EP0898692A1 - Munition mit einer infrarotstrahlung emittierenden leuchtladung - Google Patents

Munition mit einer infrarotstrahlung emittierenden leuchtladung

Info

Publication number
EP0898692A1
EP0898692A1 EP97932134A EP97932134A EP0898692A1 EP 0898692 A1 EP0898692 A1 EP 0898692A1 EP 97932134 A EP97932134 A EP 97932134A EP 97932134 A EP97932134 A EP 97932134A EP 0898692 A1 EP0898692 A1 EP 0898692A1
Authority
EP
European Patent Office
Prior art keywords
flare
flares
base propellant
nir
composition
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.)
Withdrawn
Application number
EP97932134A
Other languages
English (en)
French (fr)
Other versions
EP0898692A4 (de
Inventor
Patricia L. Farnell
Russell Broad
Stuart Nemiroff
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of EP0898692A1 publication Critical patent/EP0898692A1/de
Publication of EP0898692A4 publication Critical patent/EP0898692A4/de
Withdrawn legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C06EXPLOSIVES; MATCHES
    • C06CDETONATING OR PRIMING DEVICES; FUSES; CHEMICAL LIGHTERS; PYROPHORIC COMPOSITIONS
    • C06C15/00Pyrophoric compositions; Flints
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B4/00Fireworks, i.e. pyrotechnic devices for amusement, display, illumination or signal purposes
    • F42B4/26Flares; Torches

Definitions

  • the U.S. Army has certain rights and licenses in the above invention by grant from the above inventors .
  • This invention concerns covert flare articles, compositions and systems; these are for situations which use infra-red night vision techniques.
  • night vision systems There are two common types of night vision systems; one type uses special goggles that amplify the existing light.
  • the other type uses a flare which has a payload or candle that burns and emits near infra red (NIR) illumination. This is used in combination with infra red sensitive night vision goggles.
  • NIR near infra red
  • the flares should desirably have a high IR output, a fast burn time and a very favorable IR/visible light ratio. It is also important that chunking of the burning flare composition be controlled.
  • the United States Navy has developed one such system which uses a flare known as Black Knight.
  • Thiokol Corporation has reported a system known as Thiolite which is described in U.S. P. 5,056,435, Jones et al, October 15, 1991. There are deficiencies in these systems in that the Black Knight flare has a relatively long burn time, a low intensity of infra red illumination and a low IR/visible ratio.
  • the reported product from Thiokol Corporation included boron to increase the burn rate and increase intensity. These used potassium nitrate or potassium perchlorate as oxidizers. The IR/visible ratio was not improved and chunking was observed. There is need for an improved night vision flare and system using the flare.
  • the improved covert flares of this invention have increased intensity of NIR illumination, fast burn rates and a very favorable IR/visible ratio.
  • the combination of these properties has resulted in substantial improvement and acceptability of the flares of this invention.
  • the conventional flare infra-red candle composition can be modified to increase the burn rate while maintaining a substantially uniform burning of the candle, without substantial chunking or subdivision into embers .
  • the invention uses a small amount of an additive selected from the group consisting of a primary energetic material, a single base propellant material, a double base propellant material, a triple base propellant material and mixtures thereof to significntly improve the properties of conventional NIR flares.
  • the mechanism of the action of the additive in the candle composition is to increase the surface which is burning and , to some extent, cause an expulsion of composition from the flare while the flare is burning.
  • the effect of the additive is to increase burn rate and increase NIR output while keeping a favorable IR/visable light ratio and avoiding chunking.
  • a desired formulation will use an oxidant with strong emission in the near infra red , such as cesium nitrate or mixtures in which cesium nitrate is the major ingredient such as cesium nitrate and potassium nitrate; a metallic fuel with low visible light emission, such as silicon; a near infra-red emission enhancer, such as hexamine; a binder such as a nitrogen containing epoxy resin and a small amount of the additive. Nitrocellulose based additives are preferred materials because they do not decompose under shear as is the tendency with black powder and red powder.
  • Nitrocellulose with or without a plasticizer is a traditional single base propellant material.
  • a suitable double base propellant material is nitrocellulose and nitroglycerin .
  • a suitable triple base propellant material is nitrocellulose, nitroglycerin and nitroguanidine.
  • the overall night vision system has a delivery system for the flare such as a mortar, an artillery round, a rocket or a bomb.
  • One or more flares are delivered to the target area; these flares will be of conventional construction which includes a housing, an ignition train, a propellant charge and the candle or payload with the flare composition.
  • the burning flare illuminates the target area with the high intensity NIR.
  • the highly illuminated target area can be seen through infra red sensitive night vision goggles.
  • the low visible light output will cause the flare to be virtually invisible to the unaided eye. This is very important for a successful covert operation.
  • FIG. 1 illustrates a manufacturing process for a total flare and this includes the steps for the preparation of the candle according to this invention.
  • the invention can be applied to any conventional payload delivery system.
  • a preferred range of current weapon sizes are 40, 60, 81 and 120 mm. rounds. These can be fired by gun or mortar or can be hand held signals such as the 40 mm.
  • the invention has an advantage in that the faster burn time of the composition allows for additional volume in the candle. The excess volume can be filled with an inert material for matching ballistic performance or the active ingredient to provide greater illumination intensity or burn time.
  • the burn time range is about 40 to 90 seconds. It should be understood that the elevation of the flare during burning affects the area which is illuminated and the time available for the burn time of the flare.
  • the Nitrocellulose was a conventional single base propellant material and had about 13% Nitrogen.
  • the black powder was added at the end of the mixing cycle because it breaks up under shear. Red powder has a similar behavior.
  • the flares are prepared by forming a mixture of the ingredients and then pressing this mixture into a container which forms the candle. After mixing the initial ingredients, the composition should be free of solvent for best results .
  • the ingredients in the article can be pressed from top to bottom of from bottom to top. The pressure of pressing will be about 7,000 psi.
  • compositions of this invention can be readily prepared in different sizes.
  • the flares can be made up in the form of rounds to fit 40mm, 60 mm., 81 mm or 120 mm mortars.
  • the flares are capable of producing a large amount of radiation in the near infra red region of about .75 to 1.0 microns .
  • the effect of the additive is to impart a faster burning rate which increases the intensity of the NIR illumination.
  • the additives may be used separately or in combination with each other. It is easiest to fabricate the compositions when nitrocellulose based propellant materials are used.
  • the preferred ingredients will also include a major amount of the cesium nitrate oxidizer, a minor amount of a potassium nitrate or chlorate oxidizer, a small amount of metal fuel such as about 5 to 15 wt. % of silicon metal, an amount of hexamine sufficient to enhance emission in the NIR region, about 16%, and a binder in about 4 wt%.
  • a suitable binder is amine curable, aromatic based epoxy resin.
  • a weapon system having a delivery means and a munition, said munition having an infrared illuminating composition , said composition containing a relatively small amount of an additive selected from the group consisting of a primary energetic material, a single base propellant material, a double base propellant material, and a triple base propellant.
  • a munition having an infrared illuminating composition said composition containing a relatively small amount of an additive selected from the group consisting of a primary energetic material, a single base propellant material, a double base propellant material, and a triple base propellant.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Metallurgy (AREA)
  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Fats And Perfumes (AREA)
EP97932134A 1997-05-07 1997-05-07 Munition mit einer infrarotstrahlung emittierenden leuchtladung Withdrawn EP0898692A4 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
PCT/US1997/007722 WO1998002712A1 (en) 1997-05-07 1997-05-07 Munitions using infrared flare weapon systems
1999-05-06

