The invention relates to a universal hypersonic flight test system, which comprises an effective load system, a ground system, a test carrying platform, a ground comprehensive control machine, a launch vehicle, a test launch control vehicle, a remote measurement vehicle and an external measurement vehicle, and is characterized in that the ground comprehensive control machine is a central node of the whole test system and is used for task planning, parameter instruction issuing and data recovery analysis; a test launch control front end and a carrier are arranged on the launch vehicle, the test launch control front end is used for executing instruction signals transmitted by the test launch control vehicle, the carrier comprises a carrying platform and a test load, the test load is installed in a fairing of the test platform, and the test platform provides a flight environment, power supply and communication conditions for the test load. The system provided by the invention adopts a universal and automatic design, the system works efficiently, and various hypersonic flight tests can be conveniently carried out.

    本发明涉及一种通用化高超声速飞行试验系统,包括有效载荷系统、地面系统和试验运载平台,包括地面综控机、发射车、测发控车、遥测车和外测车,地面综控机是整个试验系统的中心节点,用于任务规划、参数指令下发和数据回收分析;发射车上设置测发控前端和运载器,测发控前端用于执行测发控车传递过来的指令信号,运载器包括运载平台和试验载荷,试验载荷安装于试验平台的整流罩内,试验平台为试验载荷提供飞行环境、供电和通信条件。本发明所提供的系统采用通用化和自动化设计,系统工作高效,方便开展各型高超声速飞行试验。


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    Title :

    Universal hypersonic flight test system


    Additional title:

    一种通用化高超声速飞行试验系统


    Contributors:
    LI XIAOHUI (author) / ZHANG PEIJUN (author) / ZHANG BINGFENG (author) / YANG MINGXING (author) / WANG XIAONI (author) / LIU XUFEI (author) / ZHENG PEI (author) / ZHANG YONGHUA (author)

    Publication date :

    2023-07-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen




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    Hypersonic airbreathing propulsion - Flight test needs

    Falempin, F / Thevenot, R / Vancamberg, ard, PhRol, PhGirard, | AIAA | 1995


    Flight-test guidance for airbreathing hypersonic vehicles

    Cliff, Eugene M. / Well, KLAUS-H. / Schnepper, Klaus | NTRS | 1992