Spacecraft High Tensile Fabric Barrier for Hot Re-Entry Gases

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20200130867A1
SERIAL NO

16173821

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A multi-layer shell structure for a vehicle and method of providing a multi-layer shell structure for a vehicle. The multi-layer structure includes a thermal protection system (TPS) layer, a structural layer connected to the TPS layer, and a high tensile fabric barrier layer bonded to the structural layer. Room-temperature-vulcanizing silicone may be used to bond the TPS layer to the structural layer and bond the high tensile fabric barrier layer to the structural layer. The high tensile fabric barrier layer may create a seal on the structural layer. The multi-layer shell structure may include inner shell enclosing a passenger and/or cargo compartment and an annulus between the inner shell and the high tensile fabric barrier layer. The high tensile fabric barrier layer may prohibit entry of gas into the annulus in the event a hole is created through a portion of the multi-layer shell structure.

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Patent Owner(s)

Patent OwnerAddress
THE BOEING COMPANY100 NORTH RIVERSIDE PLAZA CHICAGO IL 60606

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bland, Mitchell C Houston, US 1 0

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