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The Space Shuttle - Key considerationsTypical Space Shuttle flight operations, including launch/insertion, on-orbit operations, de-orbit, and ground turnaround, are summarized. The orbiter, main engine, and solid rocket boosters will be reusable. The Shuttle will be able to abort ascent and return the orbiter plus payload to the launch site if necessary. Mission capabilities include a 7-30 day duration, crew of 4-7 (with 1-4 payload specialists), and 14,500-29,500 kg payloads. Payload accommodations, including cabin, crew provisions, pointing and position stability, thermal constraints, electric power, communications, payload deployment and retrieval, contamination control, and kits for extended missions, are considered. The Thermal Protection System, utilizing pyrolized carbon and silica tiles, is described. The Space Shuttle Main Engine design and performance are considered and compared to those of the J-2 engine used on Saturn/Apollo missions.
Document ID
19750029639
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Malkin, M. S.
(NASA Office of Manned Space Flight Washington, D.C., United States)
Date Acquired
August 8, 2013
Publication Date
September 1, 1974
Subject Category
Space Transportation
Report/Patent Number
IAF PAPER 74-077
Report Number: IAF PAPER 74-077
Accession Number
75A13711
Distribution Limits
Public
Copyright
Other

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