NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Large thermal protection system panelA protective panel for a reusable launch vehicle provides enhanced moisture protection, simplified maintenance, and increased temperature resistance. The protective panel includes an outer ceramic matrix composite (CMC) panel, and an insulative bag assembly coupled to the outer CMC panel for isolating the launch vehicle from elevated temperatures and moisture. A standoff attachment system attaches the outer CMC panel and the bag assembly to the primary structure of the launch vehicle. The insulative bag assembly includes a foil bag having a first opening shrink fitted to the outer CMC panel such that the first opening and the outer CMC panel form a water tight seal at temperatures below a desired temperature threshold. Fibrous insulation is contained within the foil bag for protecting the launch vehicle from elevated temperatures. The insulative bag assembly further includes a back panel coupled to a second opening of the foil bag such that the fibrous insulation is encapsulated by the back panel, the foil bag, and the outer CMC panel. The use of a CMC material for the outer panel in conjunction with the insulative bag assembly eliminates the need for waterproofing processes, and ultimately allows for more efficient reentry profiles.
Document ID
20080007077
Acquisition Source
Langley Research Center
Document Type
Other - Patent
Authors
Myers, Franklin K.
Weinberg, David J.
Tran, Tu T.
Date Acquired
August 24, 2013
Publication Date
January 14, 2003
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
Patent Number: US-PATENT-6,505,794
Patent Application Number: US-PATENT-APPL-SN-769118
Funding Number(s)
CONTRACT_GRANT: NCC1-192
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-6,505,794
Patent Application
US-PATENT-APPL-SN-769118
No Preview Available