Wedge clamp for missile launcher

Ordnance – Rocket launching – Having guide means

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89 15G, F41F 700

Patent

active

041552865

ABSTRACT:
An adjustable clamp for a missile launcher system having a pair of semi-resilient wedge members which fit between the missile hanger lugs and launcher rail and are drawn into the gap by means of a pair of plate members and a pair of bolts. The Teflon wedges fill the gap between the missile hanger lugs and the launcher rail and reduce vibration during captive flight and protect the rails against damage.

REFERENCES:
patent: 2414579 (1947-01-01), Anderson et al.
patent: 2993254 (1961-07-01), Larson
patent: 3040629 (1962-06-01), Duncan et al.
patent: 3115059 (1963-12-01), Moul
patent: 3228297 (1966-01-01), Kossan et al.
patent: 3267809 (1966-08-01), Sikora
patent: 3967529 (1976-07-01), Ingle et al.

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