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Small Mercury Ion Clock for On-board Spacecraft NavigationI.Small Ion Clock Approach and Heritage: a) No lasers, uwave cavities, cryogenics, atomic beams, etc. b) Ions are electrically shuttled between separate optical and microwave traps. II. Each trap is optimized for its task: quadrupole for optical state selection; multi-pole for microwave clock. a) Very good stability shown in USNO. Timescale running "open loop." III. "Open loop" operation means no self-measurements of frequency offsets: (Zeeman, ion temperature,... etc.) a) Fewer parts and procedures, produces stable output continuously. IV. Ion clock is not so sensitive to temperature fluctuations a) Measured u:nshielded temperature coefficient of few 10(exp -15) per C. b) No bulky temperature isolation needed.
Document ID
20060014044
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
Authors
Prestage, John D.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Chung, Sang
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Le, Thanh
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hamell, R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Maleki, Lute
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Tjoelker, Robert
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Publication Information
Publication: Proceedings of the 2004 NASA/JPL Workshop on Physics for Planetary Exploration
Subject Category
Physics (General)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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