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New Understanding of Hubble Space Telescope Gyro Current Increase Led to a Method to Save a Failing GyroThroughout the history of the Hubble Space Telescope (HST) program, gyro current increases have been observed to occur, oftentimes leading to gyro failure. The explanation was that debris from the surfaces of the gas bearings, with only 50 millionths on an inch clearance, resulted in rotor restriction, which increased friction, torque, and current. However, the rotor restriction theory never could account for the fact that a restart of the gyro would restore the current back to nominal. An effort was made to understand this puzzling gyro behavior after two HST gyros exhibited increased current within the same week in November 2015. A review board was created to resolve these anomalies and generate operational procedures to potentially extend gyro life.
Document ID
20170008997
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Blumenstock, Kenneth A.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
September 26, 2017
Publication Date
September 20, 2017
Subject Category
Mechanical Engineering
Report/Patent Number
GSFC-E-DAA-TN43390
Meeting Information
Meeting: European Space Mechanisms and Tribology Symposium
Location: Hatfield
Country: United Kingdom
Start Date: September 20, 2017
End Date: September 22, 2017
Sponsors: European Space Agency, Airbus Defence and Space
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Mechanism
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