Nov 3, 2026

US12782097 - Optical command airburst ammunition fuze system

A method of airburst fuze configuration by which airburst capability may be retrofitted to existing weapons systems or munitions or configured for new ones. The system consists of a nose or mid-body fuze package for a host projectile, incorporating a rear-looking optical sensor system, which will periscope outwards to establish a rearwards line of sight. The fuze package is to be used with a separate and retained detonation control system which performs fire control calculations and transmits an optical signal at the time airbursting is desired, which subsequently prompts the rear-looking optical sensor to trigger the payload of the host projectile.

ammunitionfuzeexplosive

The patent describes an airburst fuze system that can be retrofitted to existing munitions or designed for new ones, utilizing a rear-looking optical sensor to receive command signals for detonation. This system includes a signal discrimination component to verify the command code and an output element to activate the projectile’s explosive payload based on the received signal.

Claim 1

1 . A projectile launchable from a host weapon, comprising: a payload including an explosive charge; and a fuze package comprising: a rear-looking optical sensor configured to receive an optical command signal transmitted from a remote optical emitter, wherein the rear-looking optical sensor is positioned forward of at least a portion of the payload along a longitudinal axis of the projectile and has a rearward line of sight during flight of the projectile; a signal discrimination component configured to determine whether the received optical command signal matches a predetermined command code; and an output element configured to activate the payload in response to a determination that the received optical command signal matches the predetermined command code. a payload including an explosive charge; and a fuze package comprising: a rear-looking optical sensor configured to receive an optical command signal transmitted from a remote optical emitter, wherein the rear-looking optical sensor is positioned forward of at least a portion of the payload along a longitudinal axis of the projectile and has a rearward line of sight during flight of the projectile; a signal discrimination component configured to determine whether the received optical command signal matches a predetermined command code; and an output element configured to activate the payload in response to a determination that the received optical command signal matches the predetermined command code. a rear-looking optical sensor configured to receive an optical command signal transmitted from a remote optical emitter, wherein the rear-looking optical sensor is positioned forward of at least a portion of the payload along a longitudinal axis of the projectile and has a rearward line of sight during flight of the projectile; a signal discrimination component configured to determine whether the received optical command signal matches a predetermined command code; and an output element configured to activate the payload in response to a determination that the received optical command signal matches the predetermined command code.

Google Patents

https://patents.google.com/patent/US12782097

USPTO PDF

https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/12782097

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