US3601054A - Method and apparatus for electromagnetically initiating ordnance - Google Patents

Method and apparatus for electromagnetically initiating ordnance Download PDF

Info

Publication number
US3601054A
US3601054A US807727A US3601054DA US3601054A US 3601054 A US3601054 A US 3601054A US 807727 A US807727 A US 807727A US 3601054D A US3601054D A US 3601054DA US 3601054 A US3601054 A US 3601054A
Authority
US
United States
Prior art keywords
cluster
conductors
pyroignition
electromagnetic energy
initiating
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.)
Expired - Lifetime
Application number
US807727A
Inventor
William O Christianson
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.)
Unidynamics Phoenix Inc
Original Assignee
Unidynamics Phoenix 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 Unidynamics Phoenix Inc filed Critical Unidynamics Phoenix Inc
Application granted granted Critical
Publication of US3601054A publication Critical patent/US3601054A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B5/00Cartridge ammunition, e.g. separately-loaded propellant charges
    • F42B5/02Cartridges, i.e. cases with charge and missile
    • F42B5/08Cartridges, i.e. cases with charge and missile modified for electric ignition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41AFUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
    • F41A19/00Firing or trigger mechanisms; Cocking mechanisms
    • F41A19/58Electric firing mechanisms
    • F41A19/63Electric firing mechanisms having means for contactless transmission of electric energy, e.g. by induction, by sparking gap
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C19/00Details of fuzes
    • F42C19/08Primers; Detonators
    • F42C19/12Primers; Detonators electric

Definitions

  • the devices presently used for initiating the ammunition of the larger ordnance pieces may be classified broadly as either firing pins or electrical probes. Firing pins and electrical probes, however, continue to display a disturbing tendency to fail. In particular, when used with caseless ammunition, firing pins and electrical probes have been observed to be subject to severe and rapid deterioration such that failure occurs at a rate intolerable in modern warfare.
  • a cluster of conductors each cut to a predetermined length, within a mass of pyroignition material and subjecting the cluster of conductors to'electromagnetic energy preferably at the frequency at which the individual conductors are one-half wavelength.
  • the high current coupled into the conductors quickly heat them into an incandescent state to initiate the pyroignition material surrounding them.
  • FIG. 1 is a schematic representation of the firing system
  • FIG. 2 is a cross-sectional detail of the ignitor.
  • an ammunition round including propellant l packed within a case 2 is shown in cross section as disposed within a barrel 3.
  • the illustration of cased ammu nition is merely exemplary, and it will be understood that the invention is equally applicable to ordnance pieces using caseless ammunition.
  • An ignitor 4 is contained within a coaxial recess in the base of the case 2.
  • the power supply 6 may be automatically or manually energized and deenergized by any convenient means suitable to the particular operating environment as represented by the block labeled initiation command in FIG. 1.
  • Electromagnetic energy generated when the power oscillator is in operation, is coupled through a conventional wave guide 8 to an antenna horn disposed within the ordnance piece as represented in H0. 1.
  • the antenna horn 9 directs the electromagnetic energy, through an electromagnetic window" 10, into the ignitor 4.
  • FIG. 2 The construction of the ignitor 4 is shown more clearly in FIG. 2.
  • a mass of pyroignition material 10 is packed within an inner casing 11 and an outer case comprising a cap 12 and a cover 13.
  • the cover 13 must pass electromagnetic energy without significant attenuation and, therefore, should, like the window 10 of FIG. 1, be composed of any one of the wellknown materials possessing'the requisite properties.
  • a cluster of conductor sections 14 is generally centrally disposed within the pyroignition material 10 as best shown in FIG. 2.
  • the cluster comprises a plurality of metallic wires, for example, aluminum or pyrofuse wires, cut to substantially the same predetermined length. Their function will be described below. It may also be observed at this oint that the upper portlon 15 of t e inner casing 11 is para olic and consists of a material, such as carbon or metal, which efficiently reflects electromagnetic waves.
  • the initiation command device 7 is activated to energize the power supply 6 thereby bringing the power oscillator 5 into operation.
  • Electromagnetic energy from the power oscillator 5 is coupled through the wave guide 8 to the antenna horn 9 from which it is directed through the window 10 and the cover 13 to the ignitor.
  • the electromagnetic energy passes through the pyroignition material 10 and is reflected from the parabolic surface 15 of the inner casing 11 to focus on the conductor cluster 14.
  • the resulting currents developed in the individual conductors of the cluster quickly heat them into an incandescent state to initiate the pyroignition material 10 which, in turn, initiates the propellant.
  • the conductive wire cluster 14 will be centered at the focus of the parabolic reflector 15. Further, each of the conductors in the cluster 14 will have been cut to a length which is nominally one-half wavelength at the frequency of the electromagnetic energy directed at the cluster. For example, for a frequency of 13 gigaI-Iertz, this length is approximately 0.5 inch. Adjustment of the sensitivity of the conductor cluster can be changed by varying the wire diameter and/or the material. The dimensions of the parabolic reflector 15, the antenna horn 9,
  • Apparatus for igniting pyroignition material comprising:
  • said electrical conductors are of predetermined substantially equal lengths
  • said electromagnetic energy has a frequency such that the predetermined lengths of said conductors is substantially one-half wavelength.
  • the apparatus of claim 1 which further includes means for selectively activating said course of electromagnetic ener- 3.
  • the apparatus of claim 2 in which the pyroignition material is contained within a housing, said housing including a first side composed of a material exhibiting the properties of an electromagnetic window.
  • said housing further includes a second side disposed opposite said first side, said second side comprising a paraboloid of electromagnetically reflective material whereby the electromagnetic energy is focused on said cluster of conductors.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Constitution Of High-Frequency Heating (AREA)

