Vertical takeoff and landing aircraft

Aeronautics and astronautics – Aircraft – heavier-than-air – Airplane and fluid sustained

Patent

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244120, B64C 130

Patent

active

039661423

ABSTRACT:
A Vertical Takeoff and Landing (VTOL) aircraft that has a small stowage envelope made possible by articulation of the aircraft empennage and fuselage, the aircraft having propulsion units capable of providing in all attitudes of the empennage with respect to said fuselage engine wash of the empennage thereby insuring aircraft control without additional reaction stabilizing units.

REFERENCES:
patent: 3002719 (1961-10-01), Weiland et al.
patent: 3165280 (1965-01-01), Shaa-Tang Lee

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