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High accuracy thrust measurement of aeronautical propulsion systems with particular consideration to a hydraulic force measuring device, part 1Thrust measurement of aircraft and rocket propulsion systems is discussed. The costs as well as the characteristics of mechanical, electrical and hydraulic systems are compared.
Document ID
19870019125
Acquisition Source
Legacy CDMS
Document Type
Technical Translation (TT)
Authors
Fruboese, Joachim (NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1987
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.77:20080
NASA-TT-20080
Report Number: NAS 1.77:20080
Report Number: NASA-TT-20080
Accession Number
87N28558
Funding Number(s)
CONTRACT_GRANT: NASW-4005
Distribution Limits
Public
Copyright
Public Use Permitted.
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