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Lamp reliability studies for improved satellite rubidium frequency standardIn response to the premature failure of Rb lamps used in Rb atomic clocks onboard NAVSTAR GPS satellites experimental and theoretical investigations into their failure mechanism were initiated. The primary goal of these studies is the development of an accelerated life test for future GPS lamps. The primary failure mechanism was identified as consumption of the lamp's Rb charge via direct interaction between Rb and the lamp's glass surface. The most effective parameters to accelerate the interaction between the Rb and the glass are felt to be RF excitation power and lamp temperature. Differential scanning calorimetry is used to monitor the consumption of Rb within a lamp as a function of operation time. This technique yielded base line Rb consumption data for GPS lamps operating under normal conditions.
Document ID
19820012657
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Frueholz, R. P.
(Aerospace Corp. Los Angeles, CA, United States)
Wun-Fogle, M.
(Aerospace Corp. Los Angeles, CA, United States)
Eckert, H. U.
(Aerospace Corp. Los Angeles, CA, United States)
Volk, C. H.
(Aerospace Corp. Los Angeles, CA, United States)
Jones, P. F.
(Aerospace Corp. Los Angeles, CA, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1982
Publication Information
Publication: NASA. Goddard Space Flight Center Proc. of the 13th Ann. Precise Time and Time Interval (PTTI) Appl. and Planning Meeting
Subject Category
Lasers And Masers
Accession Number
82N20531
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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