Combustion of condensed systems consisting of HMX and a binder capable of self-sustained combustion

Fizika Goreniya i Vzryva

Volumn 34, Issue 5, 1998, Pages 59-69

  Denisyuk, A P ^a   Shabalin, V S ^a   Shepelev, Y ^a  

^a NONE

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EID: 33748271757     PISSN: 04306228     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (19)

1. Sumi K., Kubota N., Andoh E., Shiromoto K. Gas-phase details of HMX based CMDB propellants // Proc. 12th Intern. Symp. Space Technol. and Sci. Tokyo, 1977. P. 483-488.
2. Kubota N., Okuhara H. Burning rate temperature sensitivity of HMX propellants // Chem. Abstr. 1989. V. 111. P. 152 (117793n).
3. Lengelle G., Bizot A. Combustion des differents propergols solides // Memorial de l'Artillerie francaise. 1986. T. 60, N 232. P. 157-211.
4. Kubota N. Role of additives in combustion waves and effect on stable combustion limit of double base propellants // Propellant and Explosives. 1978. V. 3, N° 6. P. 163-168.
5. The Fundamental Study of HMX Composite Propellant and its Practical Application / National Aerospace Lab., Tokyo (Japan). HMX Propellant Research Group // Scient. and Techn. Aerospace Reports («STAR»). 1986. V. 24, N 11. P. 1750. N 86-20582 (NAL-TR-875).
6. Kubota N. Physicochemical processes of HMX propellant combustion // 19th. Symp. (Intern.) Combustion. Haifa, Aug. 8-13, 1982. Pittsburgh, Pa, 1982. P. 777-784.
7. 1982. T. 20, N° 2. C. 115-126; AIAA Journal. 1982. V. 20, N 1. P. 106-115.
8. Fogelzang A. E., Pimenov A. Ju., Margolin A. D., Denisiuk A. P. Mechanism of modifying ballistic properties of propellant formulation by fast burning inclusions // Proc. Intern. Sem. on High Energy Materials, 19-20 Nov. 1996. Pune, India, 1996.