发明名称 Missile launcher for aircraft
摘要 A mechanism rapidly and repetitively launches missiles from inside an aircraft during flight. One or more missiles are carried and launched through a tube protruding through the front of the aircraft thus obviating the necessity for bomb bay or other sizeable, open doors. The aircraft interior may be used as a large accumulator so that pressurized internal air is utilized as the propellant when admitted to a breech. Thus, a "cold" launch is achieved negating the possibility of a "hang fire". Multiple missiles can be carried in revolving chambers which are capable of rapid rotation into firing position. The advantages of the system include the ability to launch at high aircraft altitudes and speeds with the missile moving toward the target.
申请公布号 US4040334(A) 申请公布日期 1977.08.09
申请号 US19760678557 申请日期 1976.04.20
申请人 LOCKHEED AIRCRAFT CORPORATION 发明人 SMETHERS, JR., ROLLO G.
分类号 B64D7/08;F41B11/00;F41F3/06;(IPC1-7):F41F3/06 主分类号 B64D7/08
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