| 高氯酸铵／硝胺推进剂冲击感度研究 |
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| 引用本文： | 刘德辉. 高氯酸铵／硝胺推进剂冲击感度研究[J]. 固体火箭技术, 1992, 0(1): 61-65 |
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| 作者姓名： | 刘德辉 |
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| 作者单位： | 国防科学技术大学 湖南长沙 |
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| 摘 要： | 对高氯酸铵/硝胺推进剂冲击感度的研究结果表明,在丁羟推进剂中加入黑索今(RDX),可使其冲击感度增大,但RDX加入量增大,则其冲击感度增大的幅度却逐渐下降。研究还表明铝粉对推进剂的冲击感度也有影响。
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| 关 键 词： | 固体推进剂 无烟推进剂 推进剂 |
STUDY OF THE IMPACT SENSITIVITY OF AMMONIUM PERCHLORATE/NITRAMINE PROPELLANT |
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| Liu Dehui National University of Defence Technology,Changsha,Hunan. STUDY OF THE IMPACT SENSITIVITY OF AMMONIUM PERCHLORATE/NITRAMINE PROPELLANT[J]. Journal of Solid Rocket Technology, 1992, 0(1): 61-65 |
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| Authors: | Liu Dehui National University of Defence Technology Changsha Hunan |
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| Affiliation: | Liu Dehui National University of Defence Technology,Changsha,Hunan,410073 |
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| Abstract: | Impact sensitivity of ammonium perchlorate/nitramine propellant isstudied and the results indicate that adding hexogen (RDX) to HTPB propellant canmake impact sensitivity of HTPB propellant increase; however, the incresement of theimpact sensitivity become less as more RDX is added. It is also shown that aluminiumpowder exerts an effect upon the impact sensitivity of the propellant. |
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| Keywords: | Solid rocket propellant Smokeless propellant Propellant sensitivity Nitramine expolosive Hexogen |
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