Spacecraft multibeam antenna system for 30/20 GHz
Abstract
The major technical tasks that led to the definitions of operational and demonstration multiple beam antenna (MBA) flight systems and a proof of concept model (POC) are described. Features of the POC Model and its measured performance are presented in detail. Similar MBA's are proposed for transmitting and receiving with the POC Model representing the 20 GHz transmitting antenna. This POC MBA is a dual shaped-surface reflector system utilizing a movable free array to simulate complete CONUS coverage. The beam forming network utilizes ferrite components for switching from one beam to another. Measured results for components, subsystems and the complete MBA confirm the feasibility of the approach and also show excellent correlation with calculated values.
- Publication:
-
Final Report Ford Aerospace and Communications Corp
- Pub Date:
- January 1984
- Bibcode:
- 1984fac..rept.....R
- Keywords:
-
- Downlinking;
- Multibeam Antennas;
- Satellite Antennas;
- Spacecraft Communication;
- Antenna Design;
- Models;
- Radio Transmission;
- Specifications;
- Communications and Radar