KR20030042184A - Fuel Air Explosive Munition - Google Patents
Fuel Air Explosive Munition Download PDFInfo
- Publication number
- KR20030042184A KR20030042184A KR1020010072834A KR20010072834A KR20030042184A KR 20030042184 A KR20030042184 A KR 20030042184A KR 1020010072834 A KR1020010072834 A KR 1020010072834A KR 20010072834 A KR20010072834 A KR 20010072834A KR 20030042184 A KR20030042184 A KR 20030042184A
- Authority
- KR
- South Korea
- Prior art keywords
- fuel
- fae
- ignition
- filled
- explosive
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/46—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/46—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances
- F42B12/50—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing gases, vapours, powders or chemically-reactive substances by dispersion
- F42B12/52—Fuel-air explosive devices
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Dispersion Chemistry (AREA)
- Air Bags (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Description
본 발명은 개량된 연료기화폭발탄(이하 FAE탄으로 약칭한다)에 관한 것으로서, 더욱 상세하게는 지뢰, 수류탄을 포함하는 유탄, 휴대용 로켓, 대전차로켓 또는 유도탄, 다연장로켓탄, 포탄 및 폭파용키트 등의 무기체계에 응용 할 수 있는 개량된 FAE탄에 관한 것이다.The present invention relates to an improved fuel vapor bomb (hereinafter abbreviated as FAE), more specifically, mines, grenades including grenades, portable rockets, anti-tank rockets or guided missiles, multiple extended rockets, shells and blasting kits An improved FAE can be applied to weapon systems.
FAE탄 이라고 함은 폭풍형 무기로서, 연료를 공기 중에 분산시킨 뒤 일정한 지연시간 후 점화용 기폭장치를 이용하여 분산된 연료를 폭굉시켜 생성되는 과압과 온도를 이용하여 표적을 파괴하는 폭탄이다.FAE ammunition is a bomb-type weapon. It is a bomb that destroys a target by using overpressure and temperature generated by dispersing fuel in the air and detonating the dispersed fuel using a ignition detonator after a certain delay time.
FAE탄은 1960년대부터 개발하기 시작하여 1970년대 이후 본격적으로 전장에 사용되었다.FAE bullets began to be developed in the 1960s and have been used in battle since the 1970s.
FAE탄은 제작과 신뢰도 측면에서 몇 가지 중요한 단점을 가지고 있기 때문에 1980년대 후반 이후 러시아 등에서 이를 개선하여 성능이 향상된 FAE 탄두가 개발되어 왔다.FAE bullets have some important drawbacks in terms of production and reliability, and have been developed in Russia and other countries since the late 1980s to improve their performance.
전형적인 FAE탄은 기본적으로 탄체, 연료, 폭발계열(뇌관, 기폭관, 전폭약, 분산폭약) 및 2차 기폭 점화장치로 구성되어 있다.A typical FAE bomb is basically composed of coal body, fuel, explosion series (primers, detonators, full explosives, dispersed explosives) and secondary detonation ignition.
이러한 FAE(Fuel Air Explosive)의 작동 메커니즘은 연료 분산과 기폭의 2단계로 구성되어 있기 때문에 신관과 폭발계열이 이원화되어 있다.Since the FAE (Fuel Air Explosive) operating mechanism is composed of two stages of fuel dispersing and detonation, the fuse and explosion series are dualized.
이는 일반적으로 단일신관 폭발계열을 갖는 재래식 무기에 비하여 작동 신뢰도가 떨어진다는 것을 의미한다.This generally means less operational reliability than conventional weapons with single fuse explosions.
종래의 FAE탄은 분산된 연료를 점화시키기 위한 2차 기폭장치라는 특수장치를 탄에 결합하고 있고, 밀도가 낮은 액체연료를 사용하기 때문에 탄의 부피가 커질 뿐만 아니라 구조가 매우 복잡해서 제작이 어렵다.Conventional FAE coal combines a special device called a secondary detonator to ignite the dispersed fuel, and because of the low density liquid fuel, the bulk of the coal is not only large but also the structure is very complicated, making it difficult to manufacture. .
