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A superfluid helium system for an LST IR experimentThe results are presented of a study program directed toward evaluating the problems associated with cooling an LST instrument to 2 K for a year by using superfluid helium as the cooling means. The results include the parametric analysis of systems using helium only, and systems using helium plus a shield cryogen. A baseline system, using helium only is described. The baseline system is sized for an instrument heat leak of 50 mw. It contains 71 Kg of superfluid helium and has a total, filled weight of 217 Kg. A brief assessment of the technical problems associated with a long life, spaceborne superfluid helium storage system is also made. It is concluded that a one year life, superfluid helium cooling system is feasible, pending experimental verification of a suitable low g vent system.
Document ID
19760006223
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Breckenridge, R. W., Jr.
(Little (Arthur D.), Inc. Cambridge, MA, United States)
Moore, R. W., Jr.
(Little (Arthur D.), Inc. Cambridge, MA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1975
Subject Category
Engineering (General)
Report/Patent Number
NASA-CR-144688
ADL-C-76779
Report Number: NASA-CR-144688
Report Number: ADL-C-76779
Accession Number
76N13311
Funding Number(s)
CONTRACT_GRANT: NAS5-23335
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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