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The Space Shuttle Program and its technologyReview of the considerations leading to the development of the Space Shuttle system, followed by a description of the system and an analysis of the current program development status. The Space Shuttle system arose out of a need for a reusable vehicle that could routinely carry large payloads (up to 65,000 lb) into earth orbit and return on a cost-effective basis. The system, as currently baselined, consists of a manned reusable Orbiter vehicle and the booster hardware for ground launching. The proposed Orbiter will be 123 feet long, double delta-winged, and roughly the size of a DC-9. The Orbiter will normally carry a crew of four who will work without space suits in a shirtsleeve environment. The Orbiter will be boosted into space through the simultaneous operation of two solid propellant booster rockets and the Orbiter's three high-pressure liquid oxygen/liquid hydrogen main engines. The Orbiter will have reusable external insulation, since each vehicle will have a design life of ten years.
Document ID
19740037784
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Thompson, R. F.
(NASA Headquarters Washington, DC United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1974
Subject Category
Space Vehicles
Meeting Information
Meeting: Annual Meeting of the International Congress of Space Benefits
Location: Dallas, TX
Start Date: June 19, 1973
End Date: June 20, 1973
Accession Number
74A20534
Distribution Limits
Public
Copyright
Other

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