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Preliminary Development of a Multifunctional Hot Structure Heat ShieldDevelopment of a Multifunctional Hot Structure Heat Shield concept has initiated with the goal to provide advanced technology with significant benefits compared to the current state of the art heat shield technology. The concept is unique in integrating the function of the thermal protection system with the primary load carrying structural component. An advanced carbon-carbon material system has been evaluated for the load carrying structure, which will be utilized on the outer surface of the heat shield, and thus will operate as a hot structure exposed to the severe aerodynamic heating associated with planetary entry. Flexible, highly efficient blanket insulation has been sized for use underneath the hot structure to maintain desired internal temperatures. The approach was to develop a preliminary design to demonstrate feasibility of the concept. The preliminary results indicate that the concept has the potential to save both mass and volume with significantly less recession compared to traditional heat shield designs, and thus provide potential to enable new planetary missions.
Document ID
20140007353
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Walker, Sandra P.
(NASA Langley Research Center Hampton, VA, United States)
Daryabeigi, Kamran
(NASA Langley Research Center Hampton, VA, United States)
Samareh, Jamshid A.
(NASA Langley Research Center Hampton, VA, United States)
Armand, Sasan C.
(NASA Langley Research Center Hampton, VA, United States)
Perino, Scott V
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
June 12, 2014
Publication Date
January 13, 2014
Subject Category
Structural Mechanics
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-16692
AIAA Paper 2014-0350
Meeting Information
Meeting: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Location: National Harbor, MD
Country: United States
Start Date: January 13, 2014
End Date: January 17, 2014
Sponsors: American Helicopter Society, Inc., American Society for Composites, American Inst. of Aeronautics and Astronautics, American Society of Civil Engineers, American Society of Mechanical Engineers
Funding Number(s)
WBS: WBS 295670.01.07.62
Distribution Limits
Public
Copyright
Public Use Permitted.
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