NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Cryogenic foam insulation for LH2 fueled subsonic transportsShortages of petroleum-based aircraft fuels are foreseen before the end of the century. To cope with such shortages, NASA is developing a commercial aircraft which can operate on liquid hydrogen. Various foam insulators for LH2 storage are considered in terms of thermal performance and service life. Of the cryogenic foams considered (plain foam, foam with flame retardants and fiberglass reinforcement, and foam with vapor barriers), polyurethane foams were found to be the best. Tests consisted of heating a 5 cm layer of insulation around an aluminum tank containing LH2 to 316 K, and then cooling it to 266 K, while the inner surface was maintained at LH2 temperature (20 K).
Document ID
19780052094
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sharpe, E. L.
(NASA Langley Research Center Hampton, Va., United States)
Helenbrook, R. G.
(Bell Aerospace Textron Buffalo, N.Y., United States)
Date Acquired
August 9, 2013
Publication Date
May 1, 1978
Subject Category
Nonmetallic Materials
Report/Patent Number
AIAA PAPER 78-875
Meeting Information
Meeting: Thermophysics and Heat Transfer Conference
Location: Palo Alto, CA
Start Date: May 24, 1978
End Date: May 26, 1978
Sponsors: American Society of Mechanical Engineers, American Institute of Aeronautics and Astronautics
Accession Number
78A36003
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available