또한 주로 산화에틸렌이나 산화프로필렌처럼 휘발성이 크고 독성이 높아 위해성이 큰 액체연료를 사용하기 때문에 탄체 충전 작업이 어려우며, 증기압이 높기 때문에 탄의 저장시 연료의 누출 문제 등 많은 단점을 가지고 있다.In addition, it is difficult to fill the carcass due to the high risk of high volatility and high toxicity, such as ethylene oxide and propylene oxide, and the high vapor pressure has many disadvantages such as fuel leakage during storage of coal.
또한 비중이 작은 액체연료를 사용하기 때문에 발사용 탄약으로 적용이 불가능하였고 주로 항공기 투하탄 중심으로 개발되었다.In addition, since it uses liquid fuel with a small specific gravity, it was not applicable to ammunition for launching and was mainly developed for aircraft jets.
FAE탄이 가지고 있는 이와 같은 단점들을 해결하기 위해 탄의 구조를 변경하는 방법, 또는 2차 기폭장치를 개선하거나 없애는 방법 등 여러 가지 기술들이 개발되었다.To address these shortcomings of FAE, various techniques have been developed, such as changing the structure of the bullet or improving or eliminating secondary detonators.
FAE탄의 구조를 변경한 예로서 미국특허 제 4,074,628 호에서는 2중관 개념을 벗어나 분산폭약이 탄체의 밑쪽에 위치한 FAE 캐니스터에 대한 발명을 설명하고 있다.As an example of changing the structure of the FAE coal, US Patent No. 4,074,628 describes the invention of a FAE canister in which the explosive explosive is located at the bottom of the coal body beyond the double pipe concept.
또 다른 예로서 미국특허 제 5,425,311 호는 3중관 개념의 FAE 탄두에 대한 발명이다.As another example, U. S. Patent No. 5,425, 311 discloses a FAE warhead in the triple tube concept.
한편 신뢰성 있는 FAE탄을 만들기 위해서 미국특허 제 3,992,995 호, 미국특허 제 3,994,226 호, 미국특허 제 3,999,482 호, 미국특허 제 4,297,949 호에서는 개선된 2차 기폭장치에 대한 발명을 서술하고 있다.Meanwhile, in order to make a reliable FAE, US Patent No. 3,992,995, US Patent No. 3,994,226, US Patent No. 3,999,482 and US Patent No. 4,297,949 describe the invention of the improved secondary detonator.
그러나 상기 특허 발명들은 모두가 2차 기폭장치를 FAE탄에 결합시켜서 운용해야만 한다는 단점을 갖고 있다.However, the patent inventions have the disadvantage that all have to operate the secondary detonator coupled to the FAE bullet.
2차 기폭장치란 분산폭약에 의해 공기 중에 살포된 연료가 최적의 조건에 도달했을 때 연료-공기혼합 구름을 기폭 시키는 장치이다.The secondary detonator is a device for detonating the fuel-air mixture cloud when the fuel sprayed into the air by the dispersing explosive reaches an optimum condition.
여기서 최적 조건은 연료가 분산폭약에 의해 공기 중에 분산되어 연료-공기 혼합 구름 속의 연료의 농도(부피%)가 폭굉한계 범위 내에 있을 때를 말한다.Optimum conditions here are when the fuel is dispersed in the air by means of a dispersing explosive so that the concentration of the fuel in the fuel-air mixture cloud (% by volume) is within the detonation range.
따라서 2차 기폭장치는 연료가 분산됨과 동시에 탄 몸체에서 이탈되어 연료가 최적의 조건에 도달했을 때 정확한 위치에서 작동해야 한다.Therefore, the secondary detonator must run in the correct position when the fuel is dispersed and dislodged from the body of the bullet and the fuel reaches its optimum condition.
다시 말해서 일정한 지연시간 후 연료의 농도분포가 최적의 조건에 있을 동안에만 작동하여 분산된 연료를 기폭 시켜야 한다.In other words, after a certain delay, the fuel should be operated only while the concentration distribution of the fuel is in optimum condition to trigger the dispersed fuel.
