The main lines of NDT development in space-rockets techniques 1Pogorelov AA, 2Zheltov PN, 3Semenov LP. The main lines of NDT development in space-rockets techniques. Kosm. nauka tehnol. 2008 ;14(3):088-092.
Public join stock company «Ukrainian scientific research institute of manufacturing engineering» ‒ 45 years of creation and application of high technology to Ukraine industry 1Zevako VS, 2Zheltov PN. Public join stock company «Ukrainian scientific research institute of manufacturing engineering» ‒ 45 years of creation and application of high technology to Ukraine industry. Kosm. nauka tehnol. 2008 ;14(3):084-087.
45 years for the Open Joint-Stock Company «Ukrainian Research Institute of Machine-Building Technology». Main historical dates of formation and development Anon. 45 years for the Open Joint-Stock Company «Ukrainian Research Institute of Machine-Building Technology». Main historical dates of formation and development. Kosm. nauka tehnol. 2008 ;14(3):082-083.
Most effective areas for launch vehicles with combustible polyethylene tanks 1Yemets VV. Most effective areas for launch vehicles with combustible polyethylene tanks. Kosm. nauka tehnol. 2008 ;14(1):17-24.
On additional errors of float gyroscope during circulation of a carrier rocket 1Karachun VV, 1Mel’nick VN. On additional errors of float gyroscope during circulation of a carrier rocket. Kosm. nauka tehnol. 2009 ;15(6):49-56.
Advanced stabilization system algorithms of launch vehicle's first stage with attack and sliding angles control 1Kalnoguz AN, 1Tykhovskiy VM, 1Bataev VA, 1Pilguy VN, 1Rymin MN. 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 1Rakushev MYu. 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 1Aktan OYu., 2Zabashta Yu.F, 2Chernyak VYa., 3Orlovskaya SG, 2Svechnikova OS, 3Karimova FF, 3Shkoropado MS. 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 1Karachun VV, 1Mel’nick VN. 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 1Karachun VV, 1Lozovik VG, 1Mel'nik VN, 1Kunderevich EK. 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.