NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
THERMAL INSULATION SYSTEMSThermal insulation systems and with methods of their production. The thermal insulation systems incorporate at least one reflection layer and at least one spacer layer in an alternating pattern. Each spacer layer includes a fill layer and a carrier layer. The fill layer may be separate from the carrier layer, or it may be a part of the carrier layer, i.e., mechanically injected into the carrier layer or chemically formed in the carrier layer. Fill layers contain a powder having a high surface area and low bulk density. Movement of powder within a fill layer is restricted by electrostatic effects with the reflection layer combined with the presence of a carrier layer, or by containing the powder in the carrier layer. The powder in the spacer layer may be compressed from its bulk density. The thermal insulation systems may further contain an outer casing. Thermal insulation systems may further include strips and seams to form a matrix of sections. Such sections serve to limit loss of powder from a fill layer to a single section and reduce heat losses along the reflection layer.
Document ID
20060009005
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Augustynowicz, Stanislaw D.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Fesmire, James E.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
August 23, 2013
Publication Date
November 22, 2005
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Application Number: US-Patent-Appl-302315
Patent Number: NASA-Case-KSC-1202-2
Patent Number: US-Patent-6,967,051
Patent Application Number: US-Patent-Appl-939286
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-Case-KSC-1202-2|US-Patent-6,967,051
Patent Application
US-Patent-Appl-302315|US-Patent-Appl-939286
No Preview Available