하지만, 지연시간은 10 ∼ 100msec 정도이고, 연료가 폭굉 가능한 시간은 수십 msec이므로, 이 시간 내에 2차 기폭장치를 정확하게 작동하도록 만드는 일은 매우 어렵다.However, since the delay time is about 10 to 100 msec and the fuel can be detonated for several tens of msec, it is very difficult to make the secondary detonator operate correctly within this time.
주 연료를 공기 중에 넓은 면적에 분산시키기 위한 탄체 두께의 설계나 폭발계열의 설계가 매우 중요하고, 전체적으로 분산된 연료의 농도분포가 최적 조건에있을지라도 2차 기폭장치가 작동하는 지점의 연료-공기 혼합구름의 농도 분포가 폭굉 한계를 벗어난다면 연료는 기폭되지 않는다.It is very important to design the thickness of the body or the design of the explosion series to disperse the main fuel in a large area in the air. If the concentration distribution of the mixed cloud is outside the detonation limit, the fuel is not detonated.
또한, 2차 기폭장치가 정상적으로 작동했지만, 화염이 분산된 연료 전체에 걸쳐 전파되지 않는다면 원하는 FAE 효과를 얻지 못하게 된다.In addition, if the secondary detonator is operating normally, but the flame does not propagate throughout the dispersed fuel, the desired FAE effect will not be achieved.
미국특허 제 3,570,401 호와 미국특허 제 3,730,093 호는 격막을 사용하여 분리 충전된 연료와 점화원 및 분산 장약을 이용한 임플러젼(Implosion)형 FAE탄에 대한 폭발장치에 관한 것이다.US Pat. No. 3,570,401 and US Pat. No. 3,730,093 relate to an explosive device for an implosion type FAE bomb using a septum-filled fuel and an ignition source and dispersion charge.
이러한 탄두를 FAE탄에 적용한다면, 2차 기폭장치를 사용할 필요는 없지만, 연료가 분산됨과 동시에 점화제와 반응하여 폭굉으로 전이하거나, 분산폭약에 의한 점화제의 폭발에너지가 연료를 기폭시켜 주어야 한다.If such a warhead is applied to a FAE, it is not necessary to use a secondary detonator, but the fuel will disperse and react with the ignition agent to transfer to detonation, or the explosive energy of the ignition agent from the explosive explosives will detonate the fuel. .
하지만, 연료가 충분히 분산되기 전에 점화제가 연료를 기폭시킬 수도 있고, 연료-점화제의 반응이 폭발로 전이하는 과정이 실험실 규모의 시험에서는 쉽게 일어나는 현상이지만 실제 무기체계에 적용시에는 폭발이 일어나지 않을 수도 있고, 단순 연소로 끝나는 문제점이 있다.However, the ignition agent may detonate the fuel before it is sufficiently dispersed, and the process of transitioning the fuel-ignition agent reaction to an explosion is an easy phenomenon in laboratory tests, but it is unlikely that an explosion will occur in an actual weapon system. There is also a problem that ends with simple combustion.
또한 이 기술을 이용할 경우 기존의 FAE탄 보다 구조가 복잡해지고, 제조공정이 복잡하고, 비용이 많이 소요된다.In addition, using this technology, the structure is more complicated, the manufacturing process is more complicated and expensive than the existing FAE coal.
점화제로 사용되는 물질들이 주로 금속, 금속산화물이나 이들의 혼합물이기 때문에 작업시 취급이 어렵거나 유해한 경우가 많다.Since the materials used as ignition agents are mainly metals, metal oxides, or mixtures thereof, they are often difficult or harmful to handle.