Abstract

In order to obviate the necessity for using firing pins or electrical probes for initiating ammunition, a cluster of conductors are enclosed within a mass of pyroignition material, and means are provided to subject the cluster of conductors to control electromagnetic radiation such that they are heated into an incandescent state to ignite the pyroignition material.

Description

United States Patent inventor William 0. Christianson [56] References Cited Lllchfield Park, UNITED STATES PATENTS P 969 2,459,854 1/1949 Swift, Jr 89/37 x Flled d r 2,640,417 6/1953 Bjork et al. 1 102/46 x V: hoe 3,177,651 4/1965 Lawrence... 102/702 ux Assignee 1; yu l? 3,351,016 11/1967 Simpson 102/702 6 3,362,329 1/1968 Epstein 102/702 Primary Examiner-Robert F. Stahl METHOD AND APPARATUS FOR Attorney-Drummond, Cahill & Phillips ELECTROMAGNETICALLY INITIATING gmwing ABSTRACT: In order to obviate the necessity for using firing pins or electrical probes for initiating ammunition, a cluster of [1.8. CI 102/46, conductors are enclosed within a mass of pyroignition materi- 89/28, 102/702 R al, and means are provided to subject the cluster of conduc- Int. Cl F42b 9/08 tors to control electromagnetic radiation such that they are Field of Search 89/135, 28; heated into an incandescent state to ignite the pyroignition 42/84; 102/46, 70.2 material.
Patented Aug. 24, 1971 350L054 BE- E INITIATION COMMAND POWER l POWER SUPPLY (MODULATOR) OSC'LLATQR INVENTOR. WILLIA M O. CHRISTIANSON ATTORNEYS METHOD AND APPARATUS FOR ELECTROMAGNETICALLY INITIATING ORDNANCE This invention relates to ordnance and, more particularly, to a method and apparatus for initiating ammunition and the like.
The devices presently used for initiating the ammunition of the larger ordnance pieces may be classified broadly as either firing pins or electrical probes. Firing pins and electrical probes, however, continue to display a disturbing tendency to fail. In particular, when used with caseless ammunition, firing pins and electrical probes have been observed to be subject to severe and rapid deterioration such that failure occurs at a rate intolerable in modern warfare.
It is a general object of this invention to provide means for reliably initiating ammunition.
It is a further object of this invention to provide such means without the use offiring pins or electrical probes.
It is a more specific object of this invention to provide initiating means utilizing controlled electromagnetic radiation to heat a cluster of conductors to incandescence.
These and other objects are achieved, according to one aspect of the invention, by disposing a cluster of conductors, each cut to a predetermined length, within a mass of pyroignition material and subjecting the cluster of conductors to'electromagnetic energy preferably at the frequency at which the individual conductors are one-half wavelength. The high current coupled into the conductors quickly heat them into an incandescent state to initiate the pyroignition material surrounding them.
The subject matter of the invention is particularly pointed out and distinctly claimed in the concluding portion of the specification. The invention, however, both as to organization and method of operation, may best be understood by reference to the following description taken in connection with the accompanying drawings of which:
FIG. 1 is a schematic representation of the firing system; and
FIG. 2 is a cross-sectional detail of the ignitor.
Referring now to FIG. 1, an ammunition round including propellant l packed within a case 2 is shown in cross section as disposed within a barrel 3. The illustration of cased ammu nition is merely exemplary, and it will be understood that the invention is equally applicable to ordnance pieces using caseless ammunition. An ignitor 4 is contained within a coaxial recess in the base of the case 2.
A power oscillator 5, such as a klystron, magnetron or the like, is modulated by selectively energizing its power supply 6 in the manner well known in the radar and high frequency engineering arts. The power supply 6 may be automatically or manually energized and deenergized by any convenient means suitable to the particular operating environment as represented by the block labeled initiation command in FIG. 1.
