ES468612A1 - Dispositivo de control perfeccionado que permite, por la e- yeccion controlada de chorros de gas laterales, modificar latrayectoria de un proyectil. - Google Patents

Dispositivo de control perfeccionado que permite, por la e- yeccion controlada de chorros de gas laterales, modificar latrayectoria de un proyectil.

Info

Publication number
ES468612A1
ES468612A1 ES468612A ES468612A ES468612A1 ES 468612 A1 ES468612 A1 ES 468612A1 ES 468612 A ES468612 A ES 468612A ES 468612 A ES468612 A ES 468612A ES 468612 A1 ES468612 A1 ES 468612A1
Authority
ES
Spain
Prior art keywords
projectiles
projectile
arrangement
missile
fitted
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
Application number
ES468612A
Other languages
English (en)
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.)
Thomson-Brandt SA
Original Assignee
Thomson-Brandt SA
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 Thomson-Brandt SA filed Critical Thomson-Brandt SA
Publication of ES468612A1 publication Critical patent/ES468612A1/es
Expired 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
    • 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
    • F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Overhead Projectors And Projection Screens (AREA)
  • Projection Apparatus (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

Dispositivo de control perfeccionado que permite por la eyección controlada de chorros de gas laterales, modificar la trayectoria de un proyectil, caracterizado porque incluye: una fuente de energía que suministra un flujo de gas en la entrada de un cuello de tobera dispuesto sobre el eje longitudinal del proyectil; medios de distribución, colocados a la salida del cuello de tobera, que permiten distribuir el flujo de gas en conductos divergentes; orificios de eyección, situados sobre la periferia del cuerpo del proyectil, que son alimentados por la salida de los conductos divergentes y están dispuestos de manera que crean un sistema de fuerzas cuya resultante pasa sensiblemente por el centro de gravedad del proyectil.
ES468612A 1977-04-08 1978-04-07 Dispositivo de control perfeccionado que permite, por la e- yeccion controlada de chorros de gas laterales, modificar latrayectoria de un proyectil. Expired ES468612A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7710755A FR2386802A1 (fr) 1977-04-08 1977-04-08 Dispositif de pilotage pour projectile du genre missile, et projectile equipe de ce dispositif

Publications (1)

Publication Number Publication Date
ES468612A1 true ES468612A1 (es) 1979-07-16

Family

ID=9189244

Family Applications (1)

Application Number Title Priority Date Filing Date
ES468612A Expired ES468612A1 (es) 1977-04-08 1978-04-07 Dispositivo de control perfeccionado que permite, por la e- yeccion controlada de chorros de gas laterales, modificar latrayectoria de un proyectil.

Country Status (26)

Country Link
US (1) US4211378A (es)
JP (1) JPS549499A (es)
AT (1) AT354311B (es)
AU (1) AU514128B2 (es)
BE (1) BE865743A (es)
BR (1) BR7802023A (es)
CA (1) CA1097983A (es)
CH (1) CH626167A5 (es)
DE (1) DE2815087C2 (es)
DK (1) DK148728C (es)
ES (1) ES468612A1 (es)
FI (1) FI68909C (es)
FR (1) FR2386802A1 (es)
GB (1) GB1591766A (es)
GR (1) GR66175B (es)
IE (1) IE46527B1 (es)
IN (1) IN148286B (es)
IT (1) IT1158680B (es)
LU (1) LU79394A1 (es)
NL (1) NL7803723A (es)
NO (1) NO144755C (es)
OA (1) OA05931A (es)
PT (1) PT67878B (es)
SE (1) SE422244B (es)
TR (1) TR21431A (es)
ZA (1) ZA781907B (es)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2463909B1 (fr) * 1979-08-17 1985-10-25 Thomson Brandt Procede de pilotage et de guidage d'un missile, et missile equipe de moyens de mise en oeuvre de ce procede
FR2492966B1 (fr) * 1980-10-29 1986-01-31 Serat Perfectionnements aux projectiles a trajectoire corrigee
FR2504252B1 (fr) * 1981-04-21 1987-03-06 Thomson Brandt Projectile guide
FR2504085A1 (fr) * 1981-04-21 1982-10-22 Thomson Brandt Dispositif de pilotage par jets de gaz et projectile comprenant un tel dispositif
EP0245565B1 (fr) * 1986-05-12 1991-03-13 AEROSPATIALE Société Nationale Industrielle Procédé de pilotage d'un missile à faible vitesse, système d'arme et missile pour la mise en oeuvre du procédé
FR2578665B1 (fr) * 1981-06-04 1988-02-12 Aerospatiale Procede de pilotage d'un missile a faible vitesse, systeme d'arme et missile pour la mise en oeuvre du procede
DE3231528C1 (de) * 1982-08-25 1983-10-27 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Steuersystem fuer eine fluegellose Lenkmunition
US4537371A (en) * 1982-08-30 1985-08-27 Ltv Aerospace And Defense Company Small caliber guided projectile
FR2536720A1 (fr) * 1982-11-29 1984-06-01 Aerospatiale Systeme pour le pilotage d'un missile au moyen de jets gazeux lateraux et missile comportant un tel systeme
FR2538098B1 (fr) * 1982-12-17 1987-11-20 Thomson Brandt Dispositif de pilotage par jets de gaz lateraux
WO1984002974A1 (en) * 1983-01-19 1984-08-02 Ford Motor Co Ram air steering system for a guided missile
JPS60501366A (ja) * 1983-01-20 1985-08-22 ローラル・エアロスペイス・コーポレイション 誘導ミサイルのためのラム空気燃焼式操舵装置
JPS59160305U (ja) * 1983-04-14 1984-10-27 防衛庁技術研究本部長 姿勢制御装置
DE3317583C2 (de) * 1983-05-13 1986-01-23 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung mit einer von einer Treibmittelquelle versorgten Düsenanordnung
US4560120A (en) * 1983-08-19 1985-12-24 The United States Of America As Represented By The Secretary Of The Army Spin stabilized impulsively controlled missile (SSICM)
FR2557926B1 (fr) * 1984-01-06 1986-04-11 Brandt Armements Propulseur a gaz pour projectile guide.
DE3442974C1 (de) * 1984-11-24 1986-03-13 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung zum Stabilisieren und Vermindern der Pendelung eines mit UEberschallgeschwindigkeit fliegenden Flugkoerpers
DE3442972C1 (de) * 1984-11-24 1986-03-13 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Schnellfliegender Flugkörper
US4779821A (en) * 1985-05-07 1988-10-25 Allied Signal Inc. Small vehicle roll control and steering
US4685639A (en) * 1985-12-23 1987-08-11 Ford Aerospace & Communications Corp. Pneumatically actuated ram air steering system for a guided missile
DE3838100A1 (de) * 1988-11-10 1990-05-17 Messerschmitt Boelkow Blohm Fluidverteiler
DE59004020D1 (de) * 1989-09-19 1994-02-10 Diehl Gmbh & Co Bahnkorrigierbares Projektil.
US5070761A (en) * 1990-08-07 1991-12-10 The United States Of America As Represented By The Secretary Of The Navy Venting apparatus for controlling missile underwater trajectory
DE4210113C1 (de) * 1992-03-27 1998-11-05 Athanassios Dr Ing Zacharias Verfahren zum Leiten eines Flugkörpers und Flugkörper
US5456425A (en) * 1993-11-04 1995-10-10 Aerojet General Corporation Multiple pintle nozzle propulsion control system
US6178741B1 (en) 1998-10-16 2001-01-30 Trw Inc. Mems synthesized divert propulsion system
RU2156950C1 (ru) * 1999-11-22 2000-09-27 Государственное унитарное предприятие "Государственное научно-производственное предприятие "Сплав" Газореактивная система управления реактивного снаряда
US6981672B2 (en) * 2003-09-17 2006-01-03 Aleiant Techsystems Inc. Fixed canard 2-D guidance of artillery projectiles
US7989744B2 (en) * 2008-02-01 2011-08-02 Raytheon Company Methods and apparatus for transferring a fluid
US8269156B2 (en) 2008-03-04 2012-09-18 The Charles Stark Draper Laboratory, Inc. Guidance control system for projectiles
US8076623B2 (en) * 2009-03-17 2011-12-13 Raytheon Company Projectile control device
US8618455B2 (en) * 2009-06-05 2013-12-31 Safariland, Llc Adjustable range munition
FR2980265B1 (fr) * 2011-09-21 2017-02-24 Mbda France Systeme pour le pilotage d'un engin volant a l'aide de paires de tuyeres laterales
US9927217B1 (en) * 2014-09-05 2018-03-27 Valley Tech Systems, Inc. Attitude control system
US11143143B1 (en) 2018-05-11 2021-10-12 Valley Tech Systems, Inc. Extinguishable divert system

