The embodiment of the invention provides a side thrust rocket high-altitude blowing test device bound with a carrier rocket. The side thrust rocket high-altitude blowing test device comprises a high-altitude cabin (1), a vacuumizing system (2), a vacuum monitoring system (3), a data acquisition system (4) and a control system (5). And the vacuumizing system (2) is connected with the high-altitude cabin (1) through a pipeline, so that the high-altitude cabin (1) reaches a specified vacuum degree to meet the high-altitude blowing test requirements of the side thrust rocket. According to the invention, test environments of different vacuum degrees corresponding to different separation heights of the bound carrier rocket booster can be established, so that the effectiveness of safeguard measures of products on the rocket can be verified more truly, and environmental parameters can be obtained.

    本发明实施例提供了一种捆绑运载火箭的侧推火箭高空对吹试验装置,包括:高空舱(1)、抽真空系统(2)、真空监测系统(3)、数据采集系统(4)、控制系统(5)。抽真空系统(2)通过管路与高空舱连接(1),使高空舱(1)达到指定的真空度,以满足侧推火箭高空对吹试验要求。本发明可搭建出捆绑运载火箭助推器不同分离高度对应的不同真空度的试验环境,从而更真实的验证箭上产品防护措施的有效性,并获得环境参数。


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    Title :

    Lateral thrust rocket high-altitude blowing test device for binding carrier rocket


    Additional title:

    一种捆绑运载火箭的侧推火箭高空对吹试验装置


    Contributors:
    XIANG CHANGZHENG (author) / ZHAO ZHIJIE (author) / ZENG YUQIN (author) / DONG WENFENG (author) / YAN LI (author) / ZHANG LIANG (author) / ZHU LIANGCONG (author) / ZHANG WEIDONG (author)

    Publication date :

    2022-12-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS




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