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Electromechanical drive for rotary mechanisms in spacecraft

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dc.contributor.author Tsukanov O.N. en
dc.contributor.author Lopatin D.B. en
dc.contributor.author Poluektov E.A. en
dc.date.accessioned 2018-10-16T06:53:44Z
dc.date.available 2018-10-16T06:53:44Z
dc.date.issued 2009
dc.identifier.issn 1068798X
dc.identifier.uri http://dspace.susu.ru/handle/0001.74/20608
dc.description.abstract It has been shown the advantages of electromechanical drive of angular rotation with torque ac converter-fed motor, epicyclic gear, and with cylinder-conic engagement in comparison with existing drives of the same intention. The block diagram of the drive and of reductor engagement, and also some recommendations of how to calculate it are presented. © Allerton Press, Inc. 2009. en]
dc.language.iso English
dc.relation.ispartof Russian Engineering Research en]
dc.subject AC converter en]
dc.subject Angular rotations en]
dc.subject Block diagrams en]
dc.subject Electromechanical drive en]
dc.subject Epicyclic gears en]
dc.subject Torque converters en]
dc.title Electromechanical drive for rotary mechanisms in spacecraft en
dc.type Article en]
dc.identifier.doi 10.3103/S1068798X09020026
dc.identifier.scopus https://www.scopus.com/inward/record.uri?eid=2-s2.0-66449102713&doi=10.3103%2fS1068798X09020026&partnerID=40&md5=0701ba05208e2a0e078da7c83c6d0940

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