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Two-plane balance and slip-ring designA 3.25 cm (1.28 in.) two plane balance and eight channel slip ring assembly has been designed to measure and transmit the thrust (667-N;150-lb) and torque (135-N-m;100-lb-ft) components produced by wind tunnel model turboprops and drive motors operating at 300 Hz.
Document ID
19850025223
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Luna, P. M.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
August 1, 1985
Publication Information
Publication: 19th Aerospace Mech. Symp.
Subject Category
Mechanical Engineering
Accession Number
85N33536
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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