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2584127A (en) * 1946-12-05 1952-02-05 Sperry Corp Servo system
US2822755A (en) * 1950-12-01 1958-02-11 Mcdonnell Aircraft Corp Flight control mechanism for rockets
US2726510A (en) * 1952-03-26 1955-12-13 Daniel And Florence Guggenhcim Flight-control apparatus involving steering combustion chambers
US2816721A (en) * 1953-09-15 1957-12-17 Taylor Richard John Rocket powered aerial vehicle
US3045596A (en) * 1954-02-10 1962-07-24 Randolph S Rae Guided missile
US3588003A (en) * 1969-06-03 1971-06-28 Us Army Gyro controller
US3599899A (en) * 1969-06-20 1971-08-17 Thiokol Chemical Corp Rocket control
US3655148A (en) * 1969-06-20 1972-04-11 Thiokol Chemical Corp Control mechanism
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

Also Published As

Publication number Publication date
DK148728B (da) 1985-09-09
AT354311B (de) 1979-12-27
DE2815087A1 (de) 1978-10-12
GB1591766A (en) 1981-06-24
NO144755C (no) 1981-10-28
DK148728C (da) 1986-01-27
IT1158680B (it) 1987-02-25
NL7803723A (nl) 1978-10-10
PT67878A (fr) 1978-05-01
IE46527B1 (en) 1983-07-13
ATA248778A (de) 1979-05-15
FI68909C (fi) 1985-11-11
BR7802023A (pt) 1978-11-21
SE422244B (sv) 1982-02-22
CH626167A5 (es) 1981-10-30
AU3492578A (en) 1979-10-18
FI781043A7 (fi) 1978-10-09
JPS549499A (en) 1979-01-24
CA1097983A (en) 1981-03-24
DK154978A (da) 1978-10-09
BE865743A (fr) 1978-07-31
ZA781907B (en) 1979-03-28
IE780690L (en) 1978-10-08
PT67878B (fr) 1979-10-12
DE2815087C2 (de) 1986-05-28
AU514128B2 (en) 1981-01-29
GR66175B (es) 1981-01-21
FR2386802B1 (es) 1980-03-14
FR2386802A1 (fr) 1978-11-03
IN148286B (es) 1981-01-03
NO781234L (no) 1978-10-10
TR21431A (tr) 1984-06-04
OA05931A (fr) 1981-06-30
NO144755B (no) 1981-07-20
SE7803808L (sv) 1978-10-09
LU79394A1 (fr) 1978-07-13
FI68909B (fi) 1985-07-31
IT7822075A0 (it) 1978-04-07
US4211378A (en) 1980-07-08
JPS6134079B2 (es) 1986-08-05

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19980401