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Thrust augmented spin recovery deviceYaw control surfaces were developed for a jet propelled aircraft. A thrust augmented rudder is disposed above the jet exhaust stream and a thrust rudder tab extends downward into the jet exhaust stream. These components are cooperatively deflected to generate yawing moments for directional control of the aircraft.
Document ID
19810010604
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Berrier, B. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
December 2, 1980
Subject Category
Aircraft Stability And Control
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-727503
Patent Number: US-PATENT-4,236,684
Patent Number: NASA-CASE-LAR-11970-2
Patent Application Number: US-PATENT-APPL-SN-034104
Accession Number
81N19130
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-4,236,684|NASA-CASE-LAR-11970-2
Patent Application
US-PATENT-APPL-SN-727503|US-PATENT-APPL-SN-034104

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