NASA NTRS · 19740000049
Thrust vector control for V/STOL aircraft
Abstract
To 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.
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Toney, E. W.. 1974-05-01. Thrust vector control for V/STOL aircraft. https://ntrs.nasa.gov/citations/19740000049
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