본 발명은 상술한 바와 같은 종래의 FAE탄의 문제점을 개선한 것으로서, 2차기폭장치를 사용하지 않아서 구조가 간단하고, FAE탄의 작동신뢰도가 높으며, 제조비용이 저렴한 FAE탄을 제공하며, 동시에 항공기 투하탄 뿐만 아니라 일반 무기체계, 즉 지뢰, 수류탄을 포함하는 유탄, 휴대용로켓, 대전차로켓 또는 대전차 유도탄 및 대함, 대공 유도탄, 다연장로켓탄, 포탄, 폭파용키트 등에 이용 할 수 있는 FAE탄을 제공하는데 기술적 과제를 둔 것이다.The present invention improves the problems of the conventional FAE coal as described above, and does not use a secondary detonator, thereby providing a simple structure, high reliability of operation of the FAE coal, and a low manufacturing cost. In addition to aircraft missiles, it is technically capable of providing general weapons systems such as mines, grenades containing grenades, portable rockets, anti-tank rockets or anti-tank guided missiles, and FAE bullets that can be used for anti-aircraft, anti-aircraft missiles, multiple rockets, shells and blasting kits. It is a task.
도 1은 본 발명에 의한 FAE탄의 단면 개략도.1 is a schematic cross-sectional view of a FAE bullet according to the present invention.
본 발명을 예시도면에 의하여 상세히 설명한다.The present invention will be described in detail by way of illustration.
도 1은 본 발명에 의한 FAE탄의 요부를 절개한 정면도로서, 1은 탄체, 2는 마개, 3은 폭관, 4는 분산-점화장약, 5는 연료, 6은 신관 또는 점화장치, 7은 가스충전구마개이다.1 is a front view of the main portion of the FAE bullet according to the present invention, in which 1 is a body, 2 is a stopper, 3 is a width pipe, 4 is a dispersion-ignition charge, 5 is a fuel, 6 is a fuse or an ignition device, and 7 is a gas. It is a filling plug.
즉 본 발명의 FAE탄은 기본적으로 탄체(1), 연료(5) 및 분산-점화장약(4)의 3가지로 간단하게 구성되어 있다.In other words, the FAE coal of the present invention is basically composed of three simple pieces: a coal body 1, a fuel 5, and a dispersion-ignition filler 4.
탄체(1)은 철 또는 비철금속 재질로 되어 있으며 두께는 5mm 이하이며, 한쪽은 마개(2)로 밀봉되어 있다.The body 1 is made of ferrous or non-ferrous metal and has a thickness of 5 mm or less, and one side is sealed with a stopper 2.
탄체(1)의 외부는 탄두 충전물이 폭발할 때 위력을 증가시키기 위해 탄체(1)의 상부, 하부 및 중간부분이 도 1에 나타난 바와 같이 덧살(1')로 강화되어 있다.The exterior of the carcass 1 is reinforced with a dent 1 ', as shown in Figure 1, in the upper, lower and middle portions of the carcass 1 to increase the power when the warhead filling explodes.
탄체(1)의 내부에는 연료(5)와 분산-점화장약(4)을 함유하고 있는 폭관(3)이 내장되어 있다.Inside the body 1, a width tube 3 containing a fuel 5 and a dispersion-ignition charge 4 is incorporated.
폭관(3)은 탄소강으로 되어 있으며 그 두께는 약 2.5 ∼ 3.0mm이다.The width pipe 3 is made of carbon steel and has a thickness of about 2.5 to 3.0 mm.
폭관(3)의 내부에는 RDX(hexahydro-1,3,5-trinitro-1,3,5-triazine),Aluminized RDX, 콤포지션 폭약과 같은 고폭약 계열로 이루어진 분산-점화장약(4)이 충전되어 있다.The inside of the tube 3 is filled with a dispersion-ignition agent (4) consisting of a series of high explosives such as hexahydro-1,3,5-trinitro-1,3,5-triazine (RDX), aluminized RDX, and a composition explosive. have.
분산-점화장약(4)는 펠렛 형태 또는 주조식으로 충전되어 있으며 연료(5)를 분산하면서 점화시켜주는 역할을 한다.The dispersion-ignition charge 4 is filled in pellet form or cast and serves to ignite while dispersing the fuel 5.
