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Space Shuttle external tank: Today - DDT & E: Tomorrow - ProductionThe External Tank (ET) is the structural backbone of the Space Shuttle. The ET is discussed relative to its role; its design as a highly efficient Shuttle element; the liquid oxygen tank - a thin shelled monocoque; the intertank - the forward structural connection; the liquid hydrogen tank structure - the connection with the Orbiter; the ET structural verification; the propulsion system - a variety of functions; the electrical subsystem; electrical subsystem qualification; the thermal protection system; and other related problems. To date the qualification programs have been extremely successful and are almost complete, and the first flight tank has been delivered. Tomorrow's objectives will concentrate on establishing the facilities, tools and processes to achieve a production rate of 24 ETs/year.
Document ID
19800032269
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Norton, A. M.
(Martin Marietta Aerospace New Orleans, LA, United States)
Tanner, E. J.
(Martin Marietta Aerospace New Orleans, La., United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1979
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
AAS PAPER 79-272
Meeting Information
Meeting: Annual Meeting
Location: Los Angeles, CA
Start Date: October 29, 1979
End Date: November 1, 1979
Sponsors: American Astronautical Society
Accession Number
80A16439
Funding Number(s)
CONTRACT_GRANT: NAS8-30300
Distribution Limits
Public
Copyright
Other

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