HMX Propellent Research Group, Vol. 24, No. 11, Japan, Tokyo (1986), p. 1750.
6. N. Kubota, "Physicochemical processes of HMX propellant combustion," in: 19th Symp. (Int). Combustion (Haifa, August 8-13, 1982), Pittsburgh, PA (1982), pp. 777-784.
7. M. V. Backstead and K. P. Maccarthy, "Model calculations for HMX-based composite propellents," AIAA J., 20, No. 1, 106-115 (1982).
8. K. V. Raman and H. Singh, "Ballistic modification of RDX-based CMDB propellants," Propel., Explos., Pyrotech., 13, 149-151 (1988).
9. A. P. Denisyuk, L. A. Demidova, and V. I. Galkin, "Leading combustion zone of double-base propellants with catalysts," Fiz. Goreniya Vzryva, 31, No. 2, 32-40 (1995).
10. A. P. Denisyuk and A. E. Fogel'zang, "Temperature profiles in combustion of double-base propellants with abnormal pressure dependence of the burning rate," Izv. Vyssh. Uchebn. Zaved., Khim. Khim. Tekhnol., 14, No. 6, 861-864 (1971).
11. V. M. Mal'tsev and M. Summerfield, "Mechanism of the action of catalytic additives on double-base propellant combustion," Fiz. Goreniya Vzryva, 9, No. 1, 133-139 (1973).