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硝胺复合固体推进剂燃速估算
引用本文:宋洪昌. 硝胺复合固体推进剂燃速估算[J]. 推进技术, 1989, 10(6): 38-45,72
作者姓名:宋洪昌
作者单位:华东工学院
摘    要:
本文讨论了硝胺炸药RDX、HMX的热分解及其对固体推进剂燃速的影响.提出了一种适用于AP/RDX(HMX)/HTPB(PU)/Al体系复合固体推进剂燃速预估的计算程序,计算结果与实测值十分吻合.

关 键 词:黑索今  奥克托今  热离解  复合推进剂  推进剂燃速  预测

PREDICTING BURNING RATE OF AMMONIUM NITRATE PROPELLANTS
Song Hongchang. PREDICTING BURNING RATE OF AMMONIUM NITRATE PROPELLANTS[J]. Journal of Propulsion Technology, 1989, 10(6): 38-45,72
Authors:Song Hongchang
Affiliation:Hua Dong Engineering Institute
Abstract:
In this paper the decomposition of RDX, HMX and the its influence on burning rate of solid propellants is discussed.A computer program to calculate the burning rate of AP/RDX(HMX)/HTPB(PU)/A1 composition prOpellants is presented. The quantitative predictions by the method under various propellant compositions and solid particle sizes appear to be basically in accordance with the exprimental results.
Keywords:Solid rocket engine   Ammonium nitrate propellant   Propellant burning rate   Prediction  
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