| 摘要 |
Disclosed is a missile launcher (142) which includes frontal electrical access to electrical apparatus mounted in the aft portion of the luncher. A connectorized extender electrical cable (66) is connected to the aft-mounted electrical apparatus (50). The other end of the cable (66) is routed internal to the launcher (142) and exits a frontal sway brace (24). A hole (108) is bored at a 30-inch launcher mounting location (28), and a connector (90) of the extender cable (66) is mounted therein. Aircraft pylons utilizing 14-inch mounting centers and frontal electrical umbilical connections can thereby utilize existing launchers modified according to the invention.
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