NASA NTRS · 19720005264
SERT 2 gimbal system
Abstract
The gimbal system is described that was designed to mount the thruster and to reposition the thrust vector of a mercury ion bombardment thruster through the center of gravity of the SERT 2 assembly. The SERT 2 assembly was launched 3 February 1970. The gimbal ring, gimbal mounts, bearings, actuators, and environmental testing are described. Due to the accurate alinements provided, it was not necessary to use the gimbal for the intended function. However, the gimbals were operated successfully numerous times in space after 8 months of storage.
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Zavesky, R. J., Hurst, E. B.. 1971-12-01. SERT 2 gimbal system. https://ntrs.nasa.gov/citations/19720005264
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