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Enclosed capillary device for low gravity management of He IITo transfer He II in space, a large tank must be drained at low gravity. This paper describes and analyzes an enclosed gallery device designed for collecting and delivering He II to a pump. The device allows most of the liquid to move about in the tank while it maintains a liquid flow to the pump. Only the liquid in the screen-covered gallery channels and in the upper and lower receivers is contained. The device operates by providing surface tension dominated liquid paths from all locations within the tank to the lower receiver, which houses the pump. Since the fluid pressure in the channels may be below the saturated vapor pressure, an analysis of He II cavitation is performed to determine if cavitation will occur. The effect of heat dissipation from the pump is examined to determine if it may result in nucleation of boiling. It is concluded that this enclosed device can meet the requirements for transfer of He II under the predicted adverse accelerations that will be encountered on-orbit.
Document ID
19890053943
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Frank, D. J.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Yuan, S. W. K.
(Lockheed Missiles and Space Co., Inc. Research and Development Div., Palo Alto, CA, United States)
Date Acquired
August 14, 2013
Publication Date
February 1, 1988
Publication Information
Publication: Cryogenics
Volume: 28
ISSN: 0011-2275
Subject Category
Astronautics (General)
Accession Number
89A41314
Funding Number(s)
CONTRACT_GRANT: NAS2-12051
Distribution Limits
Public
Copyright
Other

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