Internal stabilizing device for air and water missiles

Ammunition and explosives – Igniting devices and systems

Patent

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244 31, F42B 2500

Patent

active

039371441

ABSTRACT:
An apparatus and method for reducing the launch disturbance of a weapon se on a supersonic aircraft is disclosed. The apparatus comprises a flywheel rotatably mounted within the store. The flywheel is pre-spun before launch using internal rockets or ram air. The spining flywheel produces a gyroscopic effect which appreciably reduces launch disturbance and therefore increases accuracy.

REFERENCES:
patent: 1316033 (1919-09-01), Hayden
patent: 1316363 (1919-09-01), Hayden
patent: 2402718 (1946-06-01), Albree
patent: 2406293 (1946-08-01), Hammond, Jr.
patent: 2691495 (1954-10-01), Chiroky
patent: 2729106 (1956-01-01), Mathiesen
patent: 2849955 (1958-09-01), Smathers
patent: 2960876 (1960-11-01), Saphra
patent: 3610096 (1971-10-01), Bauman et al.

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