Optimization of the trajectory of the spacecraft insertion into the system of heliocentric orbits
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DOI: 10.1134/s0010952517020034
Abstract: The possibility of the spacecraft insertion into the system of operational heliocentric orbits has been analyzed. It has been proposed to use a system of several operational heliocentric orbits. On each orbit, the spacecraft makes… read more here.
Keywords: heliocentric orbits; spacecraft; operational heliocentric; insertion system ... See more keywords