The aircraft has an elongated fuselage or hull section, jets for yawing the fuselage section while in flight between a low aspect ratio position in alignment with the direction of movement of the aircraft and a high aspect ratio position transverse to the direction of movement of the aircraft. The aircraft is delta-shaped.
Landing Arrangement for Aerial Vehicle
1965
1 pages
Report
No indication
English
Landing arrangement for aerial vehicle Patent
NTRS | 1965
|European Patent Office | 2025
|European Patent Office | 2024
|Landing arrangement for aerial vehicles Patent
NTRS | 1962
|European Patent Office | 2024