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Hubble Space Telescope Fine Guidance Sensor Post-Flight Bearing InspectionAerospace mechanism engineering success stories often, if not always, consist of overcoming developmental, test and flight anomalies. Many times it is these anomalies that stimulate technology growth and more reliable future systems. However, one must learn from these to achieve an ultimately successful mission. It is not often that a spacecraft engineer is able to inspect hardware that has flown in orbit for several years. However, in February 1997, the Fine Guidance Sensor-I (FGS-1) was removed from the Hubble Space Telescope (HST) and returned to NASA Goddard Space Flight Center (GSFC) during the second Servicing Mission (SM2). At the time of removal, FGS-1 had nearly 7 years of service and the bearings in the Star Selector Servos (SSS) had accumulated approximately 25 million Coarse Track (CT) cycles. The main reason for its replacement was due to a bearing torque anomaly leading to stalling of the B Star Selector Servo (SSS-B) when reversing direction during a vehicle offset maneuver, referred to herein as a Reversal Bump (RB). The returned HST FGS SSS bearings were disassembled for post-service condition assessment to better understand the actual cause of the torque spikes, identify potential process/design improvements, and provide information for remedial on-orbit operation modifications. The methods and technology utilized for this inspection are not unique to this system and can be adapted to most investigation ai varying stages of the mechanism life from development, through testing, io post night evaluation. The systematic methods used for the HST Fine Guidance Sensor (FGS) SSS and specific findings are the subjects presented in this paper. The lessons learned include the importance of cleanliness and handling for precision instrument bearings and the potential effects from contamination. The paper describes in detail, the analytical techniques used for the SSS and their importance in this investigation. Inspection analytical data and photographs are included throughout the paper.
Document ID
20040081290
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Pellicciotti, Joseph
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Loewenthal, Stu
(Lockheed Martin Space Systems Co. Sunnyvale, CA, United States)
Jones, William, Jr.
(Sest, Inc. Middleburgh Heights, OH, United States)
Jumper, Mike
(BEI Sensors and Motion Systems Co. Maumelle, AR, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2004
Subject Category
Instrumentation And Photography
Meeting Information
Meeting: 37th Aerospace Mechanisms Symposium
Location: Houston, TX
Country: United States
Start Date: May 15, 2004
End Date: May 17, 2004
Distribution Limits
Public
Copyright
Public Use Permitted.
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