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Keywords: rocket engines
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Journal Articles
Article Type: Technical Papers
J. Vib. Acoust. January 2003, 125(1): 64–67.
Published Online: January 6, 2003
... for a turbopump in a liquid-rocket-engine development program showed a twice-running-speed response (2E) on the order of 8 gs over a wide speed range, while synchronous response levels were only at an 0.5 g level. Childs [2] predicted a sharp 2E response for the Advanced Technology Development, High-Pressure Fuel...