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EP0790476A3 - Selfpropelled missile - Google Patents

Selfpropelled missile Download PDF

Info

Publication number
EP0790476A3
EP0790476A3 EP97101942A EP97101942A EP0790476A3 EP 0790476 A3 EP0790476 A3 EP 0790476A3 EP 97101942 A EP97101942 A EP 97101942A EP 97101942 A EP97101942 A EP 97101942A EP 0790476 A3 EP0790476 A3 EP 0790476A3
Authority
EP
European Patent Office
Prior art keywords
selfpropelled
missile
selfpropelled missile
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Withdrawn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
EP97101942A
Other languages
German (de)
French (fr)
Other versions
EP0790476A2 (en
Inventor
Rainer Schöffl
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.)
Dynamit Nobel AG
Dynamit Nobel GmbH Explosivstoff und Systemtechnik
Original Assignee
Dynamit Nobel AG
Dynamit Nobel GmbH Explosivstoff und Systemtechnik
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 Dynamit Nobel AG, Dynamit Nobel GmbH Explosivstoff und Systemtechnik filed Critical Dynamit Nobel AG
Publication of EP0790476A2 publication Critical patent/EP0790476A2/en
Publication of EP0790476A3 publication Critical patent/EP0790476A3/en
Withdrawn legal-status Critical Current

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
    • F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
    • F42B12/201—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class
    • F42B12/204—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class for attacking structures, e.g. specific buildings or fortifications, ships or vehicles
    • 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
    • F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
    • F42B12/208—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by a plurality of charges within a single high explosive warhead
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B19/00—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
    • F42B19/12—Propulsion specially adapted for torpedoes
    • F42B19/26—Propulsion specially adapted for torpedoes by jet propulsion

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
EP97101942A 1996-02-15 1997-02-07 Selfpropelled missile Withdrawn EP0790476A3 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE1996105613 DE19605613A1 (en) 1996-02-15 1996-02-15 Missile-powered ranged weapon
DE19605613 1996-02-15

Publications (2)

Publication Number Publication Date
EP0790476A2 EP0790476A2 (en) 1997-08-20
EP0790476A3 true EP0790476A3 (en) 1997-12-29

Family

ID=7785492

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97101942A Withdrawn EP0790476A3 (en) 1996-02-15 1997-02-07 Selfpropelled missile

Country Status (2)

Country Link
EP (1) EP0790476A3 (en)
DE (1) DE19605613A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2125228C1 (en) * 1997-08-14 1999-01-20 Конструкторское бюро приборостроения Shell
RU2260769C1 (en) * 2004-03-19 2005-09-20 Дочернее открытое акционерное общество "Научно-производственный центр высокоточной техники "Ижмаш" Guided artillery projectile
SE531815C2 (en) 2007-10-19 2009-08-11 Bae Systems Bofors Ab Ways to vary the firing range and impact in grenade and grenade targets designed accordingly

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3804683A (en) * 1970-01-07 1974-04-16 Us Army High energy, low burning rate solid propellant compositions based on acrylic prepolymer binders
DE2307581A1 (en) * 1973-02-16 1974-08-29 Messerschmitt Boelkow Blohm MISSILE AMMUNITION
US3954531A (en) * 1973-06-14 1976-05-04 The United States Of America As Represented By The Secretary Of The Navy Composite double base propellant composition containing ferric fluoride
US3995549A (en) * 1975-03-17 1976-12-07 The United States Of America As Represented By The Secretary Of The Navy Rocket/missile motor explosive insert detonator
US4086110A (en) * 1976-11-22 1978-04-25 Thiokol Corporation Propellant made with cocrystals of cyclotetramethylenetetranitramine and ammonium perchlorate
FR2385075A1 (en) * 1977-03-23 1978-10-20 Haut Rhin Manufacture Machines Charge scattering rocket propulsion system - has igniter charge to actuate excess of propulsive charge to destroy remaining parts
FR2385074A1 (en) * 1977-03-23 1978-10-20 Haut Rhin Manufacture Machines Anti-personnel rocket multiple explosive charge - has propulsive charge, scatter charge with detonator and impact charge with detonator
US4197800A (en) * 1970-09-04 1980-04-15 Hercules Incorporated Single chamber rap having centerport inhibitor
JPS565395A (en) * 1979-06-21 1981-01-20 Boeicho Gijutsu Kenkyu Honbuch Solid propellant composition
JPS5864297A (en) * 1981-10-09 1983-04-16 日産自動車株式会社 Composite propellant
DE3523953A1 (en) * 1985-07-04 1987-01-15 Fraunhofer Ges Forschung METHOD AND DEVICE FOR PRODUCING SOLID FUELS
USH203H (en) * 1985-01-28 1987-02-03 The United States Of America As Represented By The Secretary Of The Army Integral rocket motor-warhead
JPS62216985A (en) * 1986-03-19 1987-09-24 日本油脂株式会社 Nitramine-containing composite solid propellent composition
USH1341H (en) * 1990-12-14 1994-08-02 High energy propellant formulation

