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Investigation of the piezoelectric thrust test stand for rocket engine

โœ Scribed by Gao, C.Y.; Sun, B.Y.

Book ID
114445163
Publisher
The Institution of Engineering and Technology
Year
2009
Tongue
English
Weight
589 KB
Volume
3
Category
Article
ISSN
1751-8822

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Small thrust liquid pulsed rocket engines operating in pulsed mode have gained a good reputation in attitude control applications for their potential reliability and efficiency. However, the pulsed characteristic creates a difficult measurement problem. In this paper, a novel thrust dynamometer with