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US20030183111A1 - Mechanically fuzed high explosive projectile using pryotechnic initiation delay - Google Patents

Mechanically fuzed high explosive projectile using pryotechnic initiation delay Download PDF

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Publication number
US20030183111A1
US20030183111A1 US10/115,469 US11546902A US2003183111A1 US 20030183111 A1 US20030183111 A1 US 20030183111A1 US 11546902 A US11546902 A US 11546902A US 2003183111 A1 US2003183111 A1 US 2003183111A1
Authority
US
United States
Prior art keywords
projectile
high explosive
fuzed
pryotechnic
mechanically
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US10/115,469
Inventor
Brian Tasson
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Northrop Grumman Innovation Systems LLC
Original Assignee
Alliant Techsystems Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Alliant Techsystems Inc filed Critical Alliant Techsystems Inc
Priority to US10/115,469 priority Critical patent/US20030183111A1/en
Assigned to ALLIANT TECHSYSTEMS INC. reassignment ALLIANT TECHSYSTEMS INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: TASSON, BRIAN B.
Priority to NO20031241A priority patent/NO20031241L/en
Priority to EP03007336A priority patent/EP1351032A2/en
Publication of US20030183111A1 publication Critical patent/US20030183111A1/en
Abandoned legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B3/00Blasting cartridges, i.e. case and explosive
    • F42B3/10Initiators therefor
    • F42B3/16Pyrotechnic delay initiators

Definitions

  • the present invention relates to a projectile which incorporates an ignition delay element between the fuze and the high explosive.
  • High explosive rounds of ammunition with mechanical fuzes typically use super quick initiation. This often prevents the projectile from entering soft or semi-armored targets prior to the initiation event, which results in little or no damage to the target. Therefore, adding a delay to allow penetration of the soft or semi-armored target is desirable.
  • FIG. 1 is a side view of the inventive projectile.
  • FIG. 1 shows a side view of a standard projectile 10 , which includes a fuze 12 at the front end of the projectile and a charge of high explosive at 14 .
  • a pyrotechnic delay element 16 is placed between the fuze 12 and the high explosive 14 .
  • the pyrotechnic delay element is comprised of a modified IM-68 incendiary mix, which is comprised of:

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
  • Developing Agents For Electrophotography (AREA)
  • Manufacture Of Metal Powder And Suspensions Thereof (AREA)

Abstract

A projectile which includes a pyrotechnic delay element placed between the fuze and the high explosive.

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • Not applicable. [0001]
  • STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH
  • Not applicable [0002]
  • TECHNICAL FIELD
  • The present invention relates to a projectile which incorporates an ignition delay element between the fuze and the high explosive. [0003]
  • BACKGROUND OF THE INVENTION
  • High explosive rounds of ammunition with mechanical fuzes typically use super quick initiation. This often prevents the projectile from entering soft or semi-armored targets prior to the initiation event, which results in little or no damage to the target. Therefore, adding a delay to allow penetration of the soft or semi-armored target is desirable. [0004]
  • Prior devices have attempted to incorporate the delay element in the fuze itself. This has proven to be an expensive alternative. Chemically fuzed projectiles also exist, but these projectiles fail at high impact angles or at extended ranges. Also, chemically fuzed projectiles do not contain mechanical or physical barriers that require two separate and independent environments for fuze arming to occur. [0005]
  • BRIEF SUMMARY OF THE INVENTION
  • Applicants have solved the problems discussed above by utilizing current low cost mechanical fuze designs and with the addition of a pyrotechnic ignition delay element which is placed between the fuze and the high explosive. [0006]
  • BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWING
  • A detailed description of the invention is hereafter described with specific reference being made to the drawings in which: [0007]
  • FIG. 1 is a side view of the inventive projectile.[0008]
  • DETAILED DESCRIPTION OF THE INVENTION
  • While this invention may be embodied in many different forms, there are shown in the drawings and described in detail herein specific preferred embodiments of the invention. The present disclosure is an exemplification of the principles of the invention and is not intended to limit the invention to the particular embodiments illustrated. [0009]
  • FIG. 1 shows a side view of a [0010] standard projectile 10, which includes a fuze 12 at the front end of the projectile and a charge of high explosive at 14. A pyrotechnic delay element 16 is placed between the fuze 12 and the high explosive 14. In the preferred embodiment, the pyrotechnic delay element is comprised of a modified IM-68 incendiary mix, which is comprised of:
  • ˜24.2% barium nitrate; [0011]
  • ˜24.2% ammonium nitrate; [0012]
  • ˜48.6% Mg/Al Alloy, and [0013]
  • ˜3.0% Zinc Stearate [0014]
  • In testing with a 30 mm projectile ˜5 grams of the modified IM-68 powder were placed and consolidated on top of the high explosive [0015] 14, and this was found to provide an adequate delay to initiation.
  • The above examples and disclosure are intended to be illustrative and not exhaustive. These examples and description will suggest many variations and alternatives to one of ordinary skill in this art. All these alternatives and variations are intended to be included within the scope of the attached claims. Those familiar with the art may recognize other equivalents to the specific embodiments described herein which equivalents are also intended to be encompassed by the claims attached hereto. [0016]

