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] . Controllability ensuring during stages separation of launch vechicle low controller effectiveness of second stage. Kosm. nauka tehnol. 2001 ;7(Supplement1):082-088.
. Controlled levitators for space technologies. Kosm. nauka tehnol. 2001 ;7(2-3):016-026.
. Definition of critical loading of loss of stability for three layer payload fairing with elastic longitudinal joints. Kosm. nauka tehnol. 2001 ;7(Supplement1):025-029.
. Definition of disturbing moment effecting on satellite in flight by telemetry data. Kosm. nauka tehnol. 2001 ;7(Supplement1):067-068.
. Dependence of capacity for work of muscles on blood circulation. Kosm. nauka tehnol. 2001 ;7(Supplement1):179-182.
. Determination of spacecraft motion parameters by Doppler gauges system. Kosm. nauka tehnol. 2001 ;7(4):137-140.
. Development system of metrological maintenance for radio-navigation fields of satellite systems. Kosm. nauka tehnol. 2001 ;7(4):122-125.
. The diffusion model of extragalactic radio source extended components. Kosm. nauka tehnol. 2001 ;7(supplement2):105-109.
. Dusty particles – possible source of Rydberg states formation in low ionosphere. Kosm. nauka tehnol. 2001 ;7(supplement2):034-035.
. On elastic stability of three layer payload fairing with discrete longitudinal links for launch vehicle. Kosm. nauka tehnol. 2001 ;7(Supplement1):030-033.