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Pulsed Optimal Spacecraft Orbit Reorientation by Means of Reactive Thrust Orthogonal to the Osculating Orbit. II

Crossref DOI link: https://doi.org/10.3103/S0025654419010011

Published Online: 2019-09-03

Published Print: 2019-01

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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