火箭橇试验推力测量方法研究

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振动与冲击 ›› 2013, Vol. 32 ›› Issue (18) : 59-62.

论文

火箭橇试验推力测量方法研究

王军评1，毛勇建1，董龙雷2，雷磊2

作者信息 +

Study on thrust measurement method for rocket sled testing

WANG Jun-ping1，MAO Yong-jian1，DONG Long-lei2，LEI Lei2

Author information +

文章历史 +

摘要

以典型火箭橇试验系统为对象，对系统运动的不同阶段进行力学分析。在建立推力测量系统基础上，对不同马赫数下火箭橇试验的推力数据进行分析处理。研究结果可为综合力学环境火箭橇试验平台的建立提供参考。

Abstract

Thrust is one of the essential loading parameters of the structure on sled of rocket sled testing. In this paper, firstly, the mechanics of the movement of a typical rocket sled testing system in different stages is analyzed. Then, the thrust measurement system is built. In the end, the test data measured by this system in different Mach number are processed and discussed. The results can provide theoretical foundation for establishing an integrated mechanical environment platform based on rocket sled testing.

导出引用

王军评;毛勇建;董龙雷;雷磊. 火箭橇试验推力测量方法研究[J]. 振动与冲击, 2013, 32(18): 59-62

WANG Jun-ping;MAO Yong-jian;DONG Long-lei;LEI Lei. Study on thrust measurement method for rocket sled testing[J]. Journal of Vibration and Shock, 2013, 32(18): 59-62