NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Cryogenic leak testing of tube fittings/valvesA high pressure and variable temperature cryogenic leak testing system was conceived and designed in order to conduct leakage testing of pipe fittings/valves in liquid hydrogen supply lines of the Space Shuttle. The system can create a continuous testing environment of variable temperature, 5.5 to about 300 K, and variable pressure, 0.01 to about 70 x 10 exp 5 Pa, with a large sample space, 90 mm diameter x 228 mm length, and at low operating cost. In terms of cryogenic leak testing the system has a special capability for extensive applications. The system comprised a variable temperature cryostat, a high pressure sample chamber, a vacuum pumping station, gas flow control system, pressure and temperature control systems, and leak detecting and measuring systems. A general discussion of cryogenic leak testing methods is also presented.
Document ID
19920072100
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Jia, L. X.
(NASA John F. Kennedy Space Center Cocoa Beach, FL, United States)
Moslemian, D.
(NASA John F. Kennedy Space Center Cocoa Beach, FL, United States)
Chow, W. L.
(Florida Atlantic University Boca Raton, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Publication Information
Publication: Cryogenics
Volume: 32
Issue: 9 19
ISSN: 0011-2275
Subject Category
Engineering (General)
Accession Number
92A54724
Funding Number(s)
CONTRACT_GRANT: NAG10-0083
CONTRACT_GRANT: NAS10-11569
Distribution Limits
Public
Copyright
Other

Available Downloads

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