연료(5)는 액체 연료를 사용한 FAE와 고체 연료를 사용한 FAE의 장점을 동시에 가질 수 있도록 고체연료와 액상점화제 또는 고체연료, 액체연료 및 점화제를 블랜딩하여 슬러리화 시킨 것이다.Fuel (5) is a slurry by blending a solid fuel and a liquid tackifier or a solid fuel, a liquid fuel and an ignition agent so as to have the advantages of FAE using a liquid fuel and FAE using a solid fuel at the same time.
신관 또는 점화장치(6)은 탄두가 표적에 명중시 작동하여 분산-점화장약(4)를 기폭시키는 장치로 통상적인 전기식이나 기계식 모두 적용이 가능하다.The fuse or ignition device 6 is a device for detonating the dispersion-ignition charge 4 when the warhead hits the target and can be applied to both conventional electric and mechanical methods.
가스 충전구 마개(7)은 충전연료의 장기 저장시 산화반응을 방지하기 위해 가스충전구로 질소나 아르곤 가스를 충전한 다음에 가스충전구를 밀봉시켜 주는 것이다.Gas filling plug 7 is to fill the gas filling after filling the nitrogen or argon gas into the gas filling in order to prevent the oxidation reaction during long-term storage of the filling fuel.
보다 안전한 연료의 충전을 위해 질소나 아르곤 가스가 충전된 건조 랩(Dry-Lab) 내에서 충전작업을 수행 할 수 있다.Filling can be performed in a dry lab filled with nitrogen or argon gas for safer fuel filling.
본 발명에서 연료(5)의 고체성분으로는 금속성분으로서 알루미늄, 비금속성분으로서 붕소, 산화제성분으로서 알루미늄산화물, 고분자화합물로서 분말상 폴리에틸렌, 고폭약으로서 TNT중에서 선택한 것이며, 액체성분으로는 저분자량의 알칸, 제트연료, 노말헵탄 등에서 선택한 것이며, 점화제는 브로마인 트리플루오라이드(bromine trifluoride), 알킬 나이트레이트(alkyl nitrate) 등에서 선택한 것이다.In the present invention, the solid component of the fuel 5 is selected from aluminum as a metal component, boron as a nonmetal component, aluminum oxide as an oxidant component, powdered polyethylene as a high molecular compound, and TNT as a high explosive, and a low molecular weight alkane as a liquid component. , Jet fuel, normal heptane and the like, the ignition agent is selected from bromine trifluoride, alkyl nitrate and the like.
본 발명에 의한 FAE탄의 조립순서는 다음과 같다.The assembly sequence of FAE coal according to the present invention is as follows.
먼저 폭관(3)을 탄체(1)에 압입하여 결합한다.First, the width pipe 3 is pressed into the body 1 to be coupled.
비활성 가스로 탄체(1)의 내부를 채운 다음 연료(5)를 혼합하여 충전한 후 마개(2)를 이용하여 밀봉한다.The inside of the carbon body 1 is filled with inert gas, and then the fuel 5 is mixed and filled, and then sealed using a stopper 2.
폭관(3)에 분산-점화장약(4)를 삽입한 뒤 신관 또는 점화장치(6)를 결합하면 된다.Insert the dispersion-ignition charge (4) into the tube (3) and then combine the fuse or ignition device (6).
본 발명을 적용한 로켓탄두의 작동 메커니즘은 다음과 같다.The operating mechanism of the rocket warhead to which the present invention is applied is as follows.
본 발명에 의한 FAE탄이 발사되면 탄이 발사관에서 떠날 때의 관성에 의해 신관(6)이 무장(arming)된다.When the FAE shot according to the present invention is fired, the fuse 6 is armed by the inertia when the shot leaves the launch tube.
탄이 표적에 타격되면 관성에 의해 신관(6)이 작동하여 뇌관 또는 부스타(도 1에 표시하지 않았음)가 폭관(3) 내부에 충전된 분산-점화장약(4)를 점화시킨다.When the bullet hits the target, the fuse 6 is actuated by inertia so that a primer or booster (not shown in FIG. 1) ignites the dispersion-ignition charge 4 filled inside the tube 3.
