NASA NTRS · 19850025223
Two-plane balance and slip-ring design
Abstract
A 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.
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Luna, P. M.. 1985-08-01. Two-plane balance and slip-ring design. https://ntrs.nasa.gov/citations/19850025223
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