Electromagnetic energy, generated when the power oscillator is in operation, is coupled through a conventional wave guide 8 to an antenna horn disposed within the ordnance piece as represented in H0. 1. Thus, the antenna horn 9 directs the electromagnetic energy, through an electromagnetic window" 10, into the ignitor 4.
The construction of the ignitor 4 is shown more clearly in FIG. 2. A mass of pyroignition material 10 is packed within an inner casing 11 and an outer case comprising a cap 12 and a cover 13. The cover 13 must pass electromagnetic energy without significant attenuation and, therefore, should, like the window 10 of FIG. 1, be composed of any one of the wellknown materials possessing'the requisite properties.
A cluster of conductor sections 14 is generally centrally disposed within the pyroignition material 10 as best shown in FIG. 2. Typically, the cluster comprises a plurality of metallic wires, for example, aluminum or pyrofuse wires, cut to substantially the same predetermined length. Their function will be described below. It may also be observed at this oint that the upper portlon 15 of t e inner casing 11 is para olic and consists of a material, such as carbon or metal, which efficiently reflects electromagnetic waves.
Referring again to FIG. 1, as well as FIG. 2, to initiate the pyroignition material 10, the initiation command device 7 is activated to energize the power supply 6 thereby bringing the power oscillator 5 into operation. Electromagnetic energy from the power oscillator 5 is coupled through the wave guide 8 to the antenna horn 9 from which it is directed through the window 10 and the cover 13 to the ignitor. The electromagnetic energy passes through the pyroignition material 10 and is reflected from the parabolic surface 15 of the inner casing 11 to focus on the conductor cluster 14. The resulting currents developed in the individual conductors of the cluster quickly heat them into an incandescent state to initiate the pyroignition material 10 which, in turn, initiates the propellant.
For maximum efiiciency, it will be understood that the conductive wire cluster 14 will be centered at the focus of the parabolic reflector 15. Further, each of the conductors in the cluster 14 will have been cut to a length which is nominally one-half wavelength at the frequency of the electromagnetic energy directed at the cluster. For example, for a frequency of 13 gigaI-Iertz, this length is approximately 0.5 inch. Adjustment of the sensitivity of the conductor cluster can be changed by varying the wire diameter and/or the material. The dimensions of the parabolic reflector 15, the antenna horn 9,
etc., may also depend upon the frequency, but these are matters well known in the radar engineering art and need not be treated at length here.
While the principals of the invention have now been made clear in an illustrative embodiment, there will be immediately obvious to those skilled in the art many modifications of structure, arrangement, proportions, the elements, materials, and components used in the practice of the invention which are particularly adapted for specific environments and operating requirements without departing from those principals.
I claim:
1. Apparatus for igniting pyroignition material comprising:
A. a cluster of electrical conductors disposed in heat-conducting relationship with the pyroignition material;
B. a source of electromagnetic energy;
C. means for exposing said cluster of conductors to said electromagnetic energy;
D. said electrical conductors are of predetermined substantially equal lengths; and
E. said electromagnetic energy has a frequency such that the predetermined lengths of said conductors is substantially one-half wavelength.
2. The apparatus of claim 1 which further includes means for selectively activating said course of electromagnetic ener- 3. The apparatus of claim 2 in which the pyroignition material is contained within a housing, said housing including a first side composed of a material exhibiting the properties of an electromagnetic window.
4. The apparatus of claim 3 in which said housing further includes a second side disposed opposite said first side, said second side comprising a paraboloid of electromagnetically reflective material whereby the electromagnetic energy is focused on said cluster of conductors.

