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ATS-6 spacecraft design/performanceA description is given of major program objectives and experiment requirements established for ATS-6. The ability to slew across the earth's disk in less than 30 min was needed to support tightly scheduled communication operations involving different parts of the earth. Two major experiments were developed which involve direct satellite relay of educational color television programs to simple ground receivers. Details of spacecraft configuration are discussed along with aspects of spacecraft ground testing. The ATS-6 was successfully launched on schedule from Cape Canaveral on May 30, 1974, with the aid of a Titan IIIC. The in-orbit performance of the spacecraft communication subsystem has been excellent.
Document ID
19750041963
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Redisch, W. N.
(NASA Goddard Space Flight Center Greenbelt, Md., United States)
Hall, R. L.
(Fairchild Industries, Inc. Germantown, Md., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1974
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: EASCON ''74; Electronics and Aerospace Systems Convention
Location: Washington, DC
Start Date: October 7, 1974
End Date: October 9, 1974
Accession Number
75A26035
Funding Number(s)
CONTRACT_GRANT: NAS5-21100
Distribution Limits
Public
Copyright
Other

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