Surface tension confined liquid cryogen cooler
AssigneeThe United States of America as represented by the Administrator of the National Aeronautics and Space Administration
InventorsStephen H. Castles, Michael E. Schein
Life of this patent
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Abstract
A cryogenic cooler is provided for use in craft such as launch, orbital and space vehicles subject to substantial vibration, changes in orientation and weightlessness. The cooler contains a small pore, large free volume, low density material to restrain a cryogen through surface tension effects during launch and zero-g operations and maintains instrumentation within the temperature range of 10.degree.-140.degree. K. The cooler operation is completely passive, with no inherent vibration or power requirements.
Claims22
A cryogenic cooler for use in craft such as launch, orbital and space vehicles subject to changes in orientation and conditions of vibration and weightlessness comprising:
- an insulated tank;
- a porous open celled sponge-like material disposed substantially throughout the contained volume of said insulated tank;
- a cryogenic fluid disposed within said sponge-like material;
- a cooling finger immersed in said cryogenic fluid, said finger extending from inside said insulated tank externally to an outside source such as an instrument detector for the purpose of transmitting heat from said outside source into said cryogenic fluid;
- means for filling said insulated tank with cryogenic fluid;
- and
- means for venting vaporized cryogenic fluid from said insulated tank;
- wherein said sponge-like material is of such pore size that the surface tension of said cryogenic fluid is effective to maintain said liquid cryogenic fluid suspended within said sponge-like material during conditions of vibration, changes in said cooler orientation and zero gravity environments, and
- wherein heat entering said cooling dewar through said cooling finger is conducted at a precise temperature through said cooling finger and therefrom into said cryogenic fluid contained within said tank, said heat being dissipated by vaporization and expulsion of cryogen through said vent means.
A process for cooling spaced based instruments for use in craft such as launch, orbital and space vehicles subject to changes in orientation and conditions of vibration and weightlessness which comprises:
- placing a liquid cryogen in an insulated tank having a porous open-celled sponge-like material disposed substantially throughout the contained volume of said insulated tank, wherein said sponge-like material is of such pore size that the surface tension of said liquid cryogen is effective to maintain said liquid cryogen suspended within said sponge-like material during conditions of vibration, changes in cooler orientation and zero-gravity environments;
- placing one end of a cooling rod within said liquid cryogen;
- attaching the opposite end of said cooling finger to instrumentation located external to said cooler, thereby enabling heat generated by said instrumentation to transfer to said cooling rod, and subsequently transfer heat from said cooling rod to said liquid cryogen;
- venting any vaporized cryogen formed by the heat transferrred into said cryogen away from said insulated tank such that the temperature of the liquid cryogen, cooling rod and instrumentation remains at a predetermined level.
Dependencies are inferred from the claim text.