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An electric propulsion device for a satellite equipped with at least four active thrusters exerting a parallel thrust upon a transfer, the device comprises means for detecting a thruster failure and means for reorienting the thrusters, and comprises means for computing a reorientation angle of the t

An electric propulsion device for a satellite equipped with at least four active thrusters exerting a parallel thrust upon a transfer, the device comprises means for detecting a thruster failure and means for reorienting the thrusters, and comprises means for computing a reorientation angle of the thrusters remaining active upon a failure of a thruster, the value of the angle being computed to reorient at least two of the remaining thrusters in order to cancel the total torque about the center of mass of the satellite.

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1. A propulsion device for a satellite equipped with at least four active thrusters used in parallel, exerting a parallel thrust upon a transfer, the device comprising means for detecting a thruster failure and means for reorienting the thrusters, the device further comprising means for computing a

1. A propulsion device for a satellite equipped with at least four active thrusters used in parallel, exerting a parallel thrust upon a transfer, the device comprising means for detecting a thruster failure and means for reorienting the thrusters, the device further comprising means for computing a reorientation angle of the thrusters remaining active upon a failure of a thruster, said reorientation angle being computed to reorient at least two of the remaining active thrusters according to a same computed reorientation angle in order to cancel the total torque about the center of mass of the satellite, wherein two active thrusters are reoriented according to the computed reorientation angle. 2. The device as claimed in claim 1, wherein the thrusters are associated with mechanisms formed toward an anti-earth face of the satellite. 3. The device as claimed in claim 1, wherein all the active thrusters are reoriented according to the same computed reorientation angle. 4. The device as claimed in claim 1, wherein the thrusters are electric thrusters. 5. The device as claimed in claim 4, wherein the thrusters are Hall-effect thrusters. 6. The device as claimed in claim 4, wherein the thrusters are gated ion motors. 7. A satellite comprising a propulsion device for said satellite equipped with at least four active thrusters used in parallel, exerting a parallel thrust upon a transfer, the device comprising means for detecting a thruster failure and means for reorienting the thrusters, the device further comprising means for computing a reorientation angle of the thrusters remaining active upon a failure of a thruster, said reorientation angle being computed to reorient at least two of the remaining active thrusters according to a same computed reorientation angle in order to cancel the total torque about the center of mass of the satellite, wherein two active thrusters are reoriented according to the computed reorientation angle. 8. A method for reorienting the thrusters of an electric propulsion device for a satellite equipped with at least four active thrusters exerting a parallel thrust upon a transfer, the method comprising the steps of: detecting a failure of one of the thrusters,computing a reorientation angle of the thrusters remaining active, a value of said reorientation angle being computed in order to cancel the total torque about the center of mass of the satellite; andreorienting, by the value of said reorientation angle, at least two of the thrusters remaining active,wherein two active thrusters are reoriented according to the computed reorientation angle.