噪声与振动控制2019，Vol.39Issue(3)：118-121,4.DOI:10.3969/j.issn.1006-1355.2019.03.023
运载火箭前端测控设备减振隔噪技术研究
Study on the Vibration Absorption and Noise Insulation of Measurement and Control Equipment of Launch Vehicles
潘玉竹 1贾学军 1张国栋 1范虹 1郭金刚2
作者信息
- 1. 北京航天发射技术研究所,北京 100076
- 2. 北京宇航系统工程研究所,北京 100076
- 折叠
摘要
Abstract
To adapt for the three-verticalness mode of the new-generation launch vehicles, the front measurement and control equipment is put in the launch pad. In the takeoff stage of the launch vehicle, the equipment needs to bear crucial vibration and noise environment. To make sure that this equipment can work normally during the launch process, an idea of vibration absorption and noise insulation is presented for design. The validity and efficiency of the design idea in vibration absorption and noise insulation is verified by means of the prototype test in a flying mission.关键词
振动与波/运载火箭,减振,隔噪,前端设备Key words
vibration and wave/ launch vehicle/ vibration absorption/ noise insulation/ front equipment分类
军事科技引用本文复制引用
潘玉竹,贾学军,张国栋,范虹,郭金刚..运载火箭前端测控设备减振隔噪技术研究[J].噪声与振动控制,2019,39(3):118-121,4.
