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Determining Temperature Differential to Prevent Hardware Cross-Contamination in a Vacuum ChamberWhen contamination-sensitive hardware must be tested in a thermal vacuum chamber, cross-contamination from other hardware present in the chamber, or residue from previous tests, becomes a concern. Typical mitigation strategies involve maintaining the temperature of the critical item above that of other hardware elements at the end of the test. A formula for relating the pumping speed of a chamber, the surface area of contamination sources, and the temperatures of the chamber, source, and contamination-sensitive items has been developed. The formula allows the determination of a temperature threshold about which contamination will not condense on the sensitive items. It defines a parameter alpha that is the fraction given by (contaminant source area)/[chamber pumping speed (time under vacuum) 0.5]. If this parameter is less than 10(exp -6), cross-contamination from common spacecraft material will not occur when the sensitive hardware is at the same temperature as the source of contamination (The chamber is isothermal within 5 C.). Knowing when it becomes safe to have the hardware isothermal permits faster and easier thermal transitions when compared with maintaining an arbitrary temperature differential between parts. Furthermore, the standard temperature differential may not be adequate under some conditions (alpha>10(exp -4)).
Document ID
20130011247
Acquisition Source
Goddard Space Flight Center
Document Type
Other - NASA Tech Brief
Authors
Hughes, David
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 27, 2013
Publication Date
March 1, 2013
Publication Information
Publication: NASA Tech Briefs, March 2013
Subject Category
Quality Assurance And Reliability
Report/Patent Number
GSC-16244-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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