Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1984-03-19
1986-02-04
Kyle, Deborah L.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
244 324, 403258, 403361, F42B 1330, F42B 1502, F16B 1310, B25G 328
Patent
active
045680418
ABSTRACT:
An improved fin attachment having a socket for reception of a tang mounted n a missile fin, an element for drawing the tang into the socket, and frusto-conical concentric rings which engage the tang and the socket to connect them rigidly in a predetermined angular relation. All elements of the attachment are retained so as not to be lost when the fin is detached, and the attachment provides effective connection without the use of complex shapes or precise manufacturing tolerances.
REFERENCES:
patent: 2718155 (1955-09-01), Firth
patent: 2811881 (1957-11-01), Rieser
patent: 2956826 (1960-10-01), Nord
patent: 2974965 (1961-03-01), Welles, Jr.
patent: 3011794 (1961-12-01), Vaugn
patent: 3101962 (1963-08-01), Nunlist
patent: 3613221 (1971-10-01), Pronk
patent: 4136533 (1979-01-01), Okuda
patent: 4172574 (1979-10-01), Spillman
Beers Robert F.
Carone Michael
Church Stephen J.
Kyle Deborah L.
Skeer W. Thom
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