Guidance apparatus for projectiles

Details Guidance apparatus for projectiles Guidance apparatus for projectiles

1987-07-28

1988-08-16

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F42B 15033

Patent

active

047638575

ABSTRACT:
The trajectory of a projectile is variable by means of a thrust generated by gas issuing from a nozzle, the nozzle normally rotating at high speed about the axis of the projectile but assuming a desired angular orientation for a predetermined period of time in order to impart a lateral thrust to the projectile thereby changing its trajectory.

REFERENCES:
patent: 4463921 (1984-08-01), Metz
patent: 4482107 (1984-11-01), Metz
patent: 4589594 (1986-05-01), Kranz
patent: 4646991 (1987-03-01), Kranz
patent: 4681283 (1987-07-01), Kranz
patent: 4691876 (1987-09-01), Kranz

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