A VTOL FLIGHT SYSTEM The present invention relates to a system of aircraft involving a fixed-wing aircraft 5 (100) and at least an external agent (199) capable of VTOL that form a momentary short / vertical takeoff and landing (STOL / VTOL) flight system when required. Embodiments of the external agent (199) include rotary-wing aircraft (200). Most Illustrative Diagram: FIG. 3(b) cv)r a-L
A VTOL FLIGHT SYSTEM
2021-10-07
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
NTRS | 1966
Proposed VTOL flight requirements
Engineering Index Backfile | 1963
|Flight safety in VTOL aircraft
Engineering Index Backfile | 1963
|AIAA | 1968
|Optimum VTOL flight paths under constraint
AIAA | 1970
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