| 1u cubesat platform design N Zosimovych International Journal of Aerospace Sciences 8, 1-7, 2020 | 9 | 2020 |
| Modeling of spacecraft centre mass motion stabilization system N Zosimovych Int. Ref. Journ. of Eng. and Science (IRJES).[Online] 7 (4), 34-41, 2017 | 9 | 2017 |
| Commercial Launch Vehicle Design N Zosimovych LAP LAMBERT Academic Publishing, 2016 | 7 | 2016 |
| Modeling the Integrated Guidance System of a Commercial Launch Vehicle N Zosimovych International Refereed Journal of Engineering and Science (IRJES) 3 (6), 39-54, 2014 | 7 | 2014 |
| Increasing the accuracy of the center of mass stabilization of space probe N Zosimovych International Conference on Новината за Напреднали Наук а 10, 31-37, 2017 | 6 | 2017 |
| Improving the spacecraft center of mass stabilization accuracy N Zosimovych IOSR Journ. of Eng.(IOSRJEN) 7 (6), 7-14, 2017 | 6 | 2017 |
| Laminar flow investigation between a stationary and a rotating disk with a source at centre A Singh, N Zosimovych Eng. Sci./Mech 1, 1-10, 2016 | 5 | 2016 |
| Communication system for nanosatellite earth observation N Zosimovych Advances in Aerospace Science and Technology 6 (03), 134-157, 2021 | 4 | 2021 |
| Mission capability assessment of 3D printing Cubesats Z Chen, N Zosimovych IOP Conference Series: Materials Science and Engineering 608 (1), 012025, 2019 | 4 | 2019 |
| 3D printing CubeSat: a low-cost mode of space exploration N Zosimovych, Z Chen Aeron Aero 2 (5), 320-324, 2018 | 4 | 2018 |
| CubeSat Design and Manufacturing Technique Analysis N Zosimovych, Z Chen Retrieved from IOSR Journal of Engineering: http://www. iosrjen. org/Papers …, 2018 | 4 | 2018 |
| Structural and parametric optimization for flight vehicle structures N Zosimovych development (D&D) 1 (4), 12, 2017 | 4 | 2017 |
| Increasing the Accuracy of the Center of Mass Stabilization of Space Probe with Partially Invariant System N Zosimovych Science and Education, a New Dimension. Natural and Techn. Science 14 (132 …, 2017 | 4 | 2017 |
| Design objectives for a commercial launch vehicle with integrated guidance system N Zosimovych, A Voytsytskyy Novus International Journal of Engineering&Technology 3 (4), 7-28, 2014 | 4 | 2014 |
| Functional Simulation of the Integrated Onboard System for a Commercial Launch Vehicle N Zosimovych International Refereed Journal of Engineering and Science (IRJES) 3 (11), 92-106, 2014 | 4 | 2014 |
| Integrated Guidance System of a Commercial Launch Vehicle N Zosimovych Уральский научный вестник, 36-49, 2014 | 4 | 2014 |
| Selecting Design Objectives for an Integrated Guidance System of a Commercial Launch Vehicle with Application of GPS Technologies N Zosimovych The Open Aerospace Engineering Journal 6 (1), 2013 | 4 | 2013 |
| Flight Transient Estimation of VTOL Aircraft with Propellers N Zosimovych Advances in Aerospace Science and Technology 7 (1), 85-95, 2022 | 3 | 2022 |
| General technique for solving structural and parametri c optimization of flying vehicle structures N Zosimovych Int Conf on Naukowa Przestrze ń Europy 11, 50-63, 2017 | 3 | 2017 |
| Invariant Stabilization Algorithms in a Control System with Rotating Operating Device N Zosimovych American Journ. of Eng. Research (AJER) 6 (10), 297-11, 2017 | 3 | 2017 |
