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Structures and Materials Technologies for Extreme Environments Applied to Reusable Launch VehiclesThis paper provides an overview of the evolution of structures and materials technology approaches to survive the challenging extreme environments encountered by earth-to-orbit space transportation systems, with emphasis on more recent developments in the USA. The evolution of technology requirements and experience in the various approaches to meeting these requirements has significantly influenced the technology approaches. While previous goals were primarily performance driven, more recently dramatic improvements in costs/operations and in safety have been paramount goals. Technologies that focus on the cost/operations and safety goals in the area of hot structures and thermal protection systems for reusable launch vehicles are presented. Assessments of the potential ability of the various technologies to satisfy the technology requirements, and their current technology readiness status are also presented.
Document ID
20040008891
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Scotti, Stephen J.
(NASA Langley Research Center Hampton, VA, United States)
Clay, Christopher
(Air Force Research Lab. Wright-Patterson AFB, OH, United States)
Rezin, Marc
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Structural Mechanics
Report/Patent Number
AIAA Paper 2003-2697
Report Number: AIAA Paper 2003-2697
Meeting Information
Meeting: AIAA/ICAS International Air and Space Symposium and Exposition
Location: Dayton, OH
Country: United States
Start Date: July 14, 2003
End Date: July 17, 2003
Sponsors: American Inst. of Aeronautics and Astronautics, International Council of the Aeronautical Sciences
Funding Number(s)
OTHER: RTA 23-721-21-51-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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