导弹与航天运载技术2024,Issue(6) :54-62.DOI:10.7654/j.issn.2097-1974.20240609

斜架发射适配器落点研究及增推设计

Adapter Drop Point Study and Boost Design for Oblique Fixed Launcher

刘越 王志浩 饶蔚巍 谢朝夕
导弹与航天运载技术2024,Issue(6) :54-62.DOI:10.7654/j.issn.2097-1974.20240609

斜架发射适配器落点研究及增推设计

Adapter Drop Point Study and Boost Design for Oblique Fixed Launcher

刘越 1王志浩 1饶蔚巍 2谢朝夕2
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作者信息

  • 1. 北京机电工程研究所,北京,100074
  • 2. 成都航旭智能装备科技有限公司,成都,610200
  • 折叠

摘要

针对斜架发射装置发射时对适配器出箱后分离落点问题,通过试验中各适配器落点情况,利用C编程复算适配器整个运动过程,预估了适配器在燃气流场中的冲击载荷和适配器落点,确定了落点问题的主要成因;首次利用富氮化合物(五氨基四唑)作为增推动力源,实现适配器分离的瞬时增推设计,通过运动仿真与试验,验证了增推装置应用原理的正确性和分离的有效性.

Abstract

When launching missiles from oblique fixed launcher,the adapter is out of the canister launcher after the separation of the falling point problem.Through the test of the adapter falling point situation,the use of C programming recalculate the adapter throughout the motion process.The adapter in the exhaust flow field of the exhaust force and the adapter falling point are,predicted.The main causes of the falling point problem are determined.For the first time,the nitrogen-rich compounds(penta-amino tetrazolium)is first used as a boosting force source to realize the separation of the adapter instantaneous boost design,.Through the motion simulation and testing,the research validates that the application of the principle of the boosting device is correct and the validity of the separation.

关键词

发射装置/适配器/运动/落点/增推装置

Key words

launcher/adapter/motion/falling point/boosting device

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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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