FLIGHT VEHICLE THAT HAVE THE VALVE ASSEMBLY FOR ATTITUDE CONTROL AND AERODYNAMIC CONTROL

摘要

The present invention relates to a flight vehicle capable of controlling attitude and aerodynamic force by side thrust. According to the present invention, the flight vehicle comprises: a flight vehicle; a body installed in the flight vehicle and including a plurality of rotating blades to control aerodynamic force of the flight vehicle; a rotating unit installed in the body and making the plurality of rotating blades move along a circumferential direction of the body; a gas supply unit installed in the body; and a side thrust generation unit installed in the body and receiving gas from a gas generator to generate side thrust for controlling an advancing direction of the flight vehicle. According to the present invention, in a system which generates force to control the direction and attitude of the flight vehicle by using the side thrust applied to a side of the flight vehicle, the side thrust can be controlled.