Combustion of GAP/HMX and GAP/TAGN Energetic Composite Materials

Propellants, Explosives, Pyrotechnics

Volumn 25, Issue 2, 2000, Pages 86-91

  Kubota, Naminosuke ^a   Kuwahara, Takuo ^b  

^a MITSUBISHI ELECTRIC CORPORATION   (Japan)

^b Hosoya Kako Co Ltd   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0345846273     PISSN: 07213115     EISSN: None     Source Type: Journal    
DOI: 10.1002/(SICI)1521-4087(200004)25:2<86::AID-PREP86>3.0.CO;2-M     Document Type: Article

References (16)

1. N. Kubota, "Survey of Rocket Propellants and Their Combustion Characteristics", in: K. K. Kuo and M. Summerfield (eds), "Fundamentals of Solid-Propellant Combustion", Progress in Astronautics and Aeronautics, Vol. 90, AIAA, Washington, DC, 1984, Chap. 1.
2. I. Aoki and N. Kubota, "Combustion Wave Structures of High- and Low-Energy Double-Base Propellants", AIAA Journal 20, 100-106 (1982).
3. R. A. Fifer, "Chemistry of Nitrate Ester and Nitramine Propellants", in: K. K. Kuo and M. Summerfield (eds), ″Fundamentals of Solid-Propellant Combustion", Progress in Astronautics and Aeronautics, Vol. 90. AIAA, Washington, DC, 1984, pp. 177-237.
4. T. L. Boggs, "The Thermal Behavior of Cyclotrimethylenetrinitramie (RDX) and Cyclotetramethylenetetranitramine (HMX)", in: K. K. Kuo and M. Summerfield (eds), "Fundamentals of Solid-Propellant Combustion", Progress in Astronautics and Aeronautics, Vol. 90, AIAA, Washington, DC, 1984, Chap. 1, pp. 121-175.
5. N. Kubota and S. Sakamoto, "Combustion Mechanism of HMX," Propellants, Explosives, Pyrotechnics 14, 6-11 (1989).
6. N. Kubota, N. Hirata, and S. Sakamoto, "Combustion Mechanism of TAGN", Twenty-first Symposium (International) on Combustion, The Combustion Institute, 1986, pp. 1925-1931.
7. N. Kubota and T. Sonobe, "Combustion Mechanism of Azide Polymer", Propellants, Explosives, Pyrotechnics 13, 172-177 (1988).
8. N. Kubota, "Combustion of Energetic Azide Polymers", J. of Propulsion and Power 11(4), 677-682 (1995).
9. N. Kubota, "Flame Structure of Modern Solid Propellants", in: L. De Luca, E. W. Price, and M. Summerfield (eds), "Nonsteady Burning and Combustion Stability of Solid Propellants" Progress in Astronautics and Aeronautics, Vol. 143, AIAA, Washington, DC, 1991, Chap. 7.
10. N. Kubota and T. Masamoto, "Flame Structures and Burning Rate Characteristics of CMDB Propellants", Sixteenth Symposium (International) on Combustion, The Combustion Institute, Pittsburgh, PA, 1976, pp. 1201-1209.
11. Y. Yano and N. Kubota, "Combustion of HMX-CMDB Propellants (I)", Propellants, Explosives, Pyrotechnics 10, 192-196 (1985).
12. Y. Yano and N. Kubota, "Combustion of HMX-CMDB Propellants (II)", Propellants, Explosives, Pyrotechnics 11, 1-5 (1986).
13. N. Kubota and H. Okuhara, "Burning Rate Temperature Sensitivity of HMX Propellants", J. Propulsion and Power 5(4), 406-410 (1989).
14. N. S. Cohen, and D. A. Flanigan, "Mechanisms and Models of Solid-Propellant Burn Rate Temperature Sensitivity: A Review", AIAA Journal 23(10), 1538-1547 (1985).
15. R. L. Glick, "Temperature Sensitivity of Solid Propellant Burning Rate", AIAA Journal 5(3), 586-587 (1967).
16. N. Kubota, "Temperature Sensitivity of Solid Propellants and Affecting Factors: Experimental Results", in: L. De Luca, E. W. Price, and M. Summerfield (eds), "Nonsteady Burning and Combustion Stability of Solid Propellants", Progress in Astronautics and Aeronautics, Vol. 143, AIAA, Washington, DC, 1991, Chap. 4.