DocumentCode :
2551071
Title :
Antenna subsystem for the INTELSAT VII spacecraft
Author :
Schennum, G.H. ; Ersoy, L.
Author_Institution :
Ford Aerosp., Palo Alto, CA, USA
fYear :
1990
fDate :
4-9 Feb. 1990
Firstpage :
83
Lastpage :
92
Abstract :
A multifunction antenna subsystem consisting of communications and telemetry/command antennas for the INTELSAT VII communications satellite is described. The antenna subsystem design is dictated by a requirement to provide multiple communications links between the Earth and the spacecraft and by a need to track, command, and monitor the spacecraft during all phases of its flight. The eight different types of antennas on the spacecraft are described in detail. The subsystem performance has been analytically verified by computer modeling. The basic hardware design has been completed, and fabrication and testing of the engineering model hardware are in progress.<>
Keywords :
aerospace computing; artificial satellites; digital simulation; mobile antennas; satellite relay systems; INTELSAT VII spacecraft; antenna subsystem design; communications satellite; computer modeling; coverage; engineering model hardware; fabrication; microwave antenna; multifunction antenna; multiple communications links; telemetry/command antennas; testing; Artificial satellites; Computerized monitoring; Earth; Fabrication; Hardware; Performance analysis; Satellite antennas; Space vehicles; Telemetry; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Applications Conference, 1990. Digest., 1990 IEEE
Conference_Location :
Vail, CO, USA
Type :
conf
DOI :
10.1109/AERO.1990.109074
Filename :
109074
Link To Document :
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