DE69100454D1 - Raketensteuerungsanlage mit seitlichem Düsen. - Google Patents

Raketensteuerungsanlage mit seitlichem Düsen.

Info

Publication number: DE69100454D1
Authority: DE; Germany
Prior art keywords: control system; side nozzles; missile control; missile; nozzles
Prior art date: 1990-03-14
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 - Fee Related

Application number

DE91400520T

Other languages

English (en)

Other versions

DE69100454T2 (de

Inventor

Jean-Pierre Morgand

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.)

Airbus Group SAS

Original Assignee

Airbus Group SAS

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.)

1990-03-14

Filing date

1991-02-26

Publication date

1993-11-11

1991-02-26 Application filed by Airbus Group SAS filed Critical Airbus Group SAS

1993-11-11 Publication of DE69100454D1 publication Critical patent/DE69100454D1/de

1994-03-03 Application granted granted Critical

1994-03-03 Publication of DE69100454T2 publication Critical patent/DE69100454T2/de

2011-02-27 Anticipated expiration legal-status Critical

Status Expired - Fee Related legal-status Critical Current

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)
Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Nozzles (AREA)
Jet Pumps And Other Pumps (AREA)
Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

DE91400520T 1990-03-14 1991-02-26 Raketensteuerungsanlage mit seitlichem Düsen. Expired - Fee Related DE69100454T2 (de)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
FR909003252A FR2659733B1 (fr)	1990-03-14	1990-03-14	Systeme pour le pilotage d'un missile au moyen de tuyeres laterales.

Publications (2)

Publication Number	Publication Date
DE69100454D1 true DE69100454D1 (de)	1993-11-11
DE69100454T2 DE69100454T2 (de)	1994-03-03

Family

ID=9394722

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
DE91400520T Expired - Fee Related DE69100454T2 (de)	1990-03-14	1991-02-26	Raketensteuerungsanlage mit seitlichem Düsen.

Country Status (8)

Country	Link
US (1)	US5074492A (de)
EP (1)	EP0447283B1 (de)
JP (1)	JP3181930B2 (de)
AU (1)	AU631969B2 (de)
CA (1)	CA2038091C (de)
DE (1)	DE69100454T2 (de)
ES (1)	ES2046862T3 (de)
FR (1)	FR2659733B1 (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2659734B1 (fr) *	1990-03-14	1992-07-03	Aerospatiale	Systeme pour le pilotage d'un missile au moyen de jets gazeux lateraux.
WO1994010527A1 (fr) *	1992-10-23	1994-05-11	Arkhangelsky Ivan I	Procede de guidage d'un missile et son dispositif de mise en ×uvre
FR2699610B1 (fr) *	1992-12-22	1995-02-10	Aerospatiale	Dispositif d'actionnement d'un organe mécanique, notamment pour le pilotage en force d'un missile, et missile équipé dudit dispositif.
US6254031B1 (en) *	1994-08-24	2001-07-03	Lockhead Martin Corporation	Precision guidance system for aircraft launched bombs
US5631830A (en)	1995-02-03	1997-05-20	Loral Vought Systems Corporation	Dual-control scheme for improved missle maneuverability
RU2125701C1 (ru) *	1998-03-16	1999-01-27	Государственное научно-производственное предприятие "Сплав"	Ракета
US6308911B1 (en)	1998-10-30	2001-10-30	Lockheed Martin Corp.	Method and apparatus for rapidly turning a vehicle in a fluid medium
RU2247926C1 (ru) *	2003-06-18	2005-03-10	Государственное унитарное предприятие "Конструкторское бюро приборостроения"	Способ стабилизации ракеты в полете и ракета для его реализации
US7287725B2 (en) *	2005-04-25	2007-10-30	Raytheon Company	Missile control system and method
US7856806B1 (en) *	2006-11-06	2010-12-28	Raytheon Company	Propulsion system with canted multinozzle grid
US7872215B2 (en) *	2008-02-29	2011-01-18	Raytheon Company	Methods and apparatus for guiding a projectile
US8269156B2 (en)	2008-03-04	2012-09-18	The Charles Stark Draper Laboratory, Inc.	Guidance control system for projectiles
US8117847B2 (en)	2008-03-07	2012-02-21	Raytheon Company	Hybrid missile propulsion system with reconfigurable multinozzle grid
US8338768B2 (en)	2008-10-15	2012-12-25	Honeywell International Inc.	Actuation assembly
US8362408B2 (en) *	2009-10-22	2013-01-29	Honeywell International Inc.	Steerable projectile charging system
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
RU2485342C1 (ru) *	2012-02-20	2013-06-20	Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации	Силовой блок двигательной установки ракеты-носителя
US9068808B2 (en) *	2013-01-17	2015-06-30	Raytheon Company	Air vehicle with bilateral steering thrusters
KR102134354B1 (ko) *	2020-04-16	2020-07-15	국방과학연구소	화염 차단 장치 및 이를 포함하는 유도 무기

