| CPC B64D 1/02 (2013.01) | 20 Claims |

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1. A system to launch a payload from an aircraft, the system comprising:
a magazine having opposed first and second ends, a payload chamber to retain the payload, and an exit port at the first end through which the payload is launched from the magazine;
a rotatable conveying member to contact an outer surface of the payload and cause the payload to launch out of the magazine through the exit port; and
a pivot structure connected to the magazine and the aircraft, the pivot structure to pivot the magazine about the second end between a stowed orientation and a deployed orientation, the stowed orientation to position the first end internal to an outer skin surface of the aircraft, and the deployed orientation to position the first end outside the outer skin surface and position the second end internal to the outer skin surface.
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