On additional errors of float gyroscope during circulation of a carrier rocket
. On additional errors of float gyroscope during circulation of a carrier rocket. Kosm. nauka tehnol. 2009 ;15(6):49-56.
Space-Rocket Vehicles
Advanced stabilization system algorithms of launch vehicle's first stage with attack and sliding angles control
. Advanced stabilization system algorithms of launch vehicle's first stage with attack and sliding angles control. Kosm. nauka tehnol. 2009 ;15(4):72-78.
Integration circuit for motion equation of a space vehicle on the basis of differential-taylor transformation with reduced computing
Integration circuit for motion equation of a space vehicle on the basis of differential-taylor transformation with reduced computing. Kosm. nauka tehnol. 2010 ;16(6):51-56.
Physical foundation for the construction of paraffin-based hybrid rocket engines. Кinetics of melting and combustion
. Physical foundation for the construction of paraffin-based hybrid rocket engines. Кinetics of melting and combustion. Kosm. nauka tehnol. 2011 ;17(3):28-33.
Absorbed acoustic radiation as a factor of the transformation of inertial sensing elements of gyrostabilized platforms into impedance ones. Mixed boundary problem
. Absorbed acoustic radiation as a factor of the transformation of inertial sensing elements of gyrostabilized platforms into impedance ones. Mixed boundary problem. Kosm. nauka tehnol. 2011 ;17(2):22-31.
Non-stationary problem of the interaction of acoustic radiation from rocket carriers with two-sedate gyroscope
. Non-stationary problem of the interaction of acoustic radiation from rocket carriers with two-sedate gyroscope. Kosm. nauka tehnol. 2001 ;7(5-6):021-025.
Feasibility of the ultrasound testing of the first-stage engine of the Zenith rocket carrier. 1.Construction of the physical model of the object to be tested
. Feasibility of the ultrasound testing of the first-stage engine of the Zenith rocket carrier. 1.Construction of the physical model of the object to be tested. Kosm. nauka tehnol. 2001 ;7(5-6):003-007.
The simplest model of the relation between the specific payload cost and specific impulse
. The simplest model of the relation between the specific payload cost and specific impulse. Kosm. nauka tehnol. 2001 ;7(2-3):100-103.
Сontrol system for a light-duty aerospace rocket complex based on a platformless inertial navigation system
. Сontrol system for a light-duty aerospace rocket complex based on a platformless inertial navigation system. Kosm. nauka tehnol. 2001 ;7(2-3):003-015.
Methodological aspects for designing a launch vehicle through the efficiency criterion
. Methodological aspects for designing a launch vehicle through the efficiency criterion. Kosm. nauka tehnol. 2004 ;10(2-3):068-073.