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弹托与火箭的粘连特性研究分析
引用本文:曹听荣,张福祥.弹托与火箭的粘连特性研究分析[J].弹道学报,1991(3).
作者姓名:曹听荣  张福祥
作者单位:华东工学院102室 (曹听荣),华东工学院102室(张福祥)
摘    要:火箭同时离轨发射技术研究的一个重要问题是,火箭离轨后弹托分离不一致所造成的火箭起始弹道偏差定量计算.本文介绍了弹托与火箭粘连期力学模型、弹托对火箭的干扰力的计算公式和弹托分离不一致引起的火箭散布的计算方法。

关 键 词:发射技术  外弹道  火箭

RESEARCH AND ANALYSIS OF ADHESIVE PROPERTY BETWEEN SABOT AND ROCKET
Cao ting rong,Zhang Fu xiang.RESEARCH AND ANALYSIS OF ADHESIVE PROPERTY BETWEEN SABOT AND ROCKET[J].Journal of Ballistics,1991(3).
Authors:Cao ting rong  Zhang Fu xiang
Affiliation:Cao ting rong;Zhang Fu xiang
Abstract:An important Study problem of rocket gun non-tip--off launching technology is the quantita-tive analysis for disturbance of rocket starting flight resulting from the non-synchronization of sabots sep-aration after rocket leaving the laucher. In this paper, mechanics model of adhesion phase between sabotand rocket, and computational formulas of rocket disturbance force because of sabot, and method ofcomputing rocket scatter due to the non -synchronication of sabot separation by means of rocker exteriorballistic equation are infroduced.
Keywords:Launching Technology  Rockets  Exterior Ballistics  
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