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Using a "HOLLoW" Design for Traditional Shuttle Tiles to Reduce Mass up to 30%For spacecraft entering an atmosphere, a reduction in TPS mass is directly proportional to the increase in payload mass. The HOLLOW TPS concept is a reusable material with lower density and similar thermal capabilities to traditional tiles. Using HOLLOW TPS to replace a percentage of the tiles on a flight vehicle could save up to 35% mass depending on the mission objectives and flight path. The HOLLOW TPS will also increase an equal amount of payload capacity, increasing the efficiency of the mission.
Document ID
20190031965
Acquisition Source
Ames Research Center
Document Type
Abstract
Authors
Peterson, Keith H.
(NASA Ames Research Center Moffett Field, CA, United States)
Carder, Nichole B.
(Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Date Acquired
October 4, 2019
Publication Date
September 29, 2019
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN71614
Meeting Information
Meeting: Materials, Science & Technology
Location: Portland, OR
Country: United States
Start Date: September 29, 2019
End Date: October 3, 2019
Sponsors: The American Ceramic Society (ACerS)
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
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