IP Library › Granted Patent US 12,467,703
Granted Patent B2
US 12,467,703 · App. 18/684,949 · Granted Nov 11, 2025

Cartridges for recoil management of shoulder fired weapons

Inventors: Roger C. Esplin (Marana, AZ); Daniel Kenneth Johnson (Golden, CO); Morgan J. Bakarich (Tucson, AZ); Saeed Adil Merza (Palmetto, FL); Gary Leonard Abrams (Oro Valley, AZ); Cody Alan Jensen (Tucson, AZ)
Assignee: Raytheon Company
F41A1/08F42B5/16F42C19/0807F42C19/0826
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Quick Facts
Patent No.
US 12,467,703
App. No.
18/684,949
Granted
Nov 11, 2025
Kind
B2
Abstract

A cartridge ( 20 ) has a cartridge case ( 22 ) extending along an axis ( 500 ) from a base ( 104 ) to a mouth ( 102 ) and having an interior. A projectile ( 24 ) is mounted in the case. A propellant ( 26 ) is contained within the case. The propellant has an annular grain encircling the axis.

Claims (75)

1 . A cartridge ( 20 ) comprising:

a cartridge case ( 22 ) extending from a base ( 104 ) to a mouth ( 102 ) and having an interior;

a projectile ( 24 ) mounted in the case and having a rocket motor ( 48 );

a primer ( 28 ) mounted in the base, the primer comprising:

a main primer charge ( 194 ); and

a percussion primer ( 192 ) having a percussion primer charge ( 196 ); and

a propellant grain ( 26 ) within the case interior,

wherein:

a nozzle ( 153 ) is encircled by the propellant grain and comprises a plurality of radially-open outlet ports ( 170 ); and

the propellant grain comprises an annular body encircling a centerline ( 500 ) of the cartridge.

2 . The cartridge of claim 1 wherein the propellant grain is a single continuous full annulus piece.

3 . The cartridge of claim 1 wherein the propellant grain comprises:

a non-convoluted inner diameter surface ( 224 ).

4 . The cartridge of claim 1 wherein the propellant grain comprises:

a right circular cylindrical inner diameter surface ( 224 ).

5 . The cartridge of claim 1 wherein the propellant grain comprises:

a plurality of axial passageways ( 700 ).

6 . The cartridge of claim 1 wherein:

the propellant grain is adhered ( 236 ) to an inner diameter (ID) surface of the case.

7 . The cartridge of claim 1 wherein:

the propellant grain is an ammonium perchlorate composite propellant (APCP).

8 . The cartridge of claim 1 wherein:

the propellant grain is in a propellant unit having a fibrous or plastic casing ( 230 ).

9 . The cartridge of claim 1 wherein:

the primer further comprises a primer case ( 190 ) containing the main primer charge and having a primer pocket ( 180 ); and

the percussion primer ( 192 ) has a cup mounted in the primer pocket and containing the percussion primer charge ( 196 ).

10 . The cartridge of claim 9 wherein:

the main primer charge ( 194 ) comprises BKNO 3 .

11 . The cartridge of claim 1 wherein:

the projectile is a missile having:

a seeker ( 50 ); and

the rocket motor ( 48 ); and/or

the cartridge contains an ignition train ( 34 ) for transferring ignition of the propellant grain to the rocket motor; and/or

the case comprises:

a base piece ( 130 ); and

a sidewall piece ( 132 ) secured to the base piece.

12 . A loaded firearm ( 400 ) including the cartridge of claim 1 and further comprising a barrel ( 402 ) having:

a muzzle ( 408 ); and

a chamber ( 404 ) accommodating the cartridge.

13 . The loaded firearm of claim 12 wherein:

the case extends through the muzzle.

14 . The loaded firearm of claim 12 wherein:

the barrel is a rifled ( 410 ) barrel.

15 . A method for manufacturing the cartridge of claim 1 , the method comprising:

casting the propellant grain;

inserting the cast propellant grain into the case; and

inserting the projectile into the case.

16 . The method of claim 15 further comprising:

adhering the propellant grain to an inner diameter (ID) surface of the case.

17 . A method for using the loaded firearm of claim 12 , the method comprising:

igniting the primer;

combustion gas from the primer passing radially outward to ignite the propellant; and

combustion gas from the propellant driving the projectile from the case.

18 . The method of claim 17 wherein:

the projectile is a missile; and

the combustion gas of the propellant indirectly ignites the rocket motor.

19 . A loaded firearm ( 400 ) comprising:

a barrel ( 402 ) having:

a muzzle ( 408 ); and

a chamber ( 404 ); and

a cartridge ( 20 ) accommodated by the chamber and comprising:

a cartridge case ( 22 ) extending from a base ( 104 ) to a mouth ( 102 ) and having an interior;

a projectile ( 24 ) mounted in the case;

a primer ( 28 ) mounted in the base, the primer comprising:

a main primer charge ( 194 ); and

a percussion primer ( 192 ) having a percussion primer charge ( 196 ); and

a propellant grain ( 26 ) within the case interior,

wherein:

the cartridge has a nozzle ( 153 ) encircled by the propellant grain and comprises a plurality of radially-open outlet ports ( 170 );

the propellant grain comprises an annular body encircling a centerline ( 500 ) of the cartridge; and

the case extends through the muzzle.

20 . The loaded firearm of claim 19 wherein:

the barrel is a rifled ( 410 ) barrel.

21 . The loaded firearm of claim 19 wherein:

the projectile protrudes from the case mouth.

Continuity (2)
Provisional Application 63234465 · Aug 18, 2021
Related Publication 20240369332A1 · Nov 7, 2024
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