DocumentCode
990233
Title
Multifunction single-package antenna system for spin-stabilized near-synchronous satellite
Author
Rankin, J. Bruce ; Devane, Mark E. ; Rosenthal, Milton L.
Author_Institution
M.I.T. Lincoln Lab., Lexington, MA, USA
Volume
17
Issue
4
fYear
1969
fDate
7/1/1969 12:00:00 AM
Firstpage
435
Lastpage
442
Abstract
An antenna system is described for a spin-stabilized satellite with its axis normal to the orbital plane. Three antennas in a compact lightweight package comprise the antenna system: a switched-beam
-band transmitting antenna, an omnidirectional
-band receiving antenna and an omnidirectional VHF telemetry antenna. The first is a cluster of eight circularly polarized horns pointed radially outward every 45 degrees about the spin axis. An eight-throw solid-state waveguide switch turns on that horn currently pointing most nearly to earth. This is accomplished by providing the switch with electrical signals from a logic circuit operating on information from earth sensors. The second antenna is a circularly polarized biconical horn located above the cluster of transmitting horns. Its sense of polarization is opposite that of the transmitting antenna, and a filter in the transmission line to the receiver insures the required isolation. The third antenna is obtained by feeding across the gap between the two
-band antennas and exciting the external surfaces to radiate in a linearly polarized mode. Total weight of the three-antenna package is less than
pounds; it occupies a volume less than 10 inches square by 8 inches high above the top panel of the satellite.
-band transmitting antenna, an omnidirectional
-band receiving antenna and an omnidirectional VHF telemetry antenna. The first is a cluster of eight circularly polarized horns pointed radially outward every 45 degrees about the spin axis. An eight-throw solid-state waveguide switch turns on that horn currently pointing most nearly to earth. This is accomplished by providing the switch with electrical signals from a logic circuit operating on information from earth sensors. The second antenna is a circularly polarized biconical horn located above the cluster of transmitting horns. Its sense of polarization is opposite that of the transmitting antenna, and a filter in the transmission line to the receiver insures the required isolation. The third antenna is obtained by feeding across the gap between the two
-band antennas and exciting the external surfaces to radiate in a linearly polarized mode. Total weight of the three-antenna package is less than
pounds; it occupies a volume less than 10 inches square by 8 inches high above the top panel of the satellite.Keywords
Multifunction antennas; Satellite antennas; Antenna feeds; Earth; Optical polarization; Packaging; Receiving antennas; Satellite antennas; Solid state circuits; Switches; Telemetry; Transmitting antennas;
fLanguage
English
Journal_Title
Antennas and Propagation, IEEE Transactions on
Publisher
ieee
ISSN
0018-926X
Type
jour
DOI
10.1109/TAP.1969.1139474
Filename
1139474
Link To Document