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:
Feb. 18, 2025

Filed:

Apr. 25, 2022
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

John K. Foster, St. Peters, MO (US);

Ryan Binkholder, Webster Groves, MO (US);

Thaddeus Jakubowski, Jr., St. Charles, MO (US);

Assignee:

The Boeing Company, Arlington, VA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F42B 10/46 (2006.01); B64C 30/00 (2006.01); B64D 1/06 (2006.01); F42B 10/64 (2006.01);
U.S. Cl.
CPC ...
F42B 10/46 (2013.01); B64C 30/00 (2013.01); B64D 1/06 (2013.01); F42B 10/64 (2013.01);
Abstract

A propulsionless munition configured to be launched from a hypersonic aerial includes a munition body that is free of any propulsion system for producing thrust. The munition body includes a forward section including a radome assembly and an aft section including a control system. The radome assembly includes a nose radome and a frangible radome cover disposed over the nose radome for shielding the nose radome from high temperatures resulting from aerodynamic heating at hypersonic speeds. The frangible radome cover is detachable from the nose radome upon detection by the control system of a predetermined threshold comprising at least one of a predetermined speed, a predetermined altitude, and a predetermined temperature.


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