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1Aizenberg Ya.E, 1Zlatkin Yu.M, 2Kalnoguz AN, 2Bataev VA, 2Kuzmin AI. Control on angles of attack and slip of the first stages of the launcher. Kosm. nauka tehnol. 2002 ;8(1):061-080.
1Aizenberg Ya.E. Concept of developing the control system for automatic spacecraft of "Spectrum" series. Kosm. nauka tehnol. 1995 ;1(1):35–46.
1Aizenberg Ya.E, 2Yastrebenetskii MA. Comparison of the safety principles for the control systems for launchers and atomic power stations. Kosm. nauka tehnol. 2002 ;8(1):055-060.
1Aizenberg Ya.E, 2Bataev VA, 2Kuzmin AI. High accuracy stabilization system of launch vehicle with asymmetric configuration when one engine failure is possible. Kosm. nauka tehnol. 1998 ;4(1):64–67.
1Aizenberg Ya.E, 1Bek AV, 1Zlatkin Yu.M, 1Kamenev VP, 1Konorev BM, 2Shcherbachenko VT. Dynamic testing of on-board embedded computer software of missile and spacecraft control system. Kosm. nauka tehnol. 1997 ;3(1):61–74.
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.
1Aleksandrov Yu.V. Perturbed motion of the artificial satellite of the Moon in the project «UkrSelena». Kosm. nauka tehnol. 2009 ;15(1):05-08.
1Alekseev Yu.S, 1Baulin SO, 2Konyukhov SN, 3Fedorov OP, 4Yatskiv Ya.S. Conceptul approaches to the elaboration of State target scientific-technical space program of Ukraine for 2008—2012. Kosm. nauka tehnol. 2008 ;14(1):03-09.
1Alekseev Yu.S, 2Kukushkin VI, 3Levenko AS. Prospects of the rocket-space branch of Ukraine is the rocket system on the basis of the airborne-spase vehicle. Kosm. nauka tehnol. 2006 ;12(4):003-013.
1Alexandrov Ye.Ye., 2Rafalovich OYa. Choosing the power of airborne transmitters in the space stations for digital satellite communication systems. Kosm. nauka tehnol. 1999 ;5(5):21–24.