Response functions of HMX and RDX burning rates with allowance for melting

Combustion, Explosion and Shock Waves

Volumn 43, Issue 3, 2007, Pages 309-319

  Zenin, A A ^a   Finjakov, S V ^a  

^a SEMENOV INSTITUTE OF CHEMICAL PHYSICS   (Russian Federation)

Author keywords

Burning rate; Melting; Response functions; Sensitivity of wave parameters

Indexed keywords

BURNING RATE; RESPONSE FUNCTIONS; SENSITIVITY OF WAVE PARAMETERS;

ERROR ANALYSIS; GASIFICATION; MELTING; PRESSURE CONTROL;

EXPLOSIVES;

EID: 34250206650     PISSN: 00105082     EISSN: 15738345     Source Type: Journal    
DOI: 10.1007/s10573-007-0044-z     Document Type: Article

References (34)

1. B. V. Novozhilov, "Theory of unsteady combustion of homogeneous gunpowders," Fiz. Gorvniya Vzryva, 4, No. 4, 482-493 (1968).
2. B. V. Novozhilov, Unsteady Combustion of Solid Propellants [in Russian], Nauka, Moscow (1973).
3. F. E. C. Culick and V. Yang, "Prediction of the stability of unsteady motions in solid-propellant rocket motors," in: L. De Luca, E. W. Price, and M. Summerfield (eds.), Progress in Astronautics and Aeronautics, Vol. 143: Combustion Stability of Solid Propellants, AIAA, Washington (1992), pp. 719-780.
4. L. De Luca, "Theory of nonsteady burning and combustion stability of solid propellants by flame model," ibid., pp. 519-600.
5. B. V. Novozhilov, M. Kohno, H. Maruizumi, and T. Shimara, "Solid propellant burning rate response functions of higher orders," The Inst. of Space and Astronaut. Sci. Report No. 661, Kanagava (1996).
6. C. M. Mihlfeith, A. D. Baer, and N. W. Ryan, "The response of a burning propellant surface to thermal radiation," AIAA J., 10, No. 10, 1280-1285 (1972).
7. J. C. Finlinson, D. Hanson-Parr, S. F. Son, and M. Q. Brewster, "Measurement of propellant combustion response to sinusoidal radiant heat flux," AIAA Paper No. 91-0204 (1991).
8. V. E. Zarko, V. N. Simonenko, and A. B. Kiskin, "Radiation-driven transient burning: Experimental results," in: L. De Luca, E. W. Price, and M. Summerfield (eds.), Progress in Astronautics and Aeronautics, Vol. 143: Nonsteady Burning and Combustion Stability of Solid Propellants, AIAA, Washington (1992), pp. 363-398.
9. T. A. Litzinger, C. J. Tang, G. Kudra, and Y. J. Lee, "A study of the combustion response of HMX monopropellant to sinusoidal laser heating," in: Proc. 33rd JANNAF Combustion Meeting, CPIA Publ. No. 653, Vol. II (1996), pp. 159-168.
10. M. Q. Brewster and T. B. Schroeder, "Laser-recoil combustion response of RDX," Combust. Sci. Technol., 122, 363-381 (1997).
11. J. C. Finlinson, R. A. Stalnaker, and F. S. Blomshield, "HMX and RDX T-burner pressure coupled response from 200 to 1000 psi," AIAA Paper No. 98-0556 (1998).
12. S. R. Hickman and M. Q. Brewster, "Laser-recoil response of AP-HPTB propellants," AIAA Paper No. 99-0592 (1999).
13. J. C. Finlinson and F. S. Blomshield, "HMX T-burner pressure coupled response at 200, 500, and 1000 psi," in: K. K. Kuo and L. T. De Luca (eds.), Combustion of Energetic Materials, Begell House, New York (2002), pp. 854-866.
14. F. Cauty, "Solid propellant response functions from direct measurement methods: A review of ONER A experience," in: Materials of Int. Workshop on Combustion Instability of Solid Propellants and Rocket Motors, Milan (1997).
15. M. K. King, "Composite propellant combustion modeling: pressure coupled response functions," AIAA Paper No. 80-1124 (1980).
16. E. W. Price, "Experimental observations of combustion instability," in: K. K. Kuo and M. Summerfield (eds.), Progress in Astronautics and Aeronautics, Vol. 90: Fundamentals of Solid-Propellant Combustion, AIAA, New York (1984), pp. 733-790.
