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1Arlekinova ОЕ. Study of environment parameters that determine ilv «Zenit-3SL» loading during standing before launch. Kosm. nauka tehnol. 2002 ;8(Supplement1):009-011.
1Arlekinova ОЕ, 1Vasilenko AA. Estimate of predictable loading on the base cross-section of ILV «ZENIT-3SL». Kosm. nauka tehnol. 2001 ;7(Supplement1):018-020.
1Artemenko OA, 2Popova AF. The δ-cyclin expression at early stages of embryogenesis of Brassica rapa L. under clinorotation. Kosm. nauka tehnol. 2004 ;10(5-6):211-215.
1Artemenko OA. The altered gravity effect on proliferative system of two-day pea germs. Kosm. nauka tehnol. 2007 ;132(2):043-047.
1Artemenko OA. The importance of cell cycle parameters for the development of space plant growing. Space Science and Technology. 2017 ;23(5):66-71.
1Artemenko OA. Features of plant cell cycle regulation under altered gravity conditions. Kosm. nauka tehnol. 2015 ;21(5):108–112.
1Artiushenko MV, 1Dugin SS, 2Fedorovskyi OD. Simulation and synthesis of satellite constellation for zonal observations of the territory of Ukraine. Kosm. nauka tehnol. 2011 ;17(5):50-57.
1Artyukhova TP. On elastic stability of three layer payload fairing with discrete longitudinal links for launch vehicle. Kosm. nauka tehnol. 2001 ;7(Supplement1):030-033.
1Artyukhova TP. 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.
1Ashchepkova NS, 2Sheptun Yu.D. Mathematical model of the motion of a space vehicle with a manipulator. Kosm. nauka tehnol. 1997 ;3(3):034–042.