, Russian Federation
The article is devoted to solving the problem of assessing additional microaccelerations arising as a result of a temperature shock when a small spacecraft leaves the Earth's shadow and dives into it, in order to develop recommendations for controlling the level of microaccelerations in the area of technological equipment intended for the implementation of gravitationally sensitive technological processes on board. small spacecraft
contact mechanics of engineering surfaces, friction and wear of interfaces, tribotechnical materials science, mechanics and control processes, kinematics, dynamics, strength and reliability of machines and structural elements
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