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Performance interface document for users of Tracking and Data Relay Satellite System (TDRSS) electromechanically steered antenna systems (EMSAS)Satellites that use the NASA Tracking and Data Relay Satellite System (TDRSS) require antennas that are crucial for performing and achieving reliable TDRSS link performance at the desired data rate. Technical guidelines are presented to assist the prospective TDRSS medium-and high-data rate user in selecting and procuring a viable, steerable high-gain antenna system. Topics addressed include the antenna gain/transmitter power/data rate relationship; Earth power flux-density limitations; electromechanical requirements dictated by the small beam widths, desired angular coverage, and minimal torque disturbance to the spacecraft; weight and moment considerations; mechanical, electrical and thermal interfaces; design lifetime failure modes; and handling and storage. Proven designs are cited and space-qualified assemblies and components are identified.
Document ID
19830016274
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hockensmith, R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Devine, E.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Digiacomo, M.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Hager, F.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Moss, R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:84953
G-83F0183
NASA-TM-84953
Report Number: NAS 1.15:84953
Report Number: G-83F0183
Report Number: NASA-TM-84953
Accession Number
83N24545
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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