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Test results and flight experience of ball bearing momentum and reaction wheelsThe required satellite mission durations and levels of reliability have been considerably increased: While in the beginning of the 70's 3 to 5 year missions were planned, the standard is now 10 years with an expansion to 15 years and more for such programs as INTELSAT VII. Based on a 20 year test and flight experience with basically the same design, ball bearing momentum and reaction wheels with the required 15 year mission capability can be provided.
Document ID
19900012783
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Auer, W.
(Teldix Luftfahrt-Ausruestungs G.m.b.H. Heidelberg, Germany)
Date Acquired
September 6, 2013
Publication Date
April 1, 1990
Publication Information
Publication: NASA, John F. Kennedy Space Center, The 24th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Accession Number
90N22099
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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