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:
Jun. 25, 2024

Filed:

Jul. 28, 2019
Applicant:

Rafael Advanced Defense Systems Ltd., Haifa, IL;

Inventors:

Nadav Tal, Haifa, IL;

Yossi Teper, Kiryat Bialik, IL;

Evgeny Guller, Yokneam Ilit, IL;

Jakov Ziv, Acre, IL;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F41F 3/045 (2006.01); F42B 3/00 (2006.01); F42B 15/36 (2006.01); F42B 30/04 (2006.01); F42B 39/20 (2006.01); F42C 15/28 (2006.01); F42C 15/31 (2006.01);
U.S. Cl.
CPC ...
F41F 3/045 (2013.01); F42B 3/006 (2013.01); F42B 15/36 (2013.01); F42B 30/04 (2013.01); F42B 39/20 (2013.01); F42C 15/28 (2013.01); F42C 15/31 (2013.01);
Abstract

Rocket armament launchable from a tubular launcher with an outside launcher non-ignition securing and motor separation during flight and a method to prevent the ignition of the armaments rocket even in the event of actuation of the armaments pyrotechnic assembly, which normally serves to eject the armament from the launcher and to ignite its rocket motor, wherein the armament comprises a gas dispersion assembly, which when the armament is not encased in the tubular launcher, prevents the ignition of the rocket motor even if the armaments pyrotechnic assembly is actuated; and a cutting and separation assembly that is actuated by the pressure of the rocket motor gases for mechanically cutting a structural connection between the rocket motor and the armaments effective payload and separate them during their flight.


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