Reusable lunar lander 1Berdnyk OI, 1Lysenko YO, 1Kaliapin MD, 1Buhaienko TK. Reusable lunar lander. Space Science and Technology. 2019 ;25(5):03-10.
Remote sensing payload complex testing for youth australian-ukrainian microsatellite JAUESAT 1Bezuglyi VA, 2Protsan YV, 3Bondarenko SG. Remote sensing payload complex testing for youth australian-ukrainian microsatellite JAUESAT. Kosm. nauka tehnol. 2003 ;9(Supplement1):024-028.
Measuring system for analysis of electromagnetic compatibvility of small satellites 1Belyayev SM, 1Dudkin FL, 1Pronenko VO, 1Korepanov VYe. Measuring system for analysis of electromagnetic compatibvility of small satellites. Space Science and Technology. 2019 ;25(4):29-35.
Results-signal of telemetering measurements at the stage of spacecrafts launch 1Malevinskii SV, 1Mironenko VN, 1Savchenko VV. Results-signal of telemetering measurements at the stage of spacecrafts launch. Kosm. nauka tehnol. 2002 ;8(Supplement1):064-069.
Rotation characteristics of rigid rotor fastened in resilient mountings with a dynamic instability 1Zhyvotov AYu. Rotation characteristics of rigid rotor fastened in resilient mountings with a dynamic instability. Kosm. nauka tehnol. 2002 ;8(Supplement1):058-063.
Method of deformations stresses determination at the shells stretching of spherical bottoms 1Ubyz'kyi NN. Method of deformations stresses determination at the shells stretching of spherical bottoms. Kosm. nauka tehnol. 2002 ;8(Supplement1):057-058.
Analitical models of vibrational diagnostics of aerospase assigning shells 1Titova ОA. Analitical models of vibrational diagnostics of aerospase assigning shells. Kosm. nauka tehnol. 2002 ;8(Supplement1):054-056.
Vibration loads tests of products 1Serbyna ОМ. Vibration loads tests of products. Kosm. nauka tehnol. 2002 ;8(Supplement1):051-054.
Laser purification model for spacecrafts illuminators 1Opachko II. Laser purification model for spacecrafts illuminators. Kosm. nauka tehnol. 2002 ;8(Supplement1):028-031.
Securing an efficiency of automatic valves in space vehicle's pneumohydraulic systems under cryogenic temperature conditions 1Bondarenko OV, 1Vorotintsev EV, 2Zevako VS. Securing an efficiency of automatic valves in space vehicle's pneumohydraulic systems under cryogenic temperature conditions. Kosm. nauka tehnol. 2002 ;8(Supplement1):012-016.