FR2537263B2 - Dispositif destine a engendrer un signal d'amorcage pour missile de survol - Google Patents

Dispositif destine a engendrer un signal d'amorcage pour missile de survol

Info

Publication number
FR2537263B2
FR2537263B2 FR8319311A FR8319311A FR2537263B2 FR 2537263 B2 FR2537263 B2 FR 2537263B2 FR 8319311 A FR8319311 A FR 8319311A FR 8319311 A FR8319311 A FR 8319311A FR 2537263 B2 FR2537263 B2 FR 2537263B2
Authority
FR
France
Prior art keywords
generating
priming signal
flying missile
missile
flying
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
FR8319311A
Other languages
English (en)
Other versions
FR2537263A2 (fr
Inventor
Jurgen Schloss
Harald Wich
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.)
Diehl Verwaltungs Stiftung
Original Assignee
Diehl GmbH and Co
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
Priority claimed from DE3122252A external-priority patent/DE3122252C1/de
Priority claimed from DE19823244708 external-priority patent/DE3244708A1/de
Application filed by Diehl GmbH and Co filed Critical Diehl GmbH and Co
Publication of FR2537263A2 publication Critical patent/FR2537263A2/fr
Application granted granted Critical
Publication of FR2537263B2 publication Critical patent/FR2537263B2/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2226—Homing guidance systems comparing the observed data with stored target data, e.g. target configuration data
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/008—Combinations of different guidance systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2246—Active homing systems, i.e. comprising both a transmitter and a receiver
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2253—Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2286—Homing guidance systems characterised by the type of waves using radio waves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G9/00—Systems for controlling missiles or projectiles, not provided for elsewhere
    • F41G9/02—Systems for controlling missiles or projectiles, not provided for elsewhere for bombing control
    • 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
    • F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
    • F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
    • F42B12/14—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge the symmetry axis of the hollow charge forming an angle with the longitudinal axis of the projectile
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C13/00—Proximity fuzes; Fuzes for remote detonation
    • F42C13/02—Proximity fuzes; Fuzes for remote detonation operated by intensity of light or similar radiation
    • F42C13/023—Proximity fuzes; Fuzes for remote detonation operated by intensity of light or similar radiation using active distance measurement

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
FR8319311A 1981-06-04 1983-12-02 Dispositif destine a engendrer un signal d'amorcage pour missile de survol Expired - Lifetime FR2537263B2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3122252A DE3122252C1 (de) 1981-06-04 1981-06-04 Einrichtung zur Erzeugung eines Zuendsignals fuer UEberflug-Flugkoerper
DE19823244708 DE3244708A1 (de) 1982-12-03 1982-12-03 Einrichtung zur erzeugung eines zuendsignals fuer ueberflug-flugkoerper

Publications (2)

Publication Number Publication Date
FR2537263A2 FR2537263A2 (fr) 1984-06-08
FR2537263B2 true FR2537263B2 (fr) 1990-04-27

Family

ID=25793694

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8319311A Expired - Lifetime FR2537263B2 (fr) 1981-06-04 1983-12-02 Dispositif destine a engendrer un signal d'amorcage pour missile de survol

Country Status (1)

Country Link
FR (1) FR2537263B2 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3515496A1 (de) * 1985-04-30 1992-03-26 Diehl Gmbh & Co Hubschrauberabwehr-hohlladungsmine
DE3919573A1 (de) * 1989-06-15 1990-12-20 Diehl Gmbh & Co Verfahren und einrichtung zur akquisition eines zielpunktes
FR2675249A1 (fr) * 1991-04-11 1992-10-16 Telecommunications Sa Procede d'autoguidage d'un engin vers une cible par mesure de distance.
FR2716966B1 (fr) * 1994-03-01 1996-03-29 Thomson Csf Système de défense anti-aérienne à très courte portée, de type missile sol-air.
DE19505791C1 (de) * 1995-02-20 1996-08-14 Daimler Benz Aerospace Ag Verfahren und Vorrichtung zur Bekämpfung verdeckt operierender Hubschrauber

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1207476A (fr) * 1958-06-20 1960-02-17 Trt Telecom Radio Electr Dispositif de mise à feu pour fusée de proximité
DE3000007A1 (de) * 1979-01-02 1980-09-18 Raytheon Co Kampffahrzeug-abwehrsystem
US4193072A (en) * 1962-03-13 1980-03-11 The United States Of America As Represented By The Secretary Of The Navy Combination infrared radio fuze
US3924233A (en) * 1969-04-10 1975-12-02 Us Navy Active-passive target detection system
DE2922583A1 (de) * 1979-06-02 1981-01-22 Messerschmitt Boelkow Blohm Annaeherungszuender fuer panzerbekaempfungsflugkoerper

Also Published As

Publication number Publication date
FR2537263A2 (fr) 1984-06-08

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