Russian Projects of Space Missions for Astrometry

Astronomy and Astrophysics – Astronomy

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Scientific paper

Since 1994 Institute of Astronomy of Russian Academy of Sciences is working on conception of astrometrical instrument of new generation under contract with Russian Space Agency. After HIPPARCOS mission it is obvious that necessary accuracy for modern astrometry is micro-arcseconds. The only way to approach this level is pupil interferometry outside atmosphere. The first Russian project was pair of twin Michelson interferometers with coincided bases. It consisted of 40-cm input telescopes and had baseline 4 meters long; its limiting magnitude was about 20^m and expected accuracy 2-4 mks. As this devise was proposed to be russian-american experiment for International Space Station, and NASA did not support it, the project was not move up. This is why improved conception of slightly diminished arcmeter-interferometer OSIRIS was proposed as national space project, and it is adopted to the Russian Federal Space Program for the period 2012-2015. Input optic of the OSIRIS will be of 20-cm aperture, and baseline will be 200 cm. It seems to be enough to get position accuracy of single measurement about 4-8 mks at arc range from 30 to 105 degrees, and limiting magnitude being 18^m. There are some technical invents that guarantee these parameters. The OSIRIS mission will establish referred to the ICRS inertial celestial reference frame in optic independent of epoch, that leads to new tasks of astrometry. The astrometrical instrument of new generation may be used for positioning of near-Earth probes as well as of ground objects. Using the same technology it became possible to point narrow-field telescope to any target with the same accuracy. A really desired for this aims accuracy is only milliseconds, and just for these applied experiments LIDA project was proposed last year. It will be suitable for bright sources above 12^m and it will measure instant positions with accuracy 1 mas. The LIDA will be low-mass and compact device suitable for launch by conversional rocket of light class.

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