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Fluidic emergency roll control systemA fluidic emergency roll control system for aircraft stabilization in the event of primary flight control failure was evaluated. The fluidic roll control units were designed to provide roll torque proportional to an electrical command as operated by two diametrically opposed thrust nozzles located in the wing tips. The control package consists of a solid propellant gas generator, two diametrically opposed vortex valve modulated thrust nozzles, and an electromagnetic torque motor. The procedures for the design, development, and performance testing of the system are described.
Document ID
19740001936
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Haefner, K. B. (General Electric Co. Schenectady, NY, United States)
Honda, T. S. (General Electric Co. Schenectady, NY, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1973
Subject Category
Aircraft
Report/Patent Number
NASA-CR-114588
Accession Number
74N10048
Funding Number(s)
CONTRACT_GRANT: NAS2-5467
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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