Patents by Inventor Alexandre KALTENBACH

Alexandre KALTENBACH has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 10005567
    Abstract: A method for stationing a satellite comprises a transfer phase, during which the satellite moves on an elliptical geosynchronous orbit, the orbit being deformed progressively by application of a thrust by electrical or hybrid electrical-chemical propulsion to bring it closer to a geostationary orbit. The transfer step comprises a substep during which, during a plurality of revolutions of the satellite, the thrust is stopped for a fraction of orbital period and tests of a telecommunications payload of the satellite are performed in the absence of thrust.
    Type: Grant
    Filed: July 24, 2015
    Date of Patent: June 26, 2018
    Assignee: THALES
    Inventors: Raphaël Hache, Alexandre Kaltenbach, Stéphane Tessandori
  • Patent number: 9650159
    Abstract: 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.
    Type: Grant
    Filed: August 29, 2014
    Date of Patent: May 16, 2017
    Assignee: THALES
    Inventor: Alexandre Kaltenbach
  • Publication number: 20160207640
    Abstract: 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.
    Type: Application
    Filed: August 29, 2014
    Publication date: July 21, 2016
    Inventor: Alexandre KALTENBACH
  • Publication number: 20160023780
    Abstract: A method for stationing a satellite comprises a transfer phase, during which the satellite moves on an elliptical geosynchronous orbit, the orbit being deformed progressively by application of a thrust by electrical or hybrid electrical-chemical propulsion to bring it closer to a geostationary orbit. The transfer step comprises a substep during which, during a plurality of revolutions of the satellite, the thrust is stopped for a fraction of orbital period and tests of a telecommunications payload of the satellite are performed in the absence of thrust.
    Type: Application
    Filed: July 24, 2015
    Publication date: January 28, 2016
    Inventors: Raphaël HACHE, Alexandre KALTENBACH, Stéphane TESSANDORI