NASA NTRS · 20060014044
Small Mercury Ion Clock for On-board Spacecraft Navigation
Abstract
I.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.
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Prestage, John D., Chung, Sang, Le, Thanh, Hamell, R., Maleki, Lute, Tjoelker, Robert. 2004-01-01. Small Mercury Ion Clock for On-board Spacecraft Navigation. https://ntrs.nasa.gov/citations/20060014044
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