DocumentCode :
1666488
Title :
Rubidium locked oscillator life testing
Author :
McClelland, Tom ; Bhaskar, Nat ; Mallette, Leo A.
Author_Institution :
Frequency Electron. Inc., Mitchel Field, NY, USA
Volume :
4
fYear :
1996
Firstpage :
469
Abstract :
Space programs increasingly use atomic frequency standards (commonly known as atomic clocks) for precision time-keeping and stable frequency generation. A new generation of military communication satellites (Milstar) will carry multiple redundant rubidium atomic frequency standards to meet two requirements-autonomous operation and reduced sensitivity to radiation. A test was developed to monitor the performance of two space qualified rubidium locked crystal oscillators for one year. To date, this represents one of the most extensive long term tests of atomic frequency standards in a space environment. There were several operational, logistic and contractual problems that developed over the test period that were overcome. The test, the test equipment, the test philosophy and some of the problems encountered are described in this paper
Keywords :
artificial satellites; atomic clocks; crystal oscillators; frequency measurement; life testing; measurement standards; military communication; performance evaluation; radiation hardening (electronics); rubidium; satellite communication; space vehicle electronics; time measurement; Milstar; Rb; Rb atomic frequency standards; Rb locked oscillator; atomic clocks; autonomous operation; life testing; long term tests; military communication satellites; multiple redundant frequency standards; precision time-keeping; sensitivity to radiation; space qualified crystal oscillators; stable frequency generation; Artificial satellites; Atomic clocks; Frequency; Global Positioning System; Life testing; Military communication; Military satellites; Oscillators; Stability; Timing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Applications Conference, 1996. Proceedings., 1996 IEEE
Conference_Location :
Aspen, CO
Print_ISBN :
0-7803-3196-6
Type :
conf
DOI :
10.1109/AERO.1996.499681
Filename :
499681
Link To Document :
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