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基于弹丸最大碎片理论的碎片云模型
引用本文:郑建东,龚自正,席 爽,侯明强,徐坤博.基于弹丸最大碎片理论的碎片云模型[J].航天器环境工程,2012,29(4):397-400.
作者姓名:郑建东  龚自正  席 爽  侯明强  徐坤博
作者单位:1. 可靠性与环境工程技术重点实验室
2. 北京卫星环境工程研究所:北京100094
基金项目:国防科工局空间碎片专项(项目编号:KJSP06209)
摘    要:文章基于弹丸最大碎片理论,建立了一种新的碎片云模型。假设碎片云分为缓冲板碎片云、弹丸碎片云及弹丸最大碎片3个部分,而缓冲板碎片云和弹丸碎片云分别为2个大小不等的膨胀球壳,而弹丸最大碎片与这2个球壳头部相切。该模型与Schonberg模型和Swift模型的对比分析结果表明,新模型形式简单、精度高、适用范围广,可以有效指导航天器空间碎片防护结构设计与防护性能分析。

关 键 词:碎片云模型  超高速撞击  特征速度
收稿时间:7/5/2011 12:00:00 AM
修稿时间:2012/7/10 0:00:00

A new debris cloud model based on the largest fragment theory
Zheng Jiandong,Gong Zizheng,Xi Shuang,Hou Mingqiang and Xu Kunbo.A new debris cloud model based on the largest fragment theory[J].Spacecraft Environment Engineering,2012,29(4):397-400.
Authors:Zheng Jiandong  Gong Zizheng  Xi Shuang  Hou Mingqiang and Xu Kunbo
Institution:1.Science and Technology on Reliability and Environmental Engineering Laboratory;2.Beijing Institute of Spacecraft Environment Engineering: Beijing 100094,China)
Abstract:A new debris cloud model based on the largest fragment theory is put forward.It is assumed that the debris cloud is split into the debris cloud of bumper,the debris cloud of projectile and the largest fragment of projectile.All debris clouds originating from the projectile and the fragments originating from the bumper plate are evenly distributed on the surface of a big and a small expanding spherical shells,respectively.The largest fragment is located on the shot axis of the leading edge of the two spherical shells.The comparison of this new model with the Schonberg model and the Swift model shows that the new model is simple,accurate and applicable in a wide range.This model can provide an effective guidance for design and performance analysis of the spacecraft shielding structure.
Keywords:debris cloud model  hypervelocity impact  characteristic velocity
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