Ejection seat with pitch, roll and yaw control

Details Ejection seat with pitch, roll and yaw control Ejection seat with pitch, roll and yaw control

1979-05-24

1980-12-02

Frankfort, Charles E.

Aeronautics and astronautics

Aircraft structure

Fuselage and body construction

244177, B64D 2510

Patent

active

042366879

ABSTRACT:
An aircraft ejection seat having pitch, roll, and yaw control. Two gimbal rocket motors are attached to an aircraft ejection seat. A servo control circuit rotates the rocket motors in response to command signals.

REFERENCES:
patent: 3362662 (1968-01-01), McIntyre et al.
patent: 3421720 (1969-01-01), MacDonald et al.
patent: 3487445 (1969-12-01), Gluhareff et al.
patent: 3592419 (1971-07-01), Hantzsch
patent: 3979089 (1976-09-01), Miller et al.
patent: 4017040 (1977-04-01), Dillinger et al.

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