NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Force and impulse measurementPractices are outlined for the design, installation, checkout, calibration, and operation of a thrust measurement system to be used during tests of a liquid monopropellant rocket engine. Appendixes include: (1) thrust measurement system elemental uncertainties; (2) short- and long-term thrust measurement system uncertainty; and (3) shunt calibration of force transducers.
Document ID
19790022113
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
79N30284
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available