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:
Nov. 24, 2015

Filed:

May. 16, 2012
Applicants:

Pascal Caubet, St. Medard En Jalles, FR;

Aurore Ferrant, St. Aubin de Medoc, FR;

Inventors:

Pascal Caubet, St. Medard En Jalles, FR;

Aurore Ferrant, St. Aubin de Medoc, FR;

Assignee:

HERAKLES, Le Haillan, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 9/08 (2006.01); B64G 1/26 (2006.01); F42B 10/66 (2006.01); B64G 1/40 (2006.01);
U.S. Cl.
CPC ...
F02K 9/08 (2013.01); B64G 1/26 (2013.01); B64G 1/401 (2013.01); F42B 10/663 (2013.01);
Abstract

A system for in-flight attitude control and side-force steering includes a thruster body and a plurality of valves capable of generating side thrusts put into communication with the thruster body. The valves are arranged in two sets of valves spaced apart from each other towards the front and towards the rear of the thruster body in substantially symmetrical manner relative to the center of gravity of the vehicle situated on a longitudinal axis (A) of the vehicle. Each set comprises a first pair of valves generating thrust in opposite directions along axes that are not in alignment and are parallel to a first axis, and a second pair of valves generating thrust in opposite directions along axes that are not aligned and are parallel to a second axis. The first and second axes are distinct and perpendicular to the longitudinal axis of the vehicle.


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