Patent ID: 7118065
Filing Date: 2006-10-10
Classification: F42B

Abstract:
1. A lateral thrust control for influencing the flight trajectory of a projectile, said control comprising: a main control unit having an internal surface; a central, axially extending main recess in the main control unit; a plurality of thruster recesses in the main control unit for accepting correction thrusters; an ignition element for one of the correction thrusters disposed in each of the thruster recesses, each of the ignition elements being provided with at least one contact element for connecting via a conductor to an electronic control unit; and at least one tubular conductor support of an electrically insulating material arranged inside the main recess of main control unit, the at least one tubular conductor support being non-rotating and immovable relative to the main control unit, wherein at least some of the electrical conductors are in the form of conductive tracks fixedly arranged on the at least one tubular conductor support such that a particular contact element for a particular ignition element contacts the conductive track assigned to the particular contact element, wherein the contact elements of the respective ignition elements disposed inside the thruster recesses project into the main recess.