NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Lightweight Thermal Insulation for a Liquid-Oxygen TankA proposed lightweight, reusable thermal-insulation blanket has been designed for application to a tank containing liquid oxygen, in place of a non-reusable spray-on insulating foam. The blanket would be of the multilayer-insulation (MLI) type and equipped with a pressure-regulated nitrogen purge system. The blanket would contain 16 layers in two 8-layer sub-blankets. Double-aluminized polyimide 0.3 mil (.0.008 mm) thick was selected as a reflective shield material because of its compatibility with oxygen and its ability to withstand ionizing radiation and high temperature. The inner and outer sub-blanket layers, 1 mil (approximately equals 0.025 mm) and 3 mils (approximately equals 0.076 mm) thick, respectively, would be made of the double-aluminized polyimide reinforced with aramid. The inner and outer layers would provide structural support for the more fragile layers between them and would bear the insulation-to-tank attachment loads. The layers would be spaced apart by lightweight, low-thermal-conductance netting made from polyethylene terephthalate.
Document ID
20110016301
Acquisition Source
Johnson Space Center
Document Type
Other - NASA Tech Brief
Authors
Willen, G. Scott
(Technology Applications, Inc. Boulder, CO, United States)
Lock, Jennifer
(Technology Applications, Inc. Boulder, CO, United States)
Nieczkoski, Steve
(Technology Applications, Inc. Boulder, CO, United States)
Date Acquired
August 25, 2013
Publication Date
October 1, 2005
Publication Information
Publication: NASA Tech Briefs, October 2005
Subject Category
Composite Materials
Report/Patent Number
MSC-23099
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available