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The ACTS SpacecraftThe tested physical and performance characteristics of the ACTS spacecraft are presented with emphasis placed on those for the multibeam antenna, the communications electronics panel, and the bus. Performance measurements for the multibeam antenna agree with predicted parameters, and the electronics panel provides four transponder channels for redundancy and system reliability. The spacecraft bus provides unique features including an attitude-control subsystem with autotrack for pitch accuracy, a sun sensor for yaw control, and thruster firing for dual spin turns.
Document ID
19920047261
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Gargione, Frank
(General Electric Co. Princeton, NJ, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 92-1962
Report Number: AIAA PAPER 92-1962
Meeting Information
Meeting: AIAA International Communication Satellite Systems Conference and Exhibit
Location: Washington, DC
Country: United States
Start Date: March 22, 1992
End Date: March 26, 1992
Accession Number
92A29885
Distribution Limits
Public
Copyright
Other

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