점화된 분산-점화장약(4)의 폭발에너지가 탄체(1)을 파열시켜 연료(5)를 분산시킨다.The explosion energy of the ignited dispersion-ignition charge 4 ruptures the carbon 1 and disperses the fuel 5.
가연성 연료(5)는 분산됨과 동시에 분산-점화장약(4)의 에너지를 이용하여 공기 중의 산소와 반응하여 연소가 일어나며, 연소반응은 전구름크기에 대해 폭발반응으로 진행된다.The combustible fuel 5 is dispersed and at the same time combustion occurs by reacting with oxygen in the air by using the energy of the dispersion-ignition charge 4, and the combustion reaction proceeds as an explosion reaction with respect to the bulb size.
연료(5)는 기폭되어 강력한 압력과 열을 생성한다.Fuel 5 is detonated to produce strong pressure and heat.
본 발명에 의한 개량형 FAE탄은 이렇게 생성된 압력에 의한 충격파(폭풍파)와 열(온도)에 의한 소이효과 및 부차적으로 탄두 파열로 인한 파편효과를 이용하여 표적을 파괴하게 되는 것이다.The improved FAE bullet according to the present invention is to destroy the target by using the shock effect (shock wave) and heat (temperature) caused by the pressure generated in this way and the debris effect due to the warhead rupture.
본 발명에 의한 FAE탄은 2차 기폭장치를 사용하고 있지 않으므로 구조가 간단해서 제조비용이 저렴할 뿐만 아니라 폭발계열이 단일화 되어 있기 때문에 작동신뢰성이 매우 높다.The FAE bomb according to the present invention does not use a secondary detonator, so the structure is simple and the manufacturing cost is low, and since the explosion series is unified, the operation reliability is very high.
아울러 본 발명에 의한 FAE탄은 슬러리형태의 연료를 사용하고 있기 때문에 액상연료를 사용한 FAE탄의 장점과 고체연료를 사용한 FAE탄의 장점을 모두 발휘 할 수 있으며 항공기 투하탄 이외의 무기체계, 즉 유탄, 로켓탄, 유도탄, 포탄 또는 폭파용키트에 두루 활용 할 수 있다.In addition, since the FAE coal according to the present invention uses fuel in the form of slurry, it can exhibit both the advantages of FAE coal using liquid fuel and FAE coal using solid fuel. It can be used throughout rockets, guided missiles, shells or blasting kits.
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR10-2001-0072834A KR100469135B1 (en) | 2001-11-22 | 2001-11-22 | Fuel Air Explosive Munition |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR10-2001-0072834A KR100469135B1 (en) | 2001-11-22 | 2001-11-22 | Fuel Air Explosive Munition |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| KR20030042184A true KR20030042184A (en) | 2003-05-28 |
| KR100469135B1 KR100469135B1 (en) | 2005-02-02 |
Family
ID=29570745
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| KR10-2001-0072834A KR100469135B1 (en) | 2001-11-22 | 2001-11-22 | Fuel Air Explosive Munition |
Country Status (1)
| Country | Link |
|---|---|
| KR (1) | KR100469135B1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101371389B1 (en) * | 2012-04-20 | 2014-03-10 | 국방과학연구소 | Bright Flash Device driven by Explosives of Directional type |
| CN104390526A (en) * | 2014-09-22 | 2015-03-04 | 西安近代化学研究所 | Fire channeling prevention device for fuel air explosive warhead |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4074628A (en) * | 1966-06-21 | 1978-02-21 | The United States Of America As Represented By The Secretary Of The Navy | Fax canister with a bottom burster charge and dispersion control ring |
| US4157928A (en) * | 1973-03-01 | 1979-06-12 | The United States Of America As Represented By The Secretary Of The Navy | Method for fuel air explosive |
| US4585495A (en) * | 1985-03-11 | 1986-04-29 | Du Pont Of Canada, Inc. | Stable nitrate/slurry explosives |
| CA1311391C (en) * | 1988-09-23 | 1992-12-15 | Stephen B. Murray | Fuel-air line-charge ordnance neutralizer |
| US5686691A (en) * | 1995-12-22 | 1997-11-11 | Oea, Inc. | Slurry-loadable electrical initiator |
-
2001
- 2001-11-22 KR KR10-2001-0072834A patent/KR100469135B1/en active IP Right Grant