17. J. S. T'ien, "Theoretical analysis of combustion instability," ibid., pp. 791-840.
18. W. W. Erikson and M. W. Beckstead, "Modeling unsteady monopropellant combustion with full chemical kinetics," AIAA Paper No. 98-0804 (1998).
19. M. W. Beckstead and W. W. Erikson, "Combustion instability of solid monopropellant," in: Proc. 33rd JANNAF Combustion Meeting, CPIA Publ. No. 653, Vol. II, Laurel (1996), pp. 145-157.
20. K. Prasad, M. A. Tanoff, M. D. Smooke, and R. A. Yetter, "Modelling of deflagration of HMX at high pressures," ibid., pp. 557-568.
21. S. V. Finjakov, "Response functions of the burning rate to pressure oscillations with allowance for melting of the burning surface," Khim. Fiz., 22, No. 9, 59-66 (2003).
22. A. A. Zenin and S. V. Finjakov, "Burning-rate response functions of nitramine-based propellants and HMX from microthermocouple data measurements," Combust. Expl., Shock Waves, 36, No. 1, 10-20 (2000).
23. A. A. Zenin and S. V. Finjakov, "Burning-rate response functions of composite-modified double-based propellants and HMX," in: V. Yang, T. B. Brill, and W.-Z. Ren (eds.), Progress in Astronautics and Aeronautics, Vol. 185: Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics, AIAA, Reston, Virginia (2000), pp. 639-662.
24. A. A. Zenin and S. V. Finjakov, "Characteristic features of burning-rate response functions: A review," in: K. K. Kuo and L. T. De Luca (eds.), Combustion of Energetic Materials, Begell House, Inc., New York (2002), pp. 837-853.
25. V. N. Simonenko, A. B. Kiskin, V. E. Zarko, and A. G. Svit, "Special features of nitramine combustion at atmospheric pressure," Combust., Expl., Shock Waves, 33, No. 6, 685-687 (1997).
26. V. N. Simonenko, V. E. Zarko, and A. B. Kiskin, "Characterization of self-sustaining combustion of cyclic nitramines," in: Energetic Materials, Proc. 29th Int. Annu. Conf. of ICT, Karlsruhe (1998), pp. 169(1)-169(14).
27. L. K. Gusachenko, V. E. Zarko, and A. D. Rychkov, "Effect of melting on dynamic combustion behavior of energetic materials," J. Propuls. Power, 15, No. 6, 816-822 (1999).
28. F. Cozzi, L. T. DeLuca, and B. V. Novozhilov, "Linear stability and pressure-driven response function of solid propellants with phase transition," ibid., pp. 806-815.
29. A. A. Zenin, V. M. Puchkov, and S. V. Finjakov, "Characteristics of HMX combustion waves at various pressures and initial temperatures," Combust., Expl., Shock Waves, 34, No. 2, 170-176 (1998).
30. A. A. Zenin, "Experimental study of the solid propellant combustion mechanism and the flow of combustion products," Doct. Dissertation in Phys.-Math. Sci., Moscow (1976).
31. S. V. Finjakov, "Study of the mechanism of powder combustion with a flow past the burning surface," Candidate Dissertation in Phys.-Math. Sci., Moscow (1992).
32. A. A. Zenin and S. V. Finjakov, "Characteristics of octogen and hexogen combustion: A comparison," in: Energetic Materials, Proc. 37th Int. Annu. Conf. of ICT, Karlsruhe (2006), pp. 154(1)-154(18).
33. T. L. Boggs, "The thermal behavior of cyclotrimethylenetrinitramine (RDX) and cyclotetramethylenetetranitramine (HMX)," in: K. K. Kuo and M. Summerfield (eds.), Progress in Astronautics and Aeronautics, Vol. 90: Fundamentals of Solid-Propellant Combustion, Academic Press, New York (1984), pp. 121-175.
34. B. V. Novozhilov, "Acoustic resonance upon propellant combustion," Combust., Expl., Shock Waves, 36, No. 1, 3-9 (2000).