DocumentCode
752786
Title
An Overview of the Space Shuttle Orbiter Communication and Tracking System
Author
Carrier, Louis M. ; Pope, Warren S.
Author_Institution
Rockwell International, Downey, CA
Volume
26
Issue
11
fYear
1978
fDate
11/1/1978 12:00:00 AM
Firstpage
1494
Lastpage
1506
Abstract
During space flight, the communications and tracking system of the Space Shuttle Orbiter uses
-band and
-band links to provide, in addition to tracking, reception of digitized voice, commands, and printed or diagrammatic data at a maximum rate of 216 kbits/s. The system provides a transmission capability for digitized voice, telemetry, television, and data at a maximum rate of 50 Mbits/s.
-band links may be established directly with a ground station and both
-band and
-band links may be routed through NASA\´s Tracking and Data Relay Satellite System. A simultaneous capability to communicate with other satellites or spacecraft, using a variety of formats and modulation techniques on more than 850
-band channels, is provided. UHF is used for communication with extravehicular astronauts. Audio and television subsystems serve on-board needs as well as interfacing with the RF equipment. During aerodynamic flight following entry, the
-band link can be supplemented or replaced by a UHF link that provides two-way simplex voice communication with Air Traffic Control facilities. TACAN is used as a navigation aid from shortly after blackout exit at about 150 000 ft (45.7 km) to about a 10 000-ft (3-km) altitude where a microwave scan-beam landing system assumes navigation aid functions. At about 2500 ft (760 m) to touchdown, radar altimeters provide accurate altitude determination.
-band and
-band links to provide, in addition to tracking, reception of digitized voice, commands, and printed or diagrammatic data at a maximum rate of 216 kbits/s. The system provides a transmission capability for digitized voice, telemetry, television, and data at a maximum rate of 50 Mbits/s.
-band links may be established directly with a ground station and both
-band and
-band links may be routed through NASA\´s Tracking and Data Relay Satellite System. A simultaneous capability to communicate with other satellites or spacecraft, using a variety of formats and modulation techniques on more than 850
-band channels, is provided. UHF is used for communication with extravehicular astronauts. Audio and television subsystems serve on-board needs as well as interfacing with the RF equipment. During aerodynamic flight following entry, the
-band link can be supplemented or replaced by a UHF link that provides two-way simplex voice communication with Air Traffic Control facilities. TACAN is used as a navigation aid from shortly after blackout exit at about 150 000 ft (45.7 km) to about a 10 000-ft (3-km) altitude where a microwave scan-beam landing system assumes navigation aid functions. At about 2500 ft (760 m) to touchdown, radar altimeters provide accurate altitude determination.Keywords
Satellite telemetry; Satellite tracking; Space Shuttle; Space-vehicle communications; Artificial satellites; Navigation; Radar tracking; Relays; Satellite broadcasting; Satellite ground stations; Space shuttles; Space vehicles; TV; Telemetry;
fLanguage
English
Journal_Title
Communications, IEEE Transactions on
Publisher
ieee
ISSN
0090-6778
Type
jour
DOI
10.1109/TCOM.1978.1094025
Filename
1094025
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