Abstract: A missile launcher and missile snubbing apparatus (32) includes a pair snubber blocks (34, 36) slideable along angled side edges of a wedge (38). The snubber blocks (34, 36) are biased by respective springs (48, 50) in a first direction, while the wedge (38) is biased in an opposite direction by a spring (84). A spring biased cam (86) is operative to move the wedge (38) in a direction to reduce the effective width of the snubber block assembly (32) so that a missle can be downloaded from the rear of the launcher (10). A spring clip (85) is engageable with a rod (43) attached to the block (38), and responsive to the action of the cam (86) for locking the wedge (38) in a first position. The spring clip (85) is shaped so as to be responsive to the downloading of the missile (12) for releasing the locked wedge (38).

Abstract: A missile launcher is disclosed having an elongate planar platform (28) formed integral with the body of the launcher (26). Plural bomb rack fasteners (34, 36) and pylon mounting lugs (38, 40) are fixed to the platform surface (28) to accommodate different aircraft types. Plural sway braces (46) are removably fixed to the side edges of the platform surface (28). Each sway brace (46) can be fixed to desired positions along the side edges of the platform surface (28) to also accommodate different aircraft type mounting apparatus.

Abstract: A charging device for electric bomb fuzes which may be oriented in more t one direction relative to the direction of movement of the bomb and still be fully operable. The device precludes the occurrence of accidental duds based on mis-orientation of the charging device with respect to the direction of travel of the bomb. The multi-directional charging device includes a unique dual inlet port and outlet port structure by means of which slipstream air may travel in either of two directions through the charging device to successfully actuate the electrical energy transducer positioned therein.

Abstract: Disclosed herein is an environmental charging system for providing energy electrically fused bombs without the need for external charging equipment. The system comprises an electrically fused bomb having conventional existing charging well which charging well is usually centrally located along the longitudinal portion of the bomb. An energizing means, which is adapted to be actuated by slip stream air, is fixed within a charging device which is located within the charging well. The energizing means is designed to pop up out of the charging device as the bomb is released from the aircraft such that in its pop-up position it receives slip-stream air which in turn actuates the device. Means are provided for making electrical contact between the energizing means and the bomb only when the energizing means is in its pop-up position.