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Orbiter S-band direct link system verification test reportSpace-to-ground S-band communications system compatibility and performance tests were performed for the various radio frequency links. These tests consisted of the various uplink and downlink signal combinations (data rates) for the phase modulation system and both realtime and playback data rates for the frequency modulated downlink systems. In addition, tests involving encryption/decryption, Doppler, and acquisition were performed. Results show that the S-band transponder for the space shuttle orbiter is compatible with the S-band equipment of the AFSCF/RTS (Air Force Satellite Control Facility/Remote Tracking Station). It is also concluded that the performance of the orbiter-AFSCF/RTS direct link exceeds the required performance and that this communications link will meet the system requirements of the Space Transportation System.
Document ID
19800018913
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Vermillion, B. K.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1980
Subject Category
Space Transportation
Report/Patent Number
NASA-TM-81110
JSC-16680
Report Number: NASA-TM-81110
Report Number: JSC-16680
Accession Number
80N27414
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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