Claims (4)

What is claimed is:
1. A projectile of the type having a housing, the housing containing a fuze and a charge of high explosive, the improvement comprising:
a pyrotechnic delay element placed between the fuze and the high explosive.
2. The projectile of claim 1 wherein the projectile has front and rear ends and the fuze is located at the front end of the projectile.
3. The projectile of claim 1 wherein the pyrotechnic delay element is a modified IM-68.
4. The projectile of claim 3 wherein the pyrotechnic delay element comprises:
approximately 24.2% barium nitrate;
approximately 24.2% ammonium nitrate;
approximately 48.6% Mg/Al Alloy, and
approximately 3.0% Zinc Stearate
US10/115,469 2002-04-02 2002-04-02 Mechanically fuzed high explosive projectile using pryotechnic initiation delay Abandoned US20030183111A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US10/115,469 US20030183111A1 (en) 2002-04-02 2002-04-02 Mechanically fuzed high explosive projectile using pryotechnic initiation delay
NO20031241A NO20031241L (en) 2002-04-02 2003-03-18 Mechanically secured high explosive projectile using pyrotechnic ignition delay
EP03007336A EP1351032A2 (en) 2002-04-02 2003-04-01 Mechanically fuzed high explosive projectile using pryotechnic initiation delay

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/115,469 US20030183111A1 (en) 2002-04-02 2002-04-02 Mechanically fuzed high explosive projectile using pryotechnic initiation delay

Publications (1)

Publication Number Publication Date
US20030183111A1 true US20030183111A1 (en) 2003-10-02

Family

ID=22361607

Family Applications (1)

Application Number Title Priority Date Filing Date
US10/115,469 Abandoned US20030183111A1 (en) 2002-04-02 2002-04-02 Mechanically fuzed high explosive projectile using pryotechnic initiation delay

Country Status (3)

Country Link
US (1) US20030183111A1 (en)
EP (1) EP1351032A2 (en)
NO (1) NO20031241L (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100242769A1 (en) * 2005-07-01 2010-09-30 Saab Ab Ammunition unit
WO2021118986A1 (en) * 2019-12-12 2021-06-17 Bae Systems Information And Electronic Systems Integration Inc. Additively manufactured self-destructive delay device

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3949675A (en) * 1974-07-03 1976-04-13 The United States Of America As Represented By The Secretary Of The Army Projectile
US4004521A (en) * 1976-04-01 1977-01-25 The United States Of America As Represented By The Secretary Of The Army Projectile fuze
US4736683A (en) * 1986-08-05 1988-04-12 Exxon Chemical Patents Inc. Dry ammonium nitrate blasting agents
US5652408A (en) * 1994-07-22 1997-07-29 Manurhin Defense Explosive projectile
US6033500A (en) * 1995-07-27 2000-03-07 Sensor Technology Co., Ltd. Airbag explosive composition and process for producing said composition

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3949675A (en) * 1974-07-03 1976-04-13 The United States Of America As Represented By The Secretary Of The Army Projectile
US4004521A (en) * 1976-04-01 1977-01-25 The United States Of America As Represented By The Secretary Of The Army Projectile fuze
US4736683A (en) * 1986-08-05 1988-04-12 Exxon Chemical Patents Inc. Dry ammonium nitrate blasting agents
US5652408A (en) * 1994-07-22 1997-07-29 Manurhin Defense Explosive projectile
US6033500A (en) * 1995-07-27 2000-03-07 Sensor Technology Co., Ltd. Airbag explosive composition and process for producing said composition

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100242769A1 (en) * 2005-07-01 2010-09-30 Saab Ab Ammunition unit
WO2021118986A1 (en) * 2019-12-12 2021-06-17 Bae Systems Information And Electronic Systems Integration Inc. Additively manufactured self-destructive delay device
US11287232B2 (en) 2019-12-12 2022-03-29 Bae Systems Information And Electronic Systems Integration Inc. Additively manufactured self-destructive delay device

Also Published As

Publication number Publication date
NO20031241D0 (en) 2003-03-18
NO20031241L (en) 2003-10-03
EP1351032A2 (en) 2003-10-08

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Legal Events

Date Code Title Description
AS Assignment

Owner name: ALLIANT TECHSYSTEMS INC., MINNESOTA

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:TASSON, BRIAN B.;REEL/FRAME:012776/0512

Effective date: 20020402

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION

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