US20030183111A1 - Mechanically fuzed high explosive projectile using pryotechnic initiation delay - Google Patents
Mechanically fuzed high explosive projectile using pryotechnic initiation delay Download PDFInfo
- 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
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B3/00—Blasting cartridges, i.e. case and explosive
- F42B3/10—Initiators therefor
- F42B3/16—Pyrotechnic 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:
Landscapes
- 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
- Not applicable.
- Not applicable
- 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.
- 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.
- 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.
- A detailed description of the invention is hereafter described with specific reference being made to the drawings in which:
- FIG. 1 is a side view of the inventive projectile.
- 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.
- FIG. 1 shows a side view of a
standard projectile 10, which includes afuze 12 at the front end of the projectile and a charge of high explosive at 14. Apyrotechnic delay element 16 is placed between thefuze 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;
- ˜24.2% ammonium nitrate;
- ˜48.6% Mg/Al Alloy, and
- ˜3.0% Zinc Stearate
- In testing with a 30 mm projectile ˜5 grams of the modified IM-68 powder were placed and consolidated on top of the high explosive14, 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.
Claims (4)
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
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)
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)
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 |
-
2002
- 2002-04-02 US US10/115,469 patent/US20030183111A1/en not_active Abandoned
-
2003
- 2003-03-18 NO NO20031241A patent/NO20031241L/en not_active Application Discontinuation
- 2003-04-01 EP EP03007336A patent/EP1351032A2/en not_active Withdrawn
Patent Citations (5)
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)
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 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US7765934B2 (en) | Lead-free projectile | |
US4497253A (en) | Armor-piercing projectile | |
US4648324A (en) | Projectile with enhanced target penetrating power | |
US5033382A (en) | Piezoelectric fuse for projectile with safe and arm mechanism | |
US4793256A (en) | Piezoelectric fuse for projectile with safe and arm mechanism | |
US11802755B2 (en) | Penetrator, use of a penetrator, and projectile | |
US5325787A (en) | Armor-piercing fragmentation projectile | |
WO2003051794A3 (en) | Dual mode fuze | |
JP7108685B2 (en) | Fully armored safety bullet especially for multi-purpose use | |
US5157221A (en) | Ammunition unit with adaptive impact fuze | |
US4714022A (en) | Warhead with tandem shaped charges | |
IL178866A (en) | Lead-free projectile with a hollow hard core | |
US5445079A (en) | Armor-piercing fragmentation projectile | |
RU2751328C1 (en) | Projectile with a pyrotechnical battle charge | |
GB2113362A (en) | Hollow charges | |
US20030183111A1 (en) | Mechanically fuzed high explosive projectile using pryotechnic initiation delay | |
US20110011296A1 (en) | Subprojectile having an energy content | |
US5612505A (en) | Dual mode warhead | |
HU202976B (en) | Warhead ammunition | |
US5355801A (en) | Small caliber fuze with arming delay, second impact and graze sensitivity | |
US4471698A (en) | Mass-spring rainhead | |
US4471696A (en) | High explosive projectile fuzing | |
GB2109513A (en) | Rifle grenade | |
RU2400697C2 (en) | 'tveritch-3' high-explosive projectile for short-range artillery piece | |
JPS59157499A (en) | Warhead fuse |
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 |