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《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2009年06期
Page:
57-60
Research Field:
测控与试验
Publishing date:

Info

Title:
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Author(s):
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Keywords:
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PACS:
V434
DOI:
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Abstract:
For improvement of thrust level measurment accuracy of liquid rocket engine, measurement system modification was conducted. The previously used strain-beam system was replaced by dual-curved-beam measuring system. System modification measures and application results were introduced in this paper. Test results show that the dual-curved-beam measuring system has higher accuracy and better enviornment adaptability.

References:

[1]卞水思, 张文声. 脉冲火箭发动机动态推力测量系统[J]. 试验技术通讯. 1981, 1(1): 1-27.
[2]张迎新. 火箭发动机参数测量技术[M]. 长沙: 国防科技大学出版社, 1987.
[3]刘伟亮, 吴建军. 机电一体化推力测量系统的研制及应用[J]. 火箭推进, 2004, 12(6): 50-54, 49.
[4]王洪业. 传感器工程[M]. 长沙: 国防科技大学出版社, 1997.

Memo

Memo:
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Last Update: 1900-01-01