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One Idea for a Next Generation ShuttleIn this configuration, the current Shuttle External Tank serves as core structure for a fully reusable second stage. This stage is equipped with wings, vertical fin, landing gear, and thermal protection. The stage is geometrically identical to (but smaller than) a single stage that has been tested hyper-sonically, super-sonically, and sub-sonically in the NASA Langley Research Center wind tunnels. The three LOX/LH engines that currently serve as main propulsion for the Shuttle Orbiter, serve as main propulsion on the new stage. The new stage is unmanned but is equipped with the avionics needed for automatic maneuvering on orbit and for landing on a runway. Three rails are installed along the top surface of the vehicle for attachment of various payloads. Pay- loads might include third stages with satellites attached, personnel pods, propellants, or other items.
Document ID
20040070775
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
MacConochie, Ian O.
(NASA Langley Research Center Hampton, VA, United States)
Cerro, Jeffrey A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
SAWE Paper-3324
Report Number: SAWE Paper-3324
Meeting Information
Meeting: 63rd Annual Conference of Society of Allied Weight Engineers, Inc.
Location: Newport Beach, CA
Country: United States
Start Date: May 17, 2004
End Date: May 19, 2004
Sponsors: Society of Allied Weight Engineers, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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