Missile deployment apparatus

Ammunition and explosives – Shells – With secondary shells

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Details

102393, F42B 1500, F42B 1328, F42B 1350

Patent

active

044559437

ABSTRACT:
Apparatus for deploying one or more submissiles (15) from a carrier missile (25) whereby each submissile (15) is deployed into a flight path which is initially parallel to a streamline (20) of the fluid flow contiguous to the carrier missile (25). An ejection mechanism (45) has a submissile support member (105) oriented substantially parallel to the streamline (20) at the point where the submissile (15) is separated from the support member (105). The ejection mechanism (45) also provides a minimum side force to the submissile (15) which is proportional to a speed of the carrier vehicle (25). Provisions are also made to reduce or minimize any change in the aerodynamic characteristics of the carrier missile (25) after a submissile (15) has been deployed.

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patent: 4210082 (1980-07-01), Brothers

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