Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Reexamination Certificate
2006-10-10
2006-10-10
Barefoot, Galen (Department: 3644)
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
C244S052000, C102S347000
Reexamination Certificate
active
07118065
ABSTRACT:
A lateral thrust control is provided for influencing the flight trajectory of a projectile. The control has a main control unit; 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; and at least one tubular conductor support of an electrically insulating material arranged inside the main recess of main control unit. 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.
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Heitmann Thomas
Schwenzer Michael
Barefoot Galen
Rheinmetall Waffe Munition GmbH
Smith Stuart I.
Venable LLP
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