Tokyo University of Science
Department of Mechanical Engineering
Faculty of Science and Technology
Space Systems Lab.

Since it is difficult to simulate the motion of the aircraft during the deployment of the deceleration chute, we try to evaluate the yaw and roll motion of the aircraft after the deployment of the deceleration chute by using a mini-scale model of WIRES#015. In order to observe the motion of the aircraft in detail, the model was made larger and lighter based on the dynamics of the aircraft.