Electromechanical drive for rotary mechanisms in spacecraft

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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