导弹与航天运载技术2024,Issue(6) :63-68.DOI:10.7654/j.issn.2097-1974.20240610

快速响应火箭星箭接口优选模式研究

Research on the Optimal Mode of Satellite-rocket Interface for Rapid Response Rocket

潘亮 李成 杨晓论 潘建平 张智宇
导弹与航天运载技术2024,Issue(6) :63-68.DOI:10.7654/j.issn.2097-1974.20240610

快速响应火箭星箭接口优选模式研究

Research on the Optimal Mode of Satellite-rocket Interface for Rapid Response Rocket

潘亮 1李成 1杨晓论 1潘建平 1张智宇1
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作者信息

  • 1. 太原卫星发射中心,太原,030031
  • 折叠

摘要

星箭接口是影响快响发射成功与否的重要因素,以快速响应固体火箭为研究对象,在提出快速响应火箭星箭接口总体要求的基础上,对其星箭接口特别是机械接口和电气接口展开分析,探究适合快速响应火箭的星箭接口优选模式,得出采用记忆合金驱动的点式星箭连接解锁装置和无线充电不预留充电接口的结论,并对如何推广运用快速响应火箭星箭接口优选模式提出建议,可为提高快响发射的可靠性和工作效率提供借鉴和参考.

Abstract

The satellite-rocket interface is an important factor affecting the success of rapid response launches.Rapid response solid rocket is taken as the research object.On the basis of proposing the general requirements of the satellite-rocket interfaces for rapid response rocket,the satellite-rocket interface is analyzed focusing on mechanical interface and electrical interface,the optimal mode of satellite-rocket interface for rapid response rocket is explored.It is concluded that the memory alloy-driven point satellite-rocket connection unlocking device and wireless charging do not reserve a charging interface.The research provides suggestions on how to promote the use of optimal model of satellite rocket interface for rapid response rocket,and provides reference for improving the reliability and efficiency of rapid response launches.

关键词

快响发射/快响火箭/星箭接口/机械接口/电气接口

Key words

rapid response launch/rapid response rocket/satellite rocket interface/mechanical interface/electrical interface

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出版年

2024
导弹与航天运载技术
中国运载火箭技术研究院

导弹与航天运载技术

CSTPCD北大核心
影响因子:0.238
ISSN:1004-7182
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