| 摘要 |
PROBLEM TO BE SOLVED: To provide a missile excellent in flying stability, in which the center of gravity of the missile can be provided in a forward position, and an inertial moment can be minimized by concentrating a load in the axial direction of a body around the center of gravity. SOLUTION: A plurality of stabilizing fins 14 is radially mounted on a rear portion of a substantially cylindrical missile body 12 of the missile 10. The missile 10 is stored in a container described below by folding the stabilizing fins 14 when it is loaded on an airplane, and the stabilizing fins 14 are radially extended when the missile is emitted from the airplane. The missile body 12 includes a stepped part 12a substantially in the axial center position, and the front part 12b of the missile body is formed with a diameter larger than that of the rear part 12c. A balancer 26 is attached to a front end portion of a power control circuit 34. COPYRIGHT: (C)2007,JPO&INPIT
|
