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

Crossref DOI link: https://doi.org/10.3103/S0025654418080083

Published Online: 2019-07-30

Published Print: 2018-09

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

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