NASA NTRS · 19790022113
Force and impulse measurement
Abstract
Practices 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.
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1979-06-01. Force and impulse measurement. https://ntrs.nasa.gov/citations/19790022113
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