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Atlas-Centaur AC-18 performance evaluation for Applications Technology Satellite ATS-5 missionThe Atlas-Centaur with the ATS-5 spacecraft was successfully launched from Eastern Test Range on August 12, 1969, and the ATS-5 was placed in the required highly elliptical transfer orbit with apogee near synchronous altitude. From this orbit the ATS-5, using its apogee motor, achieved the desired near-synchronous circular equatorial orbit. All launch vehicle systems performed satisfactorily.
Document ID
19720005227
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Date Acquired
September 2, 2013
Publication Date
November 1, 1971
Subject Category
Space Vehicles
Report/Patent Number
E-6284
NASA-TM-X-2383
Report Number: E-6284
Report Number: NASA-TM-X-2383
Accession Number
72N12876
Funding Number(s)
PROJECT: RTOP 491-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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