DocumentCode :
2688139
Title :
Cryo-cooled sapphire oscillator for the Cassini Ka-band experiment
Author :
Dick, G. John ; Wang, Rabi T.
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear :
1997
fDate :
28-30 May 1997
Firstpage :
1009
Lastpage :
1014
Abstract :
We present design aspects of a cryogenic sapphire oscillator which is being developed for ultra-high short term stability and low phase noise in support of the Cassini Ka-band Radio Science experiment. With cooling provided by a commercial cryocooler instead of liquid helium, this standard is designed to operate continuously for periods of a year or more. Performance targets are a stability of 3×10-15 (1 second⩽τ⩽100 seconds) and a phase noise of -73 dB/Hz @ 1 Hz measured at 34 GHz. Test results are reported for several subsystems; including cryocooler, vibration isolation system, and ruby compensating element
Keywords :
circuit stability; compensation; cryogenic electronics; millimetre wave oscillators; phase noise; sapphire; space vehicle electronics; 34 GHz; Al2O3; Cassini Ka-band experiment; cryo-cooled oscillator; phase noise; ruby compensating element; sapphire oscillator; ultra-high short term stability; vibration isolation system; Cooling; Cryogenics; Degradation; Frequency; Laboratories; Oscillators; Phase noise; Propulsion; Stability; Temperature;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Frequency Control Symposium, 1997., Proceedings of the 1997 IEEE International
Conference_Location :
Orlando, FL
Print_ISBN :
0-7803-3728-X
Type :
conf
DOI :
10.1109/FREQ.1997.639224
Filename :
639224
Link To Document :
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