Technique and apparatus for rearward launch of a missile

Ordnance – Bomb – flare and signal dropping

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Details

89 1816, 89 1818, 102351, 102357, F41F 306, B64D 104

Patent

active

052791998

ABSTRACT:
A technique and apparatus for rearward launch of a missile. The inventive apparatus (10) includes a launch tube (12) in which the missile (14) is mounted with the forward end of the missile being mounted at the forward end (16) of the tube. The rearward end of the launch tube is sealed with a break-away material (18) prior to expulsion of the missile (14). An expulsion mechanism expels the missile in a rearward direction from the launch tube. The expulsion mechanism includes an airbag (20) and a pressurization mechanism (30). The airbag (20) includes a bra (22) for maintaining the orientation of the missile (14) during the expulsion thereof. The airbag (20) also includes a metallized enclosure (24) for sealing the launch tube (14) after the expulsion of the missile (14).

REFERENCES:
patent: 3547000 (1970-12-01), Haberkorn
patent: 3611865 (1971-10-01), Schallert
patent: 3800656 (1974-04-01), Schnabele
patent: 4474101 (1984-10-01), Boulard et al.
patent: 4494437 (1985-01-01), von Maydell
patent: 4520975 (1985-06-01), Blackhurst
patent: 4522104 (1985-06-01), Degen
patent: 4714020 (1987-12-01), Hertsgaard et al.
patent: 4938115 (1990-07-01), von Maydell
patent: 4944210 (1990-07-01), Flock et al.

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