Claims (4)

1. Apparatus for igniting pyroignition material comprising: A. a cluster of electrical conductors disposed in heatconducting relationship with the pyroignition material; B. a source of electromagnetic energy; C. means for exposing said cluster of conductors to said electromagnetic energy; D. said electrical conductors are of predetermined substantially equal lengths; and E. said electromagnetic energy has a frequency such that the predetermined lengths of said conductors is substantially onehalf wavelength.
2. The apparatus of claim 1 which further includes means for selectively activating said course of electromagnetic energy.
3. The apparatus of claim 2 in which the pyroignition material is contained within a housing, said housing including a first side composed of a material exhibiting the properties of an electromAgnetic window.
4. The apparatus of claim 3 in which said housing further includes a second side disposed opposite said first side, said second side comprising a paraboloid of electromagnetically reflective material whereby the electromagnetic energy is focused on said cluster of conductors.
US807727A 1969-03-17 1969-03-17 Method and apparatus for electromagnetically initiating ordnance Expired - Lifetime US3601054A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US80772769A 1969-03-17 1969-03-17

Publications (1)

Publication Number Publication Date
US3601054A true US3601054A (en) 1971-08-24

Family

ID=25197061

Family Applications (1)

Application Number Title Priority Date Filing Date
US807727A Expired - Lifetime US3601054A (en) 1969-03-17 1969-03-17 Method and apparatus for electromagnetically initiating ordnance

Country Status (1)

Country Link
US (1) US3601054A (en)

Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2255140A1 (en) * 1971-11-12 1973-05-24 France Etat IGNITION DEVICE WITH ELECTRIC RELEASE
FR2631436A1 (en) * 1988-05-13 1989-11-17 Tzn Forschung & Entwicklung CARTRIDGE FOR ELECTROTHERMIC LAUNCH DEVICES
WO1993005356A1 (en) * 1989-04-18 1993-03-18 Royal Ordnance Plc The initiation of propellants
FR2702832A1 (en) * 1993-03-16 1994-09-23 Lacroix E Tous Artifices Attenuated risk pyrotechnic composition initiation device.
US5668342A (en) * 1995-12-07 1997-09-16 Discher; Stephen R. W. Apparatus and method for detection and neutralization of concealed explosives
WO1998036235A1 (en) * 1997-02-14 1998-08-20 Easat Antennas Ltd. Method and apparatus for the remote clearance of explosive devices
GB2336341A (en) * 1997-02-14 1999-10-20 Easat Antennas Ltd Method and apparatus for the remote clearance of explosive devices
US6152039A (en) * 1991-09-04 2000-11-28 Royal Ordnance Plc Initiation of propellants
EP1067354A1 (en) * 1999-07-07 2001-01-10 Giat Industries Initiating device for an explosive charge
WO2001027553A1 (en) * 1999-10-14 2001-04-19 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Propellant device for pipe weapons or ballistic projection
EP1334327A2 (en) * 2000-09-28 2003-08-13 Superior Ballistics, Inc. Firearm cartridge and case-less chamber
WO2005043069A1 (en) * 2003-10-30 2005-05-12 Gamma Kdg Systems Sa Emp firing mechanism for large caliber firearms and artillery
US20070214950A1 (en) * 2006-03-20 2007-09-20 Technology Patents, Llc Anti-terrorist system
US20080028921A1 (en) * 2006-08-02 2008-02-07 Peter Victor Bitar System for neutralizing explosive and electronic devices
DE102009006079A1 (en) 2009-01-26 2010-07-29 Oao Znjj "Burevestnik" Shot load igniting device for use in projectile chamber of artillery system, has coaxial apparatus whose part is provided at sides of chamber, and transmission source provided in frequency region, where chamber forms vertical shaft
US7775146B1 (en) 2006-08-02 2010-08-17 Xtreme Ads Limited System and method for neutralizing explosives and electronics
US8683907B1 (en) 2011-09-07 2014-04-01 Xtreme Ads Limited Electrical discharge system and method for neutralizing explosive devices and electronics
US9097503B1 (en) * 2012-12-20 2015-08-04 Los Alamos National Security, Llc Munitions having an insensitive detonator system for initiating large failure diameter explosives
RU2571459C1 (en) * 2014-11-21 2015-12-20 Михаил Иосифович Фильковский Device for propelling charge ignition
US9243874B1 (en) 2011-09-07 2016-01-26 Xtreme Ads Limited Electrical discharge system and method for neutralizing explosive devices and electronics
US10107607B1 (en) * 2017-04-04 2018-10-23 The United States Of America As Represented By The Secretary Of The Army Radio frequency igniter
US10641572B1 (en) * 2016-04-19 2020-05-05 Triad National Security, Llc Microwave ignition of energetic material housed within a gun
US10969206B1 (en) * 2018-11-29 2021-04-06 U.S. Government As Represented By The Secretary Of The Army Radio frequency antenna for use in the confines of a breech
RU2750173C1 (en) * 2020-10-20 2021-06-22 Акционерное общество "Научно-технический центр ЭЛИНС" Receiving device for initiator of a modular propellant charge with contactless ignition
RU2750196C1 (en) * 2020-11-27 2021-06-23 Акционерное общество "Научно-технический центр ЭЛИНС" Receiving device for initiator of a modular propellant charge with non-contact ignition
US11585622B1 (en) 2016-04-19 2023-02-21 Triad National Security, Llc Microwave ignition systems with launcher affixed to or located within a gun spindle

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2459854A (en) * 1946-04-18 1949-01-25 Jr Willard E Swift Grenade projector
US2640417A (en) * 1946-12-18 1953-06-02 Us Sec War Ignition safety device for induction fired rockets
US3177651A (en) * 1962-01-18 1965-04-13 United Aircraft Corp Laser ignition
US3351016A (en) * 1965-12-10 1967-11-07 Universal Match Corp Explosive arming and firing system
US3362329A (en) * 1963-12-10 1968-01-09 Epstein Sidney Electro-explosive devices

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2459854A (en) * 1946-04-18 1949-01-25 Jr Willard E Swift Grenade projector
US2640417A (en) * 1946-12-18 1953-06-02 Us Sec War Ignition safety device for induction fired rockets
US3177651A (en) * 1962-01-18 1965-04-13 United Aircraft Corp Laser ignition
US3362329A (en) * 1963-12-10 1968-01-09 Epstein Sidney Electro-explosive devices
US3351016A (en) * 1965-12-10 1967-11-07 Universal Match Corp Explosive arming and firing system

