NASA NTRS · 20060037902
Space Flyable Hg(sup +) Frequency Standards
Abstract
We discuss a design for a space based atomic frequency standard (AFS) based on Hg(sup +) ions confined in a linear ion trap. This newly developed AFS should be well suited for space borne applications because it can supply the ultra-high stability of a H-maser but its total mass is comparable to that of a NAVSTAR/GPS cesium clock, i.e., about 11kg. This paper will compare the proposed Hg(sup +) AFS to the present day GPS cesium standards to arrive at the 11 kg mass estimate. The proposed space borne Hg(sup +) standard is based upon the recently developed extended linear ion trap architecture which has reduced the size of existing trapped Hg(sup +) standards to a physics package which is comparable in size to a cesium beam tube. The demonstrated frequency stability to below 10(sup -15) of existing Hg(sup +) standards should be maintained or even improved upon in this new architecture. This clock would deliver far more frequency stability per kilogram than any current day space qualified standard.
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
Prestage, John D., Maleki, Lute. 1994-06-01. Space Flyable Hg(sup +) Frequency Standards. https://ntrs.nasa.gov/citations/20060037902
Cite the original work for its findings. Save a collection to share your selection of sources.