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3136250A (en) *	1962-05-04	1964-06-09	Samuel A Humphrey	Integrated auxiliary power unit
US4085909A (en) *	1976-10-04	1978-04-25	Ford Motor Company	Combined warm gas fin and reaction control servo
FR2504252B1 (fr) *	1981-04-21	1987-03-06	Thomson Brandt	Projectile guide
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
FR2620812B1 (fr) *	1987-09-18	1992-04-17	Thomson Brandt Armements	Dispositif de commutation de jets de gaz lateraux destine au pilotage d'engins
FR2622066B1 (fr) *	1987-10-16	1995-08-25	Rossi Rinaldo	Machine electrique a entrefers radiaux

1990
- 1990-03-14 FR FR909003252A patent/FR2659733B1/fr not_active Expired - Fee Related
1991
- 1991-02-26 DE DE91400520T patent/DE69100454T2/de not_active Expired - Fee Related
- 1991-02-26 ES ES199191400520T patent/ES2046862T3/es not_active Expired - Lifetime
- 1991-02-26 AU AU71369/91A patent/AU631969B2/en not_active Ceased
- 1991-02-26 EP EP91400520A patent/EP0447283B1/de not_active Expired - Lifetime
- 1991-03-07 US US07/665,895 patent/US5074492A/en not_active Expired - Lifetime
- 1991-03-11 CA CA002038091A patent/CA2038091C/fr not_active Expired - Lifetime
- 1991-03-14 JP JP04857691A patent/JP3181930B2/ja not_active Expired - Fee Related

Also Published As

Publication number	Publication date
FR2659733B1 (fr)	1994-07-01
EP0447283A1 (de)	1991-09-18
AU7136991A (en)	1991-09-19
JPH04222399A (ja)	1992-08-12
CA2038091A1 (fr)	1991-09-15
EP0447283B1 (de)	1993-10-06
US5074492A (en)	1991-12-24
JP3181930B2 (ja)	2001-07-03
CA2038091C (fr)	2000-08-29
FR2659733A1 (fr)	1991-09-20
AU631969B2 (en)	1992-12-10
ES2046862T3 (es)	1994-02-01
DE69100454T2 (de)	1994-03-03

Publication	Publication Date	Title
FI891935A7 (fi)	1989-12-31	Foerkontrollsystem.
NO892702L (no)	1990-01-02	Kontrollsystem.
DE69100454D1 (de)	1993-11-11	Raketensteuerungsanlage mit seitlichem Düsen.
DE69110474D1 (de)	1995-07-20	Ferngesteuerte düsenanlage.
DE69100339D1 (de)	1993-10-14	Raketensteuerungsanlage mit seitlichem Gasstrahl.
DE69115268D1 (de)	1996-01-18	Mehrmotoren-gebläsesystem mit verbesserter geschwindigkeitsregelung.
DE68906898D1 (de)	1993-07-15	Kraftstoffsteuerungssystem.
DE69006370D1 (de)	1994-03-10	Lasersteuerschaltung.
DE69127414D1 (de)	1997-10-02	Werfersteuersystem
DE3882496D1 (de)	1993-08-26	Positionssteuerungssystem.
DE69126602D1 (de)	1997-07-24	Ski mit Steifigkeitsbeeinflussungssystem
DE69119573D1 (de)	1996-06-20	Steuerungssystem mit gleitender Wirkungsweise
DE69206268D1 (de)	1996-01-04	Modellunterstüztes regelungssystem.
FI910512A7 (fi)	1992-08-02	Kontrollsystem.
DE69204760D1 (de)	1995-10-19	Geschwindigkeitssteuerung.
DE69103218D1 (de)	1994-09-08	Farbspritzanlage mit kontrolliertem Durchfluss.
DE68919297D1 (de)	1994-12-15	Flugbahnverbesserungssystem für Flugkörper mit steuerbarer Flugbahn.
DE69201421D1 (de)	1995-03-23	Systemsteuerungen.
DE69119562D1 (de)	1996-06-20	Steuerungssystem mit gleitender Wirkungsweise
DE69107881D1 (de)	1995-04-13	Fernsteuersystem.
MX173902B (es)	1994-04-07	Control optico al vuelo
DE58901726D1 (de)	1992-07-30	Waffensystem.
NO912312D0 (no)	1991-06-14	Styresystem.
DE68911721D1 (de)	1994-02-10	Getriebesteuerungssysteme.
TR24888A (tr)	1992-07-01	Yakiciya sahip kontrol sistemi.

Legal Events

Date	Code	Title	Description
1994-11-03	8364	No opposition during term of opposition
2010-12-16	8339	Ceased/non-payment of the annual fee