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タイトルData Oscillation Resolution of Propellant Flowmeter Used in FASTRAC Engine Testing
本文(外部サイト)http://hdl.handle.net/2060/20000093951
著者(英)Heflin, J.; Nesman, T.; Hicks, G. D.; Kennedy, Jim W.; Koelbl, M.; Martin, M. A.
著者所属(英)Sverdrup Technology, Inc.
発行日2000-02-01
言語eng
内容記述The Stennis Space Centers' horizontal test facility, Marshall Space Flight Centers' propulsion test article and the X-34 flight vehicle are designed with V-cone flowmeters for measurement of both RP-1 and LOX flow-rates for Fastrac engine testing. Delta pressure transducer data from these flowmeters are used to calibrate the RP-1 and LOX mixture ratio in the Fastrac engine. Data from the V-Cone flowmeter delta pressure transducers have excessive oscillation. The delta pressure oscillations have caused flowrate data fluctuations that interfered with making the accurate readings necessary to calibrate the RP-1 and LOX mixture ratio required for Fastrac engine operation. The objective of this report is to document the flowmeter data oscillation problem and the method used to obtain more reliable flowmeter data.
NASA分類Instrumentation and Photography
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/226766


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