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Centaur capabilities for communications satellite launchesThe configurations, payload capabilities, and payload envelopes for Centaur in various applications are presented. The Centaur launch record is summarized and the Atlas/Centaur launch schedule is shown. Improvements in capability are reported on, and current and proposed vehicles are depicted. Dual Delta class spacecraft will be flown using a tandem adapter or large direct broadcast satellites in a single launch model. Shuttle/Centaur will permit spacecraft weights of up to 14,000 lb to be put into orbit, including payload lengths up to 40 ft. A new capability to transfer large deployed space systems from the Shuttle to high-altitude orbits at low thrusts will be available. Spacecraft lengths requiring the full, 60-foot cargo bay and weighing 20,000 lb could be placed in geosynchronous orbit with on-orbit rendezvous and assembly of the Centaur and spacecraft in low earth orbit.
Document ID
19820052751
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rector, W. F., III
(General Dynamics Corp. Convair Div., San Diego, CA, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1982
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
AIAA PAPER 82-0558
Report Number: AIAA PAPER 82-0558
Meeting Information
Meeting: Communications Satellite System Conference
Location: San Diego, CA
Start Date: March 8, 1982
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
82A36286
Funding Number(s)
CONTRACT_GRANT: NAS3-22901
CONTRACT_GRANT: NAS3-22914
Distribution Limits
Public
Copyright
Other

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