SE8306625D0 - FACILITIES FOR THE REMOVAL OF A SUN SIGNAL FOR UEBERFLUG AIRCRAFT - Google Patents

FACILITIES FOR THE REMOVAL OF A SUN SIGNAL FOR UEBERFLUG AIRCRAFT

Info

Publication number
SE8306625D0
SE8306625D0 SE8306625A SE8306625A SE8306625D0 SE 8306625 D0 SE8306625 D0 SE 8306625D0 SE 8306625 A SE8306625 A SE 8306625A SE 8306625 A SE8306625 A SE 8306625A SE 8306625 D0 SE8306625 D0 SE 8306625D0
Authority
SE
Sweden
Prior art keywords
target
flying
orientated
terrain
ignition signal
Prior art date
Application number
SE8306625A
Other languages
Swedish (sv)
Other versions
SE458310B (en
SE8306625L (en
Inventor
J Schloss
H Wich
Original Assignee
Diehl Gmbh & 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
Application filed by Diehl Gmbh & Co filed Critical Diehl Gmbh & Co
Publication of SE8306625D0 publication Critical patent/SE8306625D0/en
Publication of SE8306625L publication Critical patent/SE8306625L/en
Publication of SE458310B publication Critical patent/SE458310B/en

Links

Classifications

    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Optical Radar Systems And Details Thereof (AREA)

Abstract

A device 16 for generating an ignition signal 14 is provided in a flying body 1 for the ejection of a projectile 3 for combatting the target 4 directly overflown, which target is detected at two different angles relative to the flying-body flight direction, in effective directions which differ from one another, by an active sensor 2' and a passive sensor 11' connected to the device 16. The active sensor may be a laser rangefinder and includes a reflection position finder 19 having a strongly bunched characteristic orientated at an angle W1, whilst the passive sensor is orientated more gently ahead or perpendicularly and is equipped with a wide directional characteristic designed to detect magnetic field, heat or sound variations in the terrain 15 in the surroundings of the target 4. An ignition signal 14 is generated when a typical height profile corresponds sufficiently with stored target-specific height information and then after an appropriate flying time span the typical variation in the terrain is ascertained. <IMAGE>
SE8306625A 1982-12-03 1983-12-01 DEVICE FOR GENERATING A FLASH SIGNAL FOR A FLYING FLIGHT BODY SE458310B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19823244708 DE3244708A1 (en) 1982-12-03 1982-12-03 DEVICE FOR GENERATING AN IGNITION SIGNAL FOR OVERFLIGHT AIRCRAFT

Publications (3)

Publication Number Publication Date
SE8306625D0 true SE8306625D0 (en) 1983-12-01
SE8306625L SE8306625L (en) 1984-06-04
SE458310B SE458310B (en) 1989-03-13

Family

ID=6179681

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8306625A SE458310B (en) 1982-12-03 1983-12-01 DEVICE FOR GENERATING A FLASH SIGNAL FOR A FLYING FLIGHT BODY

Country Status (3)

Country Link
DE (1) DE3244708A1 (en)
GB (1) GB2133514B (en)
SE (1) SE458310B (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3427020A1 (en) * 1984-07-21 1986-01-23 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn NAVIGATION AND FLIGHT GUIDANCE
DE3438305A1 (en) * 1984-10-19 1986-04-24 Diehl GmbH & Co, 8500 Nürnberg UNMANNED AIRCRAFT FOR COMBATING GROUND TARGETS
DE3514893A1 (en) * 1985-04-25 1986-11-06 Rheinmetall GmbH, 4000 Düsseldorf METHOD FOR OPERATING A PROXIMITY DETECTOR AND DEVICE FOR IMPLEMENTING THE METHOD
DE3707888A1 (en) * 1987-03-12 1988-09-22 Messerschmitt Boelkow Blohm SENSOR FOR COMBATING HELICOPTERS
DE3811314B3 (en) * 1988-04-02 2013-12-05 LFK Lenkflugkörpersysteme GmbH Sensor system for dispensers
DE3821218A1 (en) * 1988-06-23 1990-03-08 Diehl Gmbh & Co METHOD FOR COMBATING A TARGET OBJECT FROM A FLIGHT PROJECT, AND FLIGHT PROJECT TO EXERCISE THE METHOD
DE3843006A1 (en) * 1988-12-21 1990-06-28 Messerschmitt Boelkow Blohm DEVICE FOR DETECTING AND IDENTIFYING SINGLE DESTINATIONS
DE19500993A1 (en) * 1995-01-14 1996-07-18 Contraves Gmbh Establishing roll attitude of rolling flying object, e.g rocket or other projectile
SE519568C2 (en) * 2000-07-03 2003-03-11 Bofors Weapon Sys Ab Device at zone tube-mounted ammunition unit
DE102013017331A1 (en) * 2013-10-17 2015-04-23 Bundesrepublik Deutschland, vertreten durch das BMVg, vertreten durch das Bundesamt für Ausrüstung, Informationstechnik und Nutzung der Bundeswehr Method for initiating an active charge of an explosive projectile and detonator thereto

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3000007A1 (en) * 1979-01-02 1980-09-18 Raytheon Co FIGHTER VEHICLE DEFENSE SYSTEM
US4195574A (en) * 1961-09-01 1980-04-01 The United States Of America As Represented By The Secretary Of The Navy Optical fuze
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
BE795623A (en) * 1972-02-18 1973-06-18 Dynamit Nobel Ag MULTI-PURPOSE HOLLOW-LOAD MINES
US3942446A (en) * 1974-09-06 1976-03-09 The United States Of America As Represented By The Secretary Of The Army Optical fuze and/or miss distance indicator
DE2608067C3 (en) * 1976-02-28 1984-07-26 Diehl GmbH & Co, 8500 Nürnberg Ignition circuit for cluster munitions
DE2922583A1 (en) * 1979-06-02 1981-01-22 Messerschmitt Boelkow Blohm APPLICATION IGNITION FOR ANTI-FIGHTER MISSILE
SE7909385L (en) * 1979-11-14 1981-05-15 Bofors Ab ROR
DE3023290C2 (en) * 1980-06-21 1983-11-17 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Device for target acquisition of moving and stationary ground targets from low-flying aircraft
DE3113472A1 (en) * 1981-04-03 1982-10-21 Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt SENSOR SYSTEM
US4422075A (en) * 1981-05-21 1983-12-20 Honeywell Inc. Proximity monitor
DE3122252C1 (en) * 1981-06-04 1982-11-04 Diehl GmbH & Co, 8500 Nürnberg Device for generating an end signal for overflight missiles

Also Published As

Publication number Publication date
GB2133514B (en) 1986-06-11
GB2133514A (en) 1984-07-25
SE458310B (en) 1989-03-13
GB8332130D0 (en) 1984-01-11
DE3244708C2 (en) 1990-02-08
SE8306625L (en) 1984-06-04
DE3244708A1 (en) 1984-06-07

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