Publications (2)

Publication Number Publication Date
EP0898692A1 true EP0898692A1 (de) 1999-03-03
EP0898692A4 EP0898692A4 (de) 2000-02-23

Family

ID=22260858

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97932134A Withdrawn EP0898692A4 (de) 1997-05-07 1997-05-07 Munition mit einer infrarotstrahlung emittierenden leuchtladung

Country Status (3)

Country Link
EP (1) EP0898692A4 (de)
AU (1) AU3566897A (de)
WO (1) WO1998002712A1 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19818337C1 (de) * 1998-04-23 1999-11-18 Buck Werke Gmbh & Co Kg Pyrotechnische Wirkmasse mit Anzünd- und Abbrandbeschleuniger

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3856590A (en) * 1945-04-18 1974-12-24 Director Office Of Scient Res Propellants and method of producing the same
US3951706A (en) * 1962-07-03 1976-04-20 Eldridge Judson B Solid propellant mixtures and process of preparation
GB2246348A (en) * 1986-07-15 1992-01-29 Ici Plc Nitrocellulose propellant composition

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3421708A1 (de) * 1984-06-12 1985-12-12 Buck Chemisch-Technische Werke GmbH & Co, 7347 Bad Überkingen Einrichtung zur erzeugung einer scheinzielwolke, insbesondere einer infrarot-scheinzielwolke
DE3515166A1 (de) * 1985-04-26 1986-10-30 Buck Chemisch-Technische Werke GmbH & Co, 7347 Bad Überkingen Wurfkoerper zur darstellung eines infrarot-flaechenstrahlers
US5056435A (en) 1989-11-29 1991-10-15 Jones Leon L Infrared illuminant and pressing method
FR2694804B1 (fr) * 1992-08-11 1994-09-16 Poudres & Explosifs Ste Nale Leurre stabilisée et propulsé, émettant dans l'infrarouge.
US5320691A (en) * 1993-07-08 1994-06-14 The United States Of America As Represented By The Secretary Of The Army Charcoal-free black powder type granules and method of production
US5587552A (en) * 1993-11-09 1996-12-24 Thiokol Corporation Infrared illuminating composition

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3856590A (en) * 1945-04-18 1974-12-24 Director Office Of Scient Res Propellants and method of producing the same
US3951706A (en) * 1962-07-03 1976-04-20 Eldridge Judson B Solid propellant mixtures and process of preparation
GB2246348A (en) * 1986-07-15 1992-01-29 Ici Plc Nitrocellulose propellant composition

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO9802712A1 *

Also Published As

Publication number Publication date
EP0898692A4 (de) 2000-02-23
AU3566897A (en) 1998-04-02
WO1998002712A1 (en) 1998-01-22

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