Aircraft missile launcher sway brace apparatus

Details Aircraft missile launcher sway brace apparatus Aircraft missile launcher sway brace apparatus

1988-02-17

1989-05-16

Brown, David H.

Ordnance

Bomb, flare and signal dropping

Sway braces

89 1819, F41F 700

Patent

active

048298760

ABSTRACT:
A saddle sway brace (90) having a channeled planar plate (94) engageable on a missile launcher platform surface (56). Angled planar plates (100, 102) provide load support for aircraft outrigger equipment. A webbed reenforcing network (110, 112) is engageable with notches (122, 124) in the missile launcher for load support and stability.

REFERENCES:
patent: 4155286 (1979-05-01), Mihm
patent: 4233883 (1980-11-01), Miko
patent: 4412475 (1983-11-01), Hornby
patent: 4660456 (1987-04-01), Griffin et al.

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