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Cold Flow Propulsion Test Complex Pulse TestingWhen the propellants in a liquid rocket engine burn, the rocket not only launches and moves in space, it causes forces that interact with the vehicle itself. When these interactions occur under specific conditions, the vehicle's structures and components can become unstable. One instability of primary concern is termed pogo (named after the movement of a pogo stick), in which the oscillations (cycling movements) cause large loads, or pressure, against the vehicle, tanks, feedlines, and engine. Marshall Space Flight Center (MSFC) has developed a unique test technology to understand and quantify the complex fluid movements and forces in a liquid rocket engine that contribute strongly to both engine and integrated vehicle performance and stability. This new test technology was established in the MSFC Cold Flow Propulsion Test Complex to allow injection and measurement of scaled propellant flows and measurement of the resulting forces at multiple locations throughout the engine.
Document ID
20160013350
Acquisition Source
Marshall Space Flight Center
Document Type
Other
Authors
McDougal, Kris
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
November 10, 2016
Publication Date
January 1, 2016
Subject Category
Spacecraft Design, Testing And Performance
Fluid Mechanics And Thermodynamics
Spacecraft Propulsion And Power
Report/Patent Number
M17-5617
Report Number: M17-5617
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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