| 摘要 |
PROBLEM TO BE SOLVED: To provide a launcher which is used for backwardly launching a guided missile from an aircraft, can reduce the aerodynamic drag of the aircraft when the missile is mounted on the aircraft and after the missile is launched, and can protect a propulsive device from a risk that ice blocks, birds, etc., in the air come into collision with and break a weather seal in the nozzle of the device and protects a random from external environments, such as the aerodynamic heating, aerodynamic loading, rain, etc. SOLUTION: A launcher 7 for backwardly launching a guided missile 3 from an aircraft is provided with a wing guide rail 10 which houses expansion wings 5 having large aerodynamic drags in folded states and, in addition, guides expansion wings A5 and F19 until the wings A5 and F19 pass through the launcher 7, a cover A8 which protects the nozzle 6, etc., of a propulsive device 4 and, in addition, reduces the aerodynamic drag of the missile 3, and a cover F9 which protects a radome.
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