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Achieving Space Shuttle ATO Using the Five-Segment Booster (FSB)As part of the continuing effort to identify approaches to improve the safety and reliability of the Space Shuttle system, a Five-Segment Booster (FSB) design was conceptualized as a replacement for the current Space Shuttle boosters. The FSB offers a simple, unique approach to improve astronaut safety and increase performance margin. To determine the feasibility of the FSB, a Phase A study effort was sponsored by NASA and directed by the Marshall Space Flight Center. This study was initiated in March of 1999 and completed in December of 2000. The basic objective of this study was to assess the feasibility of the FSB design concept and also estimate the cost and scope of a full-scale development program for the FSB. In order to ensure an effective and thorough evaluation of the FSB concept, four team members were put on contract to support various areas of importance in assessing the overall feasibility of the design approach.
Document ID
20020023401
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Sauvageau, Donald R.
(Thiokol Propulsion Brigham City, UT United States)
McCool, Alex
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Space Transportation And Safety
Report/Patent Number
AIAA Paper 2001-3413
Report Number: AIAA Paper 2001-3413
Meeting Information
Meeting: AIAA Joint Propulsion Conference
Location: Salt Lake City, UT
Country: United States
Start Date: July 9, 2001
End Date: July 11, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAS8-97238
Distribution Limits
Public
Copyright
Public Use Permitted.
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