Control propulsion unit, especially for exerting transverse forc

Details Control propulsion unit, especially for exerting transverse forc Control propulsion unit, especially for exerting transverse forc

1989-10-31

1990-12-25

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

F41G 700

Patent

active

049796976

ABSTRACT:
A control propulsion unit with a solid propellant (4) and a discharge nozzle, through which the propellant gases emerge into the open air, especially to exert transverse forces on a missile. To be able to precisely, quantitatively regulate the transverse forces, in accordance with the invention, it is proposed to extinguish the propellant in a controlled operation by reducing the clamping of the control propulsion unit, for example, by enlarging the discharge port for the propellant gases.

REFERENCES:
patent: 3447465 (1967-06-01), White
patent: 4573648 (1986-03-01), Morenus et al.
patent: 4765565 (1988-08-01), Buchele-Buecher et al.
patent: 4826104 (1989-05-01), Bennett et al.

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