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Volumn 18, Issue 1, 2000, Pages 29-37

Combustion mechanism of the low signature propellant containing 1, 7-diazido-2, 4, 6-trinitrazaheptane(dath)

Author keywords

Burning rate; Burning surface; Combustion mechanism; Low signature (LS) propellant; Thermal decomposition

Indexed keywords


EID: 38749093612     PISSN: 07370652     EISSN: 15458822     Source Type: Journal    
DOI: 10.1080/07370650008216111     Document Type: Article
Times cited : (2)

References (10)
  • 1
    • 85023832594 scopus 로고
    • Modem Rocket Propulsion for Tactical Missiles: A Component for Future Missiles
    • Robert H Schmucker, "Modem Rocket Propulsion for Tactical Missiles: A Component for Future Missiles", Military Technology, 6, 1989
    • (1989) Military Technology , vol.6
    • Schmucker, R.H.1
  • 6
    • 85023867471 scopus 로고
    • Effect of Direct Chain Dzidonitramine on the Combustion Characteristics of Double-base Propellant
    • (in Chinese)
    • Li Shangwen, "Effect of Direct Chain Dzidonitramine on the Combustion Characteristics of Double-base Propellant", Propellant Technology, 5, 1995, (in Chinese)
    • (1995) Propellant Technology , vol.5
    • Li, S.1
  • 8
    • 0001624052 scopus 로고    scopus 로고
    • Combustion Mechanism of Glyciolyl Azide Polymer
    • Keiichi Hori and Motoyasu Kimura, "Combustion Mechanism of Glyciolyl Azide Polymer", Propellants, Explo., Pyrotech. 221, 160 (1996)
    • (1996) Propellants, Explo., Pyrotech , vol.221 , pp. 160
    • Hori, K.1    Kimura, M.2
  • 9
    • 0027641450 scopus 로고
    • Mechanism of Catalytic on AMMO/HMX Composite Propellants Combustion Rates
    • Yoshiaki Mitarai and Toshiyuki Auan, "Mechanism of Catalytic on AMMO/HMX Composite Propellants Combustion Rates", Propellants, Explosives .Pyrotechnics., 18, 195(1993)
    • (1993) Propellants, Explosives .Pyrotechnics. , vol.18 , pp. 195
    • Mitarai, Y.1    Auan, T.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.