The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Dec. 24, 2019

Filed:

Aug. 04, 2015
Applicant:

Airbus Defence and Space Sas, Les Mureaux, FR;

Inventors:

Dominique Poncet, Toulouse, FR;

Cyril Tourneur, Toulouse, FR;

René Cheynet De Beaupre, Toulouse, FR;

Assignee:

AIRBUS DEFENCE AND SPACE SAS, Les Mureaux, FR;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/00 (2006.01); B64G 1/40 (2006.01); B64G 1/10 (2006.01); B64G 1/64 (2006.01);
U.S. Cl.
CPC ...
B64G 1/007 (2013.01); B64G 1/1085 (2013.01); B64G 1/402 (2013.01); B64G 1/646 (2013.01); B64G 1/405 (2013.01);
Abstract

A system and method for transferring a satellite from an initial orbit into a mission orbit. The method includes anchoring to the satellite of an external unit having a tank containing a reserve of propellants. The system includes an autonomous spacecraft having an electric propulsion module and a small internal reserve of propellants, located in a parking orbit close to the initial orbit. The spacecraft with the external unit attached to the satellite is docketed in an initial orbit, to produce a fluidic connection of the propellant tank of the external unit to the propulsion module of the spacecraft. The external unit and satellite is transferred into the mission orbit by the electric propulsion module of the spacecraft supplied with propellants directly from the external unit, thereby releasing the satellite into the mission orbit.


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