Integrated aerodynamic fin and stowable TVC vane system

Details Integrated aerodynamic fin and stowable TVC vane system Integrated aerodynamic fin and stowable TVC vane system

1991-03-15

1994-06-14

Jordan, Charles T.

Aeronautics and astronautics

Missile stabilization or trajectory control

Automatic guidance

23926519, 244 321, F42B 1066

Patent

active

053203046

ABSTRACT:
An aerodynamic fin and stowable jet vane system preferably for rocket motor issile applications to control roll, pitch, and yaw, in either the aerodynamic or thrust flight control conditions, has a retractable and stowable aerodynamic vane integrated with a stowable thrust vector reaction steering system on a common support. The integrated aerodynamic fins and thrust vector control reduce the overall missile mainframe dimensions and are mounted on a single, space saving support.

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patent: 4913379 (1990-04-01), Kubota et al.

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