Missile/canister lateral support pad flyout control system

Details Missile/canister lateral support pad flyout control system Missile/canister lateral support pad flyout control system

1981-11-05

1984-02-14

Walsh, Donald P.

Ammunition and explosives

Projectiles

Composite

89 1819, F42B 1316

Patent

active

044309422

ABSTRACT:
An improved missile/canister support pad control system wherein rods having a flexible curved section are interconnected to the support pads and are detachably held parallel to the missile by releasing means. Upon command, after the missile leaves the canister, the releasing means allows the rods to spring away from the missile. The resultant wind in combination with the spring rods lifts and rotates the system away from the missile so as not to recontact the missile surface.

REFERENCES:
patent: 36773 (1862-10-01), Emery
patent: 2415814 (1947-02-01), Davis et al.
patent: 2998780 (1961-09-01), Anspacher et al.
patent: 3038382 (1962-06-01), Noyes et al.
patent: 3044400 (1962-07-01), Detwiler
patent: 3089417 (1963-05-01), Beyer et al.
patent: 3251301 (1966-05-01), Herrmann
patent: 4145017 (1979-03-01), Stiklorus

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