Art

J-GLOBAL ID：200902104174377164   Reference number：98A0325974

Propellants. Burning rate characteristics of energetic CMDB propellants(III). Effect of initial propellant temperature.

プロペラント 高エネルギCMDB推進薬の燃焼速度特性 (III) 推進薬初期温度の効果

Author (1)： AOKI ICHIRO (日産自動車 研開セ)
Material： 火薬学会誌  (Journal of the Japan Explosives Society)
Volume： 59  Issue： 1  Page： 36-43  Publication year： Jan. 1998 
JST Material Number： F0476A  ISSN： 1340-2781  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： JAPANESE (JA)

Thesaurus term： *double-base propellant ,...
Semi thesaurus term： octogen ,...

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JST classification (2)： Various explosives and propellants  (YE06020W) ,  Combustion in general  (XE04010W)

Reference (22)：

• GRICK, R. L. Temperature Sensitivity of Solid Propellant Burning Rate. AIAA Jouranal. 1967, 5, 586-587
• KUBOTA, N. Temperature Sensitivity of Double-Base Propellants. Proceedings of 8th JANNAF Combustion Meeting. 1971, 1, 387
• SUMMERFIELD, M. Theory of Dynamic Extinguishment of Solid Propellants with Special Reference to Nonsteady Heat Feedback Law. Journal of Spacecraft and Rockets. 1971, 8, 251-258
• COHEN-NIR, E. Temperature Sensitivity of the Burning Rate of Composite Solid Propellants. Combustion Science and Technology. 1974, 9, 183-194
• CAVENY, L. H. Influence of Thermal Radiation on Solid Propellant Burning Rate. AIAA Jouranl. 1975, 13, 202

Terms in the title (4)： 高エネルギ ,  推進薬 ,  燃焼速度 ,  初期温度