Device for a missile or the like

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

Patent

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Details

60253, 102 493, F42B 1500

Patent

active

041272439

ABSTRACT:
In a missile assembly (or the like) including a motor nozzle positioned in a central portion of a rear surface of the missile and a sustainer motor positioned a distance away from the rear surface of the missile, the invention comprising a blow pipe joining the sustainer motor and nozzle assembly, with the blow pipe including a portion extending along an axis which is eccentrically positioned with respect to the longitudinal axis of the missile.

REFERENCES:
patent: 1879579 (1932-09-01), Stolfa et al.
patent: 2489953 (1949-11-01), Burney
patent: 2816721 (1957-12-01), Taylor
patent: 3013494 (1961-12-01), Chanut

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