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Two-axis antenna positioning mechanismThe two-axis antenna positioning mechanism (TAAPM) is used to position three Ku-band and one C-band spot antennas on the INTELSAT 7 (I-7) spacecraft, which is a commercial telecommunications satellite purchased and operated by INTELSAT, an international consortium. The first I-7 was successfully launched on 22 Oct. 1993 from French Guiana on an Ariane launch vehicle. The TAAPM's on the first I-7 satellite successfully completed their in-orbit functional testing. The TAAPM was an entirely new design for Space Systems/Loral. This paper will describe the spacecraft/system requirements and application of the TAAPM and present the technical findings of TAAPM qualification and protoflight testing.
Document ID
19940028802
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Herald, Michelle
(Space Systems/Loral Palo Alto, CA, United States)
Wai, Leilani C.
(Space Systems/Loral Palo Alto, CA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1994
Publication Information
Publication: NASA. Lewis Research Center, The 28th Aerospace Mechanisms Symposium
Subject Category
Mechanical Engineering
Accession Number
94N33308
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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