Patent ID: 9163901
Filing Date: 2015-10-20
Classification: B64G,F41F,F42B

Abstract:
1. A guidance section connector interface system operable with a rocket launcher for facilitating electrical communication between a rocket and the rocket launcher, the guidance section connector interface system comprising: a rocket connector in electrical communication with a guidance system of a rocket; a connector saver coupled to the rocket connector to provide a first connection; and a launcher connector supported about a rocket launcher, and in electrical communication with a control system, wherein the connector saver is coupled to the launcher connector upon insertion of the rocket into the rocket launcher to provide a second connection, wherein the rocket connector, the connector saver and the launcher connector connect together to facilitate electrical communication between the rocket and the rocket launcher, wherein, upon launch of the rocket from the rocket launcher, the first connection releases, and the second connection remains connected, causing the connector saver to remain connected to the launcher connector.