Cited By (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2255140A1 (en) * 1971-11-12 1973-05-24 France Etat IGNITION DEVICE WITH ELECTRIC RELEASE
FR2631436A1 (en) * 1988-05-13 1989-11-17 Tzn Forschung & Entwicklung CARTRIDGE FOR ELECTROTHERMIC LAUNCH DEVICES
WO1993005356A1 (en) * 1989-04-18 1993-03-18 Royal Ordnance Plc The initiation of propellants
US6152039A (en) * 1991-09-04 2000-11-28 Royal Ordnance Plc Initiation of propellants
WO1994021980A1 (en) * 1993-03-16 1994-09-29 Etienne Lacroix Tous Artifices S.A. Firing a composition with a microwave generator________________
FR2702832A1 (en) * 1993-03-16 1994-09-23 Lacroix E Tous Artifices Attenuated risk pyrotechnic composition initiation device.
US5668342A (en) * 1995-12-07 1997-09-16 Discher; Stephen R. W. Apparatus and method for detection and neutralization of concealed explosives
WO1998036235A1 (en) * 1997-02-14 1998-08-20 Easat Antennas Ltd. Method and apparatus for the remote clearance of explosive devices
GB2336341A (en) * 1997-02-14 1999-10-20 Easat Antennas Ltd Method and apparatus for the remote clearance of explosive devices
EP1067354A1 (en) * 1999-07-07 2001-01-10 Giat Industries Initiating device for an explosive charge
FR2796141A1 (en) * 1999-07-07 2001-01-12 Giat Ind Sa DEVICE FOR INITIATING AN ENERGY COMPOSITION
WO2001027553A1 (en) * 1999-10-14 2001-04-19 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Propellant device for pipe weapons or ballistic projection
US6591753B1 (en) 1999-10-14 2003-07-15 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Propellant device for pipe weapons or ballistic projection
EP1334327A2 (en) * 2000-09-28 2003-08-13 Superior Ballistics, Inc. Firearm cartridge and case-less chamber
EP1334327A4 (en) * 2000-09-28 2006-08-23 Superior Ballistics Inc Firearm cartridge and case-less chamber
WO2005043069A1 (en) * 2003-10-30 2005-05-12 Gamma Kdg Systems Sa Emp firing mechanism for large caliber firearms and artillery
US20070214950A1 (en) * 2006-03-20 2007-09-20 Technology Patents, Llc Anti-terrorist system
US8250961B2 (en) 2006-03-20 2012-08-28 Technology Patents, Llc Anti-terrorist system
US7784389B2 (en) * 2006-03-20 2010-08-31 Technology Patents, Llc Anti-terrorist system
US7775146B1 (en) 2006-08-02 2010-08-17 Xtreme Ads Limited System and method for neutralizing explosives and electronics
US8561515B1 (en) 2006-08-02 2013-10-22 Xtreme Ads Limited Method for neutralizing explosives and electronics
US7775145B2 (en) 2006-08-02 2010-08-17 Xtreme Ads Limited System for neutralizing explosive and electronic devices
US8887611B2 (en) 2006-08-02 2014-11-18 Xtreme Ads Limited Method for neutralizing explosives and electronics
US20110120290A1 (en) * 2006-08-02 2011-05-26 Peter Victor Bitar Method for neutralizing explosives and electronics
US7958809B1 (en) 2006-08-02 2011-06-14 Xtreme Ads Limited Method for neutralizing explosives and electronics
US20080028921A1 (en) * 2006-08-02 2008-02-07 Peter Victor Bitar System for neutralizing explosive and electronic devices
DE202009014949U1 (en) 2009-01-26 2010-10-07 Oao Znjj "Burevestnik" Device for the ignition of the charge in the projectile chamber of a shellless artillery system
DE102009006079A1 (en) 2009-01-26 2010-07-29 Oao Znjj "Burevestnik" Shot load igniting device for use in projectile chamber of artillery system, has coaxial apparatus whose part is provided at sides of chamber, and transmission source provided in frequency region, where chamber forms vertical shaft
US10247525B2 (en) 2011-09-07 2019-04-02 Xtreme Ads Limited Electrical discharge system and method for neutralizing explosive devices and electronics
US8683907B1 (en) 2011-09-07 2014-04-01 Xtreme Ads Limited Electrical discharge system and method for neutralizing explosive devices and electronics
US9243874B1 (en) 2011-09-07 2016-01-26 Xtreme Ads Limited Electrical discharge system and method for neutralizing explosive devices and electronics
US9739573B2 (en) 2011-09-07 2017-08-22 Xtreme Ads Limited Electrical discharge system and method for neutralizing explosive devices and electronics
US9097503B1 (en) * 2012-12-20 2015-08-04 Los Alamos National Security, Llc Munitions having an insensitive detonator system for initiating large failure diameter explosives
RU2571459C1 (en) * 2014-11-21 2015-12-20 Михаил Иосифович Фильковский Device for propelling charge ignition
US10641572B1 (en) * 2016-04-19 2020-05-05 Triad National Security, Llc Microwave ignition of energetic material housed within a gun
US11585622B1 (en) 2016-04-19 2023-02-21 Triad National Security, Llc Microwave ignition systems with launcher affixed to or located within a gun spindle
US10107607B1 (en) * 2017-04-04 2018-10-23 The United States Of America As Represented By The Secretary Of The Army Radio frequency igniter
US10859358B1 (en) * 2017-04-04 2020-12-08 The United States Of America As Represented By The Secretary Of The Army Radio frequency igniter
US10969206B1 (en) * 2018-11-29 2021-04-06 U.S. Government As Represented By The Secretary Of The Army Radio frequency antenna for use in the confines of a breech
RU2750173C1 (en) * 2020-10-20 2021-06-22 Акционерное общество "Научно-технический центр ЭЛИНС" Receiving device for initiator of a modular propellant charge with contactless ignition
RU2750196C1 (en) * 2020-11-27 2021-06-23 Акционерное общество "Научно-технический центр ЭЛИНС" Receiving device for initiator of a modular propellant charge with non-contact ignition

