F42B30/08

FUZE ARMING TECHNIQUES FOR A SUBMUNITION

According to an aspect of the invention, there is provided a fuze arming system for a submunition, comprising: a first stage, arranged to detect launch of the submunition and its associated carrier; a second stage, arranged to detect expulsion of the submunition from the carrier, and to at least partially arm a submunition fuze based on such detection; wherein the second stage is unable to at least partially arm the submunition fuze without the first stage detecting launch of the submunition and its associated carrier.

TRACKABLE AMMUNITION
20220011080 · 2022-01-13 ·

Disclosed are ammunition and ammunition tracking systems. The ammunition and ammunition tracking system may include a first projectile and a marker. The marker may be associated with the first projectile. The marker may contain a unique signature such that the first projectile may be identifiable from a second projectile.

Very low-power actuation devices

A munition including: a casing having a first portion and the second portion; and an actuator comprising two or more pistons, each of the pistons being connected at a first end to the first portion of the casing and engaged at a second end to the second portion of the casing, each of the pistons being capable of having an extended and retracted position relative to the first and second ends, the retracted position resulting from an activation of each of the two or more pistons; wherein activation of one or more of the two or more pistons moves the first portion relative to the second portion.

Very low-power actuation devices

A munition including: a casing having a first portion and the second portion; and an actuator comprising two or more pistons, each of the pistons being connected at a first end to the first portion of the casing and engaged at a second end to the second portion of the casing, each of the pistons being capable of having an extended and retracted position relative to the first and second ends, the retracted position resulting from an activation of each of the two or more pistons; wherein activation of one or more of the two or more pistons moves the first portion relative to the second portion.

Techniques suitable for use with an object for moving through a fluid, such as a munition or reconnaissance projectile

According to a first aspect of the invention, there is provided an object for moving through a fluid, the object comprising: an outer housing, arranged to be exposed to a hydrostatic pressure exerted by the fluid; a strain gauge, arranged to obtain an indication of the hydrostatic pressure, wherein a first part of the strain gauge is arranged to be in contact with the outer housing, such that the strain gauge is arranged to obtain an indication of the hydrostatic pressure by obtaining an indication of the strain on the housing.

Techniques suitable for use with an object for moving through a fluid, such as a munition or reconnaissance projectile

According to a first aspect of the invention, there is provided an object for moving through a fluid, the object comprising: an outer housing, arranged to be exposed to a hydrostatic pressure exerted by the fluid; a strain gauge, arranged to obtain an indication of the hydrostatic pressure, wherein a first part of the strain gauge is arranged to be in contact with the outer housing, such that the strain gauge is arranged to obtain an indication of the hydrostatic pressure by obtaining an indication of the strain on the housing.

Seal for a projectile guiding kit

A device for improving the aerodynamic feature of a projectile is disclosed. The projectile has a front part and a rear part. The external diameter of the front part of the projectile is larger than the external diameter of the front end of a rear part of the projectile. The front end of the rear part of the projectile is conical having larger diameter at locations behind the front end. The device comprises an annular cut-off cone sleeve slidably disposable over the front part of the projectile. The diameter of the narrower end of the annular cone sleeve is slightly larger than the diameter of the front part of the projectile and the length of the annular cut-off cone sleeve is larger than the distance between the front end of the rear part of the projectile and a location on rear part having a diameter equal to the diameter of the rear end of the annular cut-off cone sleeve.

Sheet-metal ammunition packing tray

An ammunition tray is provided for containing a plurality of bullet cartridges within an ammunition box container having a stowage volume. The tray includes a substantially rectangular template having a horizontal surface bounded by first and second opposing longitudinal edges and opposing lateral edges joined at four corners. Each longitudinal edge includes a first tab bent substantially perpendicular to the surface in a vertical direction to form a rib. Each lateral edge includes a second tab bent substantially perpendicular to the surface to form a wall. The surface includes a first row of interior pockets that point towards the first longitudinal edge as a proximal orientation. The surface further includes a second row of interior pockets that point towards the second longitudinal edge as a distal orientation. The template has longitudinal and lateral edges bent to form the respective ribs and walls fits within the stowage volume as a vertical stack of plural templates. Each first interior pocket in the first row can cradle a cartridge on the surface along the proximal orientation, can fit the cartridge from an adjacent second row, and has lateral edges bent to curl in said vertical direction. Each second interior pocket in the second row can cradle the cartridge on the surface along the distal orientation, can fit the cartridge from an adjacent first row, and has lateral edges bent to curl opposite said vertical direction.

Sheet-metal ammunition packing tray

An ammunition tray is provided for containing a plurality of bullet cartridges within an ammunition box container having a stowage volume. The tray includes a substantially rectangular template having a horizontal surface bounded by first and second opposing longitudinal edges and opposing lateral edges joined at four corners. Each longitudinal edge includes a first tab bent substantially perpendicular to the surface in a vertical direction to form a rib. Each lateral edge includes a second tab bent substantially perpendicular to the surface to form a wall. The surface includes a first row of interior pockets that point towards the first longitudinal edge as a proximal orientation. The surface further includes a second row of interior pockets that point towards the second longitudinal edge as a distal orientation. The template has longitudinal and lateral edges bent to form the respective ribs and walls fits within the stowage volume as a vertical stack of plural templates. Each first interior pocket in the first row can cradle a cartridge on the surface along the proximal orientation, can fit the cartridge from an adjacent second row, and has lateral edges bent to curl in said vertical direction. Each second interior pocket in the second row can cradle the cartridge on the surface along the distal orientation, can fit the cartridge from an adjacent first row, and has lateral edges bent to curl opposite said vertical direction.

SEAL FOR A PROJECTILE GUIDING KIT

A device for improving the aerodynamic feature of a projectile is disclosed. The projectile has a front part and a rear part. The external diameter of the front part of the projectile is larger than the external diameter of the front end of a rear part of the projectile. The front end of the rear part of the projectile is conical having larger diameter at locations behind the front end. The device comprises an annular cut-off cone sleeve slidably disposable over the front part of the projectile. The diameter of the narrower end of the annular cone sleeve is slightly larger than the diameter of the front part of the projectile and the length of the annular cut-off cone sleeve is larger than the distance between the front end of the rear part of the projectile and a location on rear part having a diameter equal to the diameter of the rear end of the annular cut-off cone sleeve.