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Precision flow measurement techniques for low thrust auxiliary propulsion liquid rocketsPrecision flow measurement techniques for low thrust auxiliary propulsion liquid rockets
Document ID
19670030596
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Grant, D. J. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-55967
X-734-67-440
Report Number: NASA-TM-X-55967
Report Number: X-734-67-440
Accession Number
67N39925
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLOW MEASUREMENT
FUEL CONSUMPTION
THRUSTOR

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