FIELD: naval aviation.
SUBSTANCE: catapult with a controlled overload vector contains the outer ring (1) of the catapult and the inner movable ring (2) of the catapult, made with the possibility of rotation on rollers inside the said outer fixed ring. A stationary outer ring (6) of the launch pad is rigidly mounted on the inner ring (2), inside which it is fastened to the inner movable ring (5) of the launch pad. The catapult drive is made in the form of electric motors (3).
EFFECT: increased stability of the operation of the engines of the aircraft in the process of its preparation for take-off from the launch pad of the catapult.
1 cl, 7 dwg
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| FLYING VEHICLE ALIGHTING GEAR | 1994 |
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