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Assessing Parameters of the Coplanar Components of Perturbing Accelerations Using the Minimal Number of Optical Observations
Baranov A., Agapov V., Golosova N., Karatunov M.
. The approach described in this article makes it possible to determine the spacecraft’s orbit after the maneuver
Rational schemes of controlled motion of space tether systems
Razoumny Y.N., Kupreev S.A.
The article deals with the prospective trends of practical use of orbital tether systems
Even and odd crystal fields on Fe2+ions, local lattice distortion parameters, electron-deformation interaction, and magnetoelectric coupling in FeCr2O4
Vasin K.V., Eremin M.V.
are determined. Data on local lattice distortions are systematized. The parameter of the electron
Low-energy lunar transfer design using high- and low-thrust on ballistic capture trajectories
Ivanyukhin A., Ivashkin V.V., Petukhov V., Yoon S.W.
) to the Moon into a ballistic capture orbit within the ephemeris model of four-bodies, including: Earth, Moon
Overview of differential VLBI observations of lunar orbiters in SELENE (Kaguya) for precise orbit determination and lunar gravity field study
Hanada H., Iwata T., Liu Q., Kikuchi F., Matsumoto K., Goossens S., Harada Y., Asari K., Ishikawa T., Ishihara Y., Noda H., Tsuruta S., Petrova N., Kawano N., Sasaki S., Sato K., Namiki N., Kono Y., Iwadate K., Kameya O., Shibata K., Tamura Y., Kamata S., Yahagi Y., Masui W., Tanaka K., Maejima H., Hong X., Ping J., Shi X., Huang Q., Aili Y., Ellingsen S., Schlüter W.
-frequency VLBI was employed in order to improve the accuracy of the orbit determination obtained from the phase
Orbital order parameter in La0.95Sr0.05MnO 3 probed by electron spin resonance
Deisenhofer J., Kochelaev B., Shilova E., Balbashov A., Loidl A., Krug Von Nidda H.
investigated and analyzed in the paramagnetic regime across the orbital ordering transition. From
THE GEOSTATIONARY ORBIT IN THE LIGHT OF THE COMMON HERITAGE OF MANKIND (INTERNATIONAL LEGALASPECTS)
Mirzaee Siavash
Background/Objectives: since the geostationary orbit, is a limited resource located in the outer
Optimal formation and replenishment of lunar satellite constellations
Baranov A.A., Grishko D.A., Vasilkov B.O.
. It is supposed that the orbital inclination was formed during the transfer to the orbit around the Moon
ПРОЕКТИРОВАНИЕ МЕЖПЛАНЕТНЫХ ПЕРЕЛЁТОВ КОСМИЧЕСКИХ АППАРАТОВ. ОТ ЗЕМЛИ ДО ТИТАНА. ГРАВИТАЦИОННЫЙ МАНЁВР
Русанова Н.А.
The article analyzes Saturn's satellite Titan and the features of reaching the corresponding orbit
The binary star θ1Ori C: Orbital elements, evolutionary parameters and chemical composition
Rzaev A.K., Shimansky V.V., Kolbin A.I.
a methodical approach for the spectroscopic study of the orbital motions of both components

Страница 6 из 4657

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