High velocity aerodynamic body having telescopic pivotal tip

Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control

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F42B 15053

Patent

active

047564920

ABSTRACT:
A high velocity aerodynamic body, particularly a shell flying at supersonic velocity, having a device for stabilizing the aerodynamic body and for reducing its oscillation. The aerodynamic body has in the vicinity of its tip, a rotation symmetrical tip enclosure which is supported, with balanced mass, about a support point located on the longitudinal axis of the aerodynamic body, freely tiltably on all sides.

REFERENCES:
patent: 3067682 (1962-12-01), Feldmann et al.
patent: 3195462 (1965-07-01), Petre
patent: 3262655 (1966-07-01), Gillespie, Jr.
patent: 4351503 (1982-09-01), Drori
patent: 4399962 (1983-08-01), Wedertz et al.
patent: 4579298 (1986-04-01), Thomson

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