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Propellant mass usage and flow measurementPractices are outlined for the design, installation, checkout, calibration, and operation of a system to be used for measuring propellant flow in a liquid monopropellant rocket engine. Design guidelines rather than detailed specifications are provided for the critical components of each portion of the system. System elemental uncertainties are presented in an appendix.
Document ID
19790022114
Acquisition Source
Legacy CDMS
Document Type
Other
Date Acquired
August 9, 2013
Publication Date
June 1, 1979
Publication Information
Publication: Handbook of Recommended Practices for the Determination of Liquid Monopropellant Rocket Engine Performance
Subject Category
Spacecraft Propulsion And Power
Accession Number
79N30285
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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