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Thrust vector control for V/STOL aircraftTo deflect exhaust of V/STOL aircraft fan deploy set of rectangular flaps so exhaust stream can be turned as required and then directed through exit nozzles which generate thrust in appropriate direction; lateral deflection of exhaust is provided by yaw vanes.
Document ID
19740000049
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Toney, E. W. (McDonnell-Douglas Corp.)
Date Acquired
August 7, 2013
Publication Date
May 1, 1974
Subject Category
Mechanics
Report/Patent Number
ARC-10788
Report Number: ARC-10788
Accession Number
74B10049
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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