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Strategic avionics technology definition studies. Subtask 3-1A3: Electrical Actuation (ELA) Systems Test FacilityFuture aerospace vehicles will require use of the Electrical Actuator systems for flight control elements. This report presents a proposed ELA Test Facility for dynamic evaluation of high power linear Electrical Actuators with primary emphasis on Thrust Vector Control actuators. Details of the mechanical design, power and control systems, and data acquisition capability of the test facility are presented. A test procedure for evaluating the performance of the ELA Test Facility is also included.
Document ID
19950012152
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rogers, J. P.
(Rockwell International Corp. Downey, CA, United States)
Cureton, K. L.
(Rockwell International Corp. Downey, CA, United States)
Olsen, J. R.
(Rockwell International Corp. Downey, CA, United States)
Date Acquired
September 6, 2013
Publication Date
September 30, 1994
Subject Category
Aircraft Stability And Control
Report/Patent Number
SSD94D0298
NAS 1.26:188360
NASA-CR-188360
Report Number: SSD94D0298
Report Number: NAS 1.26:188360
Report Number: NASA-CR-188360
Accession Number
95N18567
Funding Number(s)
CONTRACT_GRANT: NAS9-18880
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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