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Hubble Space Telescope EVA Multisetting Torque Limiter redesignThe Hubble Space Telescope (HST) Multisetting Torque Limiter will be used by astronauts during the First Servicing Mission STS-61. It was designed to replace several individual torque limiters. This replacement reduces the number of tools required as well as reduce the time required for servicing. The Multisetting Torque Limiter design specified five separate torque settings: 2, 5.3, 9, 35 and 45 ft-lbs. This original units were tested at the 2, 5.3, and 9 ft-lbs settings and did not meet the design specifications. The 35 ft-lb and 45 ft-lb torque settings were not incorporated into the original flight design. The objective of the Goddard Space Flight Center (GSFC) redesign effort is to incorporate all five torque settings into a flight design which means the requirements for the first HST Servicing Mission. The first target of the redesign effort focused on the spring chamber and ball detent design. The original design used belleville springs in parallel; the new design changed this configuration to belleville springs stacked in series. The current engineering unit was successfully tested in ambient environment at all five settings. A flight design will soon undergo thermal vacuum testing to evaluate its performance at the temperature extremes.
Document ID
19950048820
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Richards, Paul W.
(NASA Goddard Space Flight Center Greenbelt, MD, US, United States)
Garrah, Mike
(Swales and Associates, Beltsville, MD US, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publisher: American Astronautical Society (Advances in the Astronautical Sciences, Vol. 81)
ISSN: 0065-3438
Subject Category
Mechanical Engineering
Accession Number
95A80419
Distribution Limits
Public
Copyright
Other

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