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Shuttle operational expectationsThe results of orbital flight tests (OFT) of the Space Shuttle are reviewed, and modifications planned for upcoming operational flights are discussed. The performance of the solid rocket boosters, external tank, main engines, structural system, propulsion system, reaction control system, electric power system, heat rejection system, hydraulic system, avionics, and other systems is described and evaluated as generally highly satisfactory. Payload servicing and deployment were also successfully demonstrated by OFT. Additional facilities planned for the operational flights are briefly described, and improvements that will make the Challenger spacecraft lighter than Columbia, provide it with more thrust, and give it a larger payload are summarized. Some software modifications being introduced are also mentioned.
Document ID
19830029780
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Abrahamson, J. A.
(NASA Office of Space Flight Washington, DC, United States)
Date Acquired
August 11, 2013
Publication Date
November 1, 1982
Publication Information
Publication: Astronautics and Aeronautics
Volume: 20
Subject Category
Space Transportation
Accession Number
83A10998
Distribution Limits
Public
Copyright
Other

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