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Space Shuttle Program - An overviewThe Space Shuttle's unique design features include multiple re-uses of its major elements, large cargo carrying capacity, and the capability of deploying, servicing, and retrieving a variety of payloads. These design features, i.e., reusability and cargo flexibility, were incorporated to satisfy the objective of providing a transportation system which will lower the cost of delivering a variety of payloads to the earth orbit. The Space Shuttle System consists of a reusable manned Orbiter containing three main engines, two reusable Solid Rocket Boosters, and an expendable External Tank containing propellant for the Orbiter main engines. On a typical Space Shuttle mission, the Orbiter will remain in orbit for up to 7 days conducting on-orbit observations and operations, return to earth with personnel and payload, land horizontally on a runway, and be readied for another flight in as few as 14 days. Another mission class includes deploying, servicing, and recovering satellites.
Document ID
19760043850
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kloves, T. R.
(NASA Johnson Space Center Program Planning Office, Houston, Tex., United States)
Date Acquired
August 8, 2013
Publication Date
April 1, 1976
Subject Category
Space Transportation
Report/Patent Number
AIAA PAPER 76-275
Report Number: AIAA PAPER 76-275
Meeting Information
Meeting: Communications Satellite Systems Conference
Location: Montreal
Country: Canada
Start Date: April 5, 1976
End Date: April 8, 1976
Sponsors: American Institute of Aeronautics and Astronautics and Canadian Aeronautics and Space Institute
Accession Number
76A26816
Distribution Limits
Public
Copyright
Other

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