Main propellant ignition liner for cased telescoped ammunition

• US 5,048,422 A
• Filed: 09/10/1990
• Issued: 09/17/1991
• Est. Priority Date: 09/10/1990
• Status: Expired due to Term

• Current Assignee: Alliant Techsystems Incorporated (Northrop Grumman Corporation)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Tasson, Brian B., Northrup, James R.
• Primary Examiner(s): TUDOR, HAROLD JAY
• Application Number:
  US07/580,391
• Time in Patent Office: 372 Days
• Field of Search: 102/430, 102/431, 102/433, 102/434, 102/443
• US Class Current: 102/434
• CPC Class Codes: F42B 5/045 of telescopic type F42B5/184 takes precedence

Abstract

A cased telescoped ammunition in which a rigid liner fills the gap between the control tube and the metering tube. The liner comprises an energetic material which transfers the ignition stimulus from the control tube propellant to the main propellant. Energetic materials in the liner can be modified to increase the ignition stimulus for proper cold round performance or decrease ignition stimulus for an improved timed sequencing of the round'"'"'s performance. Both double-based and single-based energetic materials may be used.

Claims

1. A cased telescoped ammunition comprising in combination;

a control tube housing a first propellant and a projectile;

a metering tube forming in combination with said control tube an axial passageway;

an outer casing surrounding said control tube and said metering tube and radially spaced therefrom;

said control tube and said metering tube spaced from one another to form a gap along said axial passageway between said tubes;

a second propellant in the space between said tubes and said outer case;

a liner disposed in said gap in contact with said control tube and said metering tube and separating said second propellant from said passageway; and

said control tube and said metering tube arranged such that ignition of said first propellant forces said projectile along said axial passageway and ignition products of said first propellant ignite said second propellant through said liner as said projectile passes said liner.

2. A cased telescoped ammunition as in claim 1 wherein said liner is comprised of an energetic material.

3. A cased telescoped ammunition as in claim 1 wherein said second propellant is a granular propellant.

4. A cased telescoped ammunition as in claim 2 wherein said second propellant is a granular propellant.

5. A cased telescoped ammunition as in claim 2 wherein said energetic material is a single-based material.

6. A cased telescoped ammunition as in claim 2 wherein said energetic material is a double-based material.

7. A cased telescoped ammunition as in claim 2 wherein said energetic material is formulated to provide a predetermined main propellant ignition characteristic.

8. A cased telescoped ammunition as in claim 4 wherein said energetic material is formulated to provide a predetermined main propellant ignition characteristic.

9. A cased telescoped ammunition as in claim 2 wherein said energetic material includes a nitrated ester.

10. A cased telescoped ammunition as in claim 2 wherein said energetic material includes nitrocellulose.

11. A cased telescoped ammunition as in claim 1 wherein said liner is comprised of the material that retards ignition of said second propellant by said first propellant.

12. A cased telescoped ammunition as in claim 2 wherein said liner is comprised of the material that retards ignition of said second propellant by said first propellant.