Optimum Design of a Fault Tolerant Linear Electromechanical Actuator for the Lower Stage Thrust Vector Control of a Satellite Launch Vehicle
12th, European space mechanisms and tribology symposium; proceedings of ESMATS ; 2007 ; Liverpool
2007-01-01
22 pages
Held on CD-ROM; Shelved in Conference Records
Conference paper
English
Space mechanisms , Tribology , ESMATS , ESA
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