Ejection seat stabilization apparatus

Aeronautics and astronautics – Aircraft structure – Fuselage and body construction

Patent

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Details

244 87, 244 91, B64D 2510

Patent

active

044808062

ABSTRACT:
An ejection seat is provided with fins on opposite sides which are normally stored along the seat side rails and are deployed immediately after ejection to yaw-stabilize the seat as it is slowed by a drogue. The fins are mounted for rotation and are deployed such that they extend rearwardly and out to the sides.

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