Missile fin deployment device

Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage

Patent

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Details

188284, 188298, 188314, 188297, F42B 1332

Patent

active

047781270

ABSTRACT:
A missile (10) and concepts for deploying the fins (14) thereof from a stored to a deployed position are disclosed. One device described has three main portions including: A first end portion (32) housing an initiator (22) that powers the device and a locking mechanism (26) that holds the fin at its stored and its locked position; a central portion (34) housing a driven piston (24) that rotates a positively connected fin (14) from the stored to the deployed position; and, a second end portion (36) housing a damping system that controls the rate of deployment of the fins.

REFERENCES:
patent: 3125956 (1964-03-01), Kongelbeck
patent: 3189133 (1965-06-01), Dillenburger
patent: 3563495 (1971-02-01), Korn
patent: 3697019 (1972-10-01), Watson
patent: 3853288 (1974-12-01), Bode
patent: 4143838 (1979-03-01), Holladay
patent: 4175720 (1979-11-01), Craig
patent: 4284177 (1981-08-01), Domek
patent: 4296895 (1981-10-01), Pazmany
patent: 4358983 (1982-11-01), Fallon et al.
patent: 4509427 (1985-04-01), Andreoli
patent: 4510846 (1985-04-01), Gazzera
patent: 4575025 (1986-03-01), Sadvary et al.

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