IT1151233B - Procedimento per il pilotaggio di un missile a bassa velocita',impianto d'arma e missile per l'attuazione del procedimento - Google Patents

Procedimento per il pilotaggio di un missile a bassa velocita',impianto d'arma e missile per l'attuazione del procedimento

Info

Publication number
IT1151233B
IT1151233B IT21465/82A IT2146582A IT1151233B IT 1151233 B IT1151233 B IT 1151233B IT 21465/82 A IT21465/82 A IT 21465/82A IT 2146582 A IT2146582 A IT 2146582A IT 1151233 B IT1151233 B IT 1151233B
Authority
IT
Italy
Prior art keywords
procedure
missile
piloting
weapon
implementing
Prior art date
Application number
IT21465/82A
Other languages
English (en)
Other versions
IT8221465A0 (it
Inventor
Jacques Raynaud
Michel Maree
Robert Vaillant
Jean Ansaldi
Jean Guillot
Original Assignee
Aerospatiale
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 Aerospatiale filed Critical Aerospatiale
Publication of IT8221465A0 publication Critical patent/IT8221465A0/it
Application granted granted Critical
Publication of IT1151233B publication Critical patent/IT1151233B/it

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/665—Steering by varying intensity or direction of thrust characterised by using a nozzle provided with at least a deflector mounted within the nozzle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
IT21465/82A 1981-06-04 1982-05-25 Procedimento per il pilotaggio di un missile a bassa velocita',impianto d'arma e missile per l'attuazione del procedimento IT1151233B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8111088A FR2578665B1 (fr) 1981-06-04 1981-06-04 Procede de pilotage d'un missile a faible vitesse, systeme d'arme et missile pour la mise en oeuvre du procede

Publications (2)

Publication Number Publication Date
IT8221465A0 IT8221465A0 (it) 1982-05-25
IT1151233B true IT1151233B (it) 1986-12-17

Family

ID=9259192

Family Applications (1)

Application Number Title Priority Date Filing Date
IT21465/82A IT1151233B (it) 1981-06-04 1982-05-25 Procedimento per il pilotaggio di un missile a bassa velocita',impianto d'arma e missile per l'attuazione del procedimento

Country Status (6)

Country Link
US (1) US4645139A (it)
BE (1) BE893252A (it)
DE (1) DE3221039C2 (it)
FR (1) FR2578665B1 (it)
IT (1) IT1151233B (it)
NL (1) NL191654C (it)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3924810A1 (de) * 1989-07-27 1991-02-07 Bundesrep Deutschland Drallstabilisierte unterkaliber-rakete mit geteilter nutzlast
GB2459914B (en) * 1989-10-17 2010-05-19 Aerospatiale Guidance system for a missile provided with a photosensitive detector
US5363766A (en) * 1990-02-08 1994-11-15 The United States Of America As Represented By The Secretary Of The Army Remjet powered, armor piercing, high explosive projectile
US5076511A (en) * 1990-12-19 1991-12-31 Honeywell Inc. Discrete impulse spinning-body hard-kill (disk)
DE4412687C2 (de) * 1994-04-13 1999-06-24 Diehl Stiftung & Co Mittels eines Laser-Leitstrahles fernsteuerbares Projektil
ES2264295B1 (es) * 2003-05-21 2008-05-16 Advanced Dynamics, S.A. Sistema dinamico para el gobierno de moviles.
IL162027A (en) * 2004-05-17 2009-05-04 Rafael Advanced Defense Sys Method and system for resetting the flight path of a non-guided bullet, including compensation for deviation from the oscillations of the launcher
DE102021003972A1 (de) 2021-08-03 2023-02-09 Diehl Defence Gmbh & Co. Kg Antriebssystem für einen Lenkflugkörper

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1194102A (it) * 1959-11-06
CH229444A (de) * 1942-04-21 1943-10-31 F Schwarzer Raketengeschoss.
US2524591A (en) * 1944-07-19 1950-10-03 Edward F Chandler Rocket projectile
US2503271A (en) * 1945-02-06 1950-04-11 Clarence N Hickman Rocket projectile
US2804823A (en) * 1955-05-13 1957-09-03 Jablansky Louis Multiple unit projectile
DE1147144B (de) * 1958-09-08 1963-04-11 Ferdinand Metzler Strahlangetriebener Flugkoerper
DE1172156B (de) * 1959-04-23 1964-06-11 Boelkow Entwicklungen Kg Aerodynamisch lenkbarer, rueckstossgetriebener Flugkoerper
US3283721A (en) * 1964-11-09 1966-11-08 Kruzell George Ralph Reaction type missile
FR1569559A (it) * 1964-11-26 1969-06-06
FR1488272A (fr) * 1966-03-22 1967-07-13 Bertin & Cie Système de pilotage de missiles
US3749334A (en) * 1966-04-04 1973-07-31 Us Army Attitude compensating missile system
DE1264869B (de) * 1966-09-15 1968-03-28 Boelkow Gmbh Dual-Treibsatz fuer Feststoffraketentriebwerke
US3859890A (en) * 1968-12-23 1975-01-14 Us Army Traveling tube ejector system
US3588003A (en) * 1969-06-03 1971-06-28 Us Army Gyro controller
SE340417B (it) * 1969-06-06 1971-11-15 Bofors Ab
DE2331031A1 (de) * 1973-06-19 1975-09-25 Diehl Fa Rueckstossfreie abschussvorrichtung fuer ein geschoss
US3986683A (en) * 1974-03-27 1976-10-19 The United States Of America As Represented By The Secretary Of The Air Force Jet tab steerable missile
US4078495A (en) * 1974-08-15 1978-03-14 The United States Of America As Represented By The Secretary Of The Navy Control after burnout for reaction steered missiles
DE2553201C2 (de) * 1975-11-27 1984-05-10 Rheinmetall GmbH, 4000 Düsseldorf Rückstoß- und knallfrei abschießbares Geschoß
FR2386802A1 (fr) * 1977-04-08 1978-11-03 Thomson Brandt Dispositif de pilotage pour projectile du genre missile, et projectile equipe de ce dispositif
FR2448706A1 (fr) * 1979-02-09 1980-09-05 Luchaire Sa Perfectionnements apportes aux munitions, notamment antichars, lancees par une arme a tir tendu
DE3205431A1 (de) * 1982-02-16 1983-08-25 Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt Raketengeschoss

Also Published As

Publication number Publication date
DE3221039A1 (de) 1987-01-08
DE3221039C2 (de) 1994-11-10
NL191654C (nl) 1995-12-02
FR2578665A1 (fr) 1986-09-12
US4645139A (en) 1987-02-24
FR2578665B1 (fr) 1988-02-12
BE893252A (fr) 1982-11-19
NL191654B (nl) 1995-08-01
IT8221465A0 (it) 1982-05-25
NL8202161A (nl) 1986-08-01

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TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19970527