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Development of a space qualified Surface Tension Confined Liquid Cryogen Cooler (STCLCC)The Surface Tension Confined Liquid Cryogen Cooler (STCLCC), a new type of cryogenic cooler which is being developed by the NASA-GSFC for spaceflight payloads, is described. The STCLCC will be capable of maintaining instrumentation within the temperature range of 10-120 K and will allow liquid cryogens to be flown in space without the risk of liquid being entrained in the vent gas. A low-density open-cell material in the STCLCC acts as a 'sponge', with the surface tension trapping the liquid cryogen within its pores and keeping the liquid away from the cooler's vent during launch, zero-g operations, and landing. It is emphasized that the STCLCC concept is amenable to a wide variety of applications, whenever a passive low-cost cooler is required or when the on-orbit service of a cooler would increase a mission's lifetime.
Document ID
19880065985
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Castles, Stephen H.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Schein, Michael E.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Engineering (General)
Meeting Information
Meeting: Advances in cryogenic engineering.
Location: Saint Charles, IL
Country: United States
Start Date: June 14, 1987
End Date: June 18, 1987
Accession Number
88A53212
Distribution Limits
Public
Copyright
Other

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