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Applications technology satellites advanced mission studyThree spacecraft configurations were designed for operation as a high powered synchronous communications satellite. Each spacecraft includes a 1 kw TWT and a 2 kw Klystron power amplifier feeding an antenna with multiple shaped beams. One of the spacecraft is designed to be boosted by a Thor-Delta launch vehicle and raised to synchronous orbit with electric propulsion. The other two are inserted into a elliptical transfer orbit with an Atlas Centaur and injected into final orbit with an apogee kick motor. Advanced technologies employed in the several configurations include tubes with multiple stage collectors radiating directly to space, multiple-contoured beam antennas, high voltage rollout solar cell arrays with integral power conditioning, electric propulsion for orbit raising and on-station attitude control and station-keeping, and liquid metal slip rings.
Document ID
19720023179
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gould, L. M.
(Hughes Aircraft Co. Los Angeles, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1972
Subject Category
Space Sciences
Report/Patent Number
NASA-CR-120872
Report Number: NASA-CR-120872
Accession Number
72N30829
Funding Number(s)
CONTRACT_GRANT: NAS3-14359
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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