Design and Experimental Study of a Turbojet VTOL Aircraft with One-Dimensional Thrust Vectoring Nozzles

Turbojet engines have a slow response and require mechanical assistance to perform vertical take-offs landings. In this paper, we propose take-off landing (VTOL) aircraft that contains one-dimensional thrust vectoring nozzle modules solve the problem of dependence on turbojet. The turbojet engine is placed horizontally in module, rotational speeds are fixed, force along axis remains constant as rotates from horizontal position. composed four modules, whose position attitude control realized by using difference caused different angles vector nozzles. no longer rely speed engine, controlling nozzles makes it easier operate aircraft. placement can reduce thickness fuselage decrease air resistance. process moving prevents blowing directly ground and, thus, reduces effect.