Similar Documents

Publication Publication Date Title
US3601054A (en) Method and apparatus for electromagnetically initiating ordnance
US3408937A (en) Light energized explosive device
US2137598A (en) Artillery projectile
US3618526A (en) Pyrotechnic pumped laser for remote ordnance initiation system
US2926566A (en) Device for accelerating the ignition of the propellant for a projectile
US3362329A (en) Electro-explosive devices
US3177651A (en) Laser ignition
US3640224A (en) Rf immune firing circuit employing high-impedance leads
US3546623A (en) Apparatus for separating light energy from shock wave energy including the pumping of a laser with an exploding wire
US3809964A (en) Electrically actuated priming device
DE19744794A1 (en) Plastics anti-personnel mine clearance method
US3398322A (en) High voltage switch
US9273942B1 (en) Disposable, miniature internal optical ignition source for ammunition application
US3275829A (en) Cavity radiator with a pyrotechnic charge that remains intact during and after combustion
US3946675A (en) Power-generating device for a projectile, shell, etc.
US3351016A (en) Explosive arming and firing system
US3167015A (en) Flash lamp ignited rocket
US5088411A (en) Apparatus for igniting detonating primer with the aid of electromagnetic wave
US5052011A (en) Explosively pumped laser light
US3659527A (en) High temperature detonator
US3451008A (en) Shock wave optically pumped laser
US3039363A (en) Rocket firing relay
US3148619A (en) High frequency immune squib
US3518943A (en) Stable electrically ignitable explosive charges
Menichelli et al. Sensitivity of explosives to laser energy