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Microelectronics Instrument Products Shock and Vibration Electro-Optics: Acceptance Data Package - Section BThe motor/encoder (henceforth referred to as the UUT) test sequence began with a baseline functional evaluation, which demonstrated that the motor satisfied the operating torque, cogging torque, winding resistance, and mechanical requirements of SOW. In addition, the encoder electrical requirements were verified, as well as the alignment of the encoder outputs relative to the motor shaft position. There were no discrepancies observed in this portion of the test. The UUT was then exposed to a number of environments, including thermal vacuum, thermal cycling, random and sine vibration, and mechanical shock. During the thermal environments, the performance of the UUT under load was verified at specified points in the cycles, as described in ATP 20049. In addition, the UUT was bench tested between the two thermal environments. No anomalies were observed during the thermal tests. The vibration and shock tests were performed by East-West Technology Corporation, West Babylon, New York. The UUT was delivered to the lab in a sealed vibration fixture in order to maintain the cleanliness levels required by the SOW. In addition, a three ounce load was attached to the motor shaft. The attachment method of this load caused damage to the shaft and bearing during random vibration of S/N 0003 on April 28, 1995, and is described further in NCR 00168.
Document ID
19990026236
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Standard/Specification
Date Acquired
September 6, 2013
Publication Date
July 20, 1995
Subject Category
Electronics And Electrical Engineering
Funding Number(s)
CONTRACT_GRANT: NAS8-39409
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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