Effiecency criterion for selection of design parameters of aerospace system

1Kalynychenko, DS, 1Baranov, Ye.Yu., 1Poluian, MV
1Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
Space Sci.&Technol. 2016, 22 ;(2):48-51
Section: Spacecraft Dynamics and Control
Publication Language: Ukrainian
We describe method of selection of design parameters for aerospace system, appointed for delivery of micro-satellites to Low-Earth Orbit. The method is developed for the analysis of existing launch vehicles, forming the base design parameters, performance criteria and determination of rational design parameters of aerospace system.
Keywords: aerospace system, design parameters
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