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] Orbit height increase by low thrust in transversal direction. Kosm. nauka tehnol. 2009 ;15(1):09-12.
Manoeuvre to bypass a dangerous zone by a satellite with thruster of low tractive force and radial direction. Kosm. nauka tehnol. 2007 ;13(3):027-030.
Influence of thrust/weight ratio of a space vehicle on a transition duration from a near-earth to a near-lunar orbit. Kosm. nauka tehnol. 2005 ;11(Supplement1):018-020.
Estimation of fuel consumption for maintenance of average height of a space vehicle. Kosm. nauka tehnol. 2004 ;10(Supplement1):063-064.
Bypass maneuver by radial boosting impulse. Kosm. nauka tehnol. 2002 ;8(4):043-048.
Building a group of two satellites without using an on-board thruster. Kosm. nauka tehnol. 2001 ;7(5-6):026-029.
Estimating the distortion of satellite — subsatellite structure under aerodynamic drag. Kosm. nauka tehnol. 1997 ;3(3):030–033.