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101371389B1 (en) * | 2012-04-20 | 2014-03-10 | 국방과학연구소 | Bright Flash Device driven by Explosives of Directional type |
| CN104390526A (en) * | 2014-09-22 | 2015-03-04 | 西安近代化学研究所 | Fire channeling prevention device for fuel air explosive warhead |
| CN104390526B (en) * | 2014-09-22 | 2015-12-09 | 西安近代化学研究所 | The anti-fiery device of leaping up of a kind of Yun Bao warhead |
Also Published As
| Publication number | Publication date |
|---|---|
| KR100469135B1 (en) | 2005-02-02 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8931415B2 (en) | Initiation systems for explosive devices, scalable output explosive devices including initiation systems, and related methods | |
| EP1272808B1 (en) | Projectile for the destruction of large explosive targets | |
| US2884859A (en) | Rocket projectile | |
| EP2203708B1 (en) | Method of varying firing range and effect in target for shell and shell configured for this purpose | |
| US3771451A (en) | Low pressure ballistic system | |
| US3620162A (en) | Rifle launched rocket | |
| US2681619A (en) | Rocket projectile | |
| KR101987170B1 (en) | Ramjet Solid Fuel with Ignition Support for Gun-Propelled Ramjet Shell | |
| UA126700C2 (en) | Projectile having a pyrotechnic explosive charge | |
| KR100469135B1 (en) | Fuel Air Explosive Munition | |
| EP0084095B1 (en) | Ballistic propulsion system for rifle grenades and similar projectiles | |
| US10502537B1 (en) | Enhanced terminal performance medium caliber multipurpose traced self-destruct projectile | |
| RU219887U1 (en) | AMMUNITION WITH VOLUMETRIC-DETONATING MIXTURE | |
| KR101302059B1 (en) | Design method of thermobaric warhead available in guided weapon using jet fuel remained in the fuel tank | |
| RU2810104C2 (en) | Method of throwing object, ammunition and launching device for its implementation | |
| KR100469136B1 (en) | Detonating Process for Fuel Air Explosive Munition | |
| US10969212B1 (en) | Multipurpose munition for personnel and materiel defeat | |
| KR102063848B1 (en) | Cartridge case with double cartridge chamber and ammunition comprising the same | |
| RU2203473C2 (en) | Rocket launcher round | |
| US2926608A (en) | Rocket projectile construction | |
| Hazell | Propellants and Explosives | |
| US3425352A (en) | Projectile fuze capable of self-destruction | |
| BG67497B1 (en) | 60 mm FRAGMENTATION PROJECTILE | |
| RU1840811C (en) | Solid propellant rocket engine | |
| CN116608744A (en) | Single-soldier rocket projectile bottom fuze release safety ignition unidirectional partition igniter |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A201 | Request for examination | ||
| E902 | Notification of reason for refusal | ||
| E902 | Notification of reason for refusal | ||
| E701 | Decision to grant or registration of patent right | ||
| GRNT | Written decision to grant | ||
| FPAY | Annual fee payment |
Payment date: 20130121 Year of fee payment: 9 |
|
| FPAY | Annual fee payment |
Payment date: 20140121 Year of fee payment: 10 |
|
| FPAY | Annual fee payment |
Payment date: 20150121 Year of fee payment: 11 |
|
| FPAY | Annual fee payment |
Payment date: 20160121 Year of fee payment: 12 |
|
| FPAY | Annual fee payment |
Payment date: 20170123 Year of fee payment: 13 |
|
| FPAY | Annual fee payment |
Payment date: 20180122 Year of fee payment: 14 |
|
| FPAY | Annual fee payment |
Payment date: 20190121 Year of fee payment: 15 |
|
| FPAY | Annual fee payment |
Payment date: 20200121 Year of fee payment: 16 |