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3804683A (en) * 1970-01-07 1974-04-16 Us Army High energy, low burning rate solid propellant compositions based on acrylic prepolymer binders
US4197800A (en) * 1970-09-04 1980-04-15 Hercules Incorporated Single chamber rap having centerport inhibitor
DE2307581A1 (en) * 1973-02-16 1974-08-29 Messerschmitt Boelkow Blohm MISSILE AMMUNITION
US3954531A (en) * 1973-06-14 1976-05-04 The United States Of America As Represented By The Secretary Of The Navy Composite double base propellant composition containing ferric fluoride
US3995549A (en) * 1975-03-17 1976-12-07 The United States Of America As Represented By The Secretary Of The Navy Rocket/missile motor explosive insert detonator
US4086110A (en) * 1976-11-22 1978-04-25 Thiokol Corporation Propellant made with cocrystals of cyclotetramethylenetetranitramine and ammonium perchlorate
FR2385074A1 (en) * 1977-03-23 1978-10-20 Haut Rhin Manufacture Machines Anti-personnel rocket multiple explosive charge - has propulsive charge, scatter charge with detonator and impact charge with detonator
FR2385075A1 (en) * 1977-03-23 1978-10-20 Haut Rhin Manufacture Machines Charge scattering rocket propulsion system - has igniter charge to actuate excess of propulsive charge to destroy remaining parts
JPS565395A (en) * 1979-06-21 1981-01-20 Boeicho Gijutsu Kenkyu Honbuch Solid propellant composition
JPS5864297A (en) * 1981-10-09 1983-04-16 日産自動車株式会社 Composite propellant
USH203H (en) * 1985-01-28 1987-02-03 The United States Of America As Represented By The Secretary Of The Army Integral rocket motor-warhead
DE3523953A1 (en) * 1985-07-04 1987-01-15 Fraunhofer Ges Forschung METHOD AND DEVICE FOR PRODUCING SOLID FUELS
JPS62216985A (en) * 1986-03-19 1987-09-24 日本油脂株式会社 Nitramine-containing composite solid propellent composition
USH1341H (en) * 1990-12-14 1994-08-02 High energy propellant formulation

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
DATABASE WPI Section Ch Week 8111, Derwent World Patents Index; Class A95, AN 81-18457D, XP002041691 *
DATABASE WPI Section Ch Week 8321, Derwent World Patents Index; Class A95, AN 83-50414K, XP002041690 *
DATABASE WPI Section Ch Week 8744, Derwent World Patents Index; Class A12, AN 87-309535, XP002041689 *
T. KUWAHARA: "Combustion of RDX/AP composite propellants at low pressures", JOURNAL OF SPACECRAFT AND ROCKETS, vol. 21, no. 5, 1 September 1984 (1984-09-01), NEW-YORK, XP002041688 *

Also Published As

Publication number Publication date
DE19605613A1 (en) 1997-08-21
EP0790476A2 (en) 1997-08-20

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