One variant of the orbit for a near-earth radio interferometer

Details One variant of the orbit for a near-earth radio interferometer One variant of the orbit for a near-earth radio interferometer

Sep 1988

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1988pazh...14..851l&link_type=abstract

Pis'ma v Astronomicheskii Zhurnal (ISSN 0320-0108), vol. 14, Sept. 1988, p. 851-855. In Russian.

Astronomy and Astrophysics

Astronomy

2

Earth Orbits, Orbit Calculation, Radio Interferometers, Very Long Base Interferometry, Ecliptic, Lunar Orbits, Spacecraft Orbits, Three Body Problem

Scientific paper

The paper described a version of a terrestrial orbit with a typical size of 106km which can be used for very long base interferometry (at the second stage of experiment). The paper demonstrates the practical stability of the orbit and evaluates the necessary energy input for putting a spacecraft into such an orbit. The research is based on the preliminary analysis of a special class of 3-dim periodic orbits in the problem of three bodies.

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