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Volumn 13, Issue 1, 1971, Pages 1047-1056

The combustion of solid monopropellants and composite propellants

Author keywords

[No Author keywords available]

Indexed keywords


EID: 5544221005     PISSN: 00820784     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0082-0784(71)80103-0     Document Type: Article
Times cited : (79)

References (26)
  • 4
    • 85007219760 scopus 로고
    • A Model of Composite Propellant Combustion Including Surface Heterogeneity and Heat Generation
    • (1966) AIAA Journal , vol.4 , pp. 1629
    • Hermance1
  • 15
    • 83155172070 scopus 로고
    • Effects of Particle Size and Initial Temperature on the Deflagration of Ammonium Perchlorate
    • University of California, Berkeley
    • (1963) Ph.D. thesis
    • Shannon1
  • 17
    • 85007709843 scopus 로고
    • Correlations between deflagration characteristics and surface properties of nitramine-based propellants.
    • (1968) AIAA Journal , vol.6 , pp. 2107
    • Zimmer-Galler1
  • 18
    • 55449102993 scopus 로고
    • Role of Scanning Electron Microscopy in the Study of Solid Propellant Combustion:* Part III. The Surface Structure and Profile Characteristics of Burning Composite Solid Propellants
    • (1970) Combustion Science and Technology , vol.1 , pp. 369
    • Derr1    Boggs2
  • 19
    • 0014738883 scopus 로고
    • Deflagration rate, surface structure, and subsurface profile of self-deflagrating single crystals of ammonium perchlorate
    • (1970) AIAA Journal , vol.8 , pp. 370
    • Boggs1    Derr2    Beckstead3
  • 23
    • 84914365640 scopus 로고    scopus 로고
    • Lockheed Propulsion Company, unpublished data, 1969.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.