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BASG thermomechanical pump helium 2 transfer testsThe purpose of the effort described was to perform experiments and calculations related to using a thermomechanical pump in the space-based resupply of the Space Infrared Telescope Facility (SIRTF) with Helium 2. Thermomechanical (fountain effect) pumps have long been suggested as a means for pumping large quantities of Helium 2. The unique properties of Helium 2 have made it useful for cooling space instruments. Several space science missions, including SIRTF, are now being planned which would benefit greatly from on-orbit resupply of Helium 2. A series of experiments were performed to demonstrate that large volumes of Helium 2 can be transferred with a thermomechanical pump at high flow rates and at high efficiency from one dewar to another through valves and lines that are similar to the plumbing arrangement that would be necessary to accomplish such a transfer on-orbit. In addition, temperature, pressure, and flow rate data taken during the tests were used to verify and refine a computer model which was developed.
Document ID
19900011781
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mills, G. L.
(Ball Aerospace Systems Div. Boulder, CO, United States)
Newell, D. A.
(Ball Aerospace Systems Div. Boulder, CO, United States)
Urbach, A. R.
(Ball Aerospace Systems Div. Boulder, CO, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-177541
NAS 1.26:177541
A-90127
Accession Number
90N21097
Funding Number(s)
PROJECT: RTOP 188-78-44
CONTRACT_GRANT: NAS2-11979
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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