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Electromechanical flight control actuatorAn electromechanical actuator that will follow a proportional control command with minimum wasted energy is developed. The feasibility of meeting space vehicle actuator requirements using advanced electromechanical concepts is demonstrated. Recommendations for further development are given.
Document ID
19760015172
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
February 1, 1976
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-147557
R76-29
Report Number: NASA-CR-147557
Report Number: R76-29
Accession Number
76N22260
Funding Number(s)
CONTRACT_GRANT: NAS9-14331
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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