Referenced Items are not available for this document.
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.<
Published in:
Aerospace Applications Conference, 1990. Digest., 1990 IEEE
Date of Conference: 4-9 Feb. 1990
- Page(s):
- 83 - 92
- Meeting Date :
- 04 Feb 1990-09 Feb 1990
- INSPEC Accession Number:
- 3936490
- Conference Location :
- Vail, CO, USA
- Digital Object Identifier :
- 10.1109/AERO.1990.109074
- Product Type:
- Conference Publications
About IEEE Xplore | Contact | Help | Terms of Use | Nondiscrimination Policy | Site Map | Privacy & Opting Out of Cookies
A not-for-profit organization, IEEE is the world's largest professional association for the advancement of technology.
© Copyright 2013 IEEE - All rights reserved. Use of this web site signifies your agreement to the terms and conditions.
