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. 22, 2016

Filed:

Oct. 21, 2013
Applicants:

Roxel France, St Medard en Jalles, FR;

Herakles, Le Haillan, FR;

Inventors:

Andre Pfiffer, Saint-Medard-en-Jalles, FR;

Pascal Caubet, Le Haillan, FR;

Jean-Michel Larrieu, Le Haillan, FR;

Assignees:

ROXEL FRANCE, Saint-Médard-en-Jalles, FR;

HERAKLES, Le Haillan, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F42B 10/66 (2006.01); F42B 15/01 (2006.01); F42B 10/40 (2006.01); F42B 10/00 (2006.01); F42B 15/00 (2006.01);
U.S. Cl.
CPC ...
F42B 15/01 (2013.01); F42B 10/40 (2013.01); F42B 10/663 (2013.01);
Abstract

A combined steering and drag reduction device for a missile is disclosed. The device includes a base and an upper part which are arranged in succession along a main axis of navigation of the missile. Advantageously, the device also includes a pressurized-gas generator and at least one lateral thruster having at least one nozzle configured to deliver a thrust, by expanding gas transmitted by the generator and oriented along an axis substantially perpendicular to the main axis. The at least one lateral thruster also has at least one stabilizing chamber configured to expand the gas transmitted by the generator and expel it through an outlet section of the base substantially perpendicular to the main axis.


Find Patent Forward Citations

Loading…