Art
J-GLOBAL ID:200902130114813845   Reference number:96A0169809

Thermal decomposition of phase-stabilised ammonium nitrate(PSAN), hydroxyl-terminated polybutadiene(HTPB) based propellants. The effect of iron(III) oxide burning-rate catalyst.

相安定化した硝酸アンモニウム(PSAN),ヒドロキシル基末端ポリブタジエン(HTPB)ベース推薬の熱分解 酸化鉄(III)燃焼速度触媒の効果
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Volume: 269/270  Page: 273-293  Publication year: Dec. 20, 1995 
JST Material Number: E0350C  ISSN: 0040-6031  Document type: Article
Article type: 原著論文  Country of issue: Netherlands (NLD)  Language: ENGLISH (EN)
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Rocket engines  ,  Chemical analysis in general 

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