DE68906964T2 - Vorrichtung zur Veränderung der Flugbahn eines Projektils durch pyrotechnische Impulsgeber. - Google Patents

Vorrichtung zur Veränderung der Flugbahn eines Projektils durch pyrotechnische Impulsgeber.

Info

Publication number
DE68906964T2
DE68906964T2 DE89401562T DE68906964T DE68906964T2 DE 68906964 T2 DE68906964 T2 DE 68906964T2 DE 89401562 T DE89401562 T DE 89401562T DE 68906964 T DE68906964 T DE 68906964T DE 68906964 T2 DE68906964 T2 DE 68906964T2
Authority
DE
Germany
Prior art keywords
pyrotechnic
projectile
trajectory
changing
pulse generators
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 - Fee Related
Application number
DE89401562T
Other languages
English (en)
Other versions
DE68906964D1 (de
Inventor
Jean Deffayet
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.)
TDA Armements SAS
Thomson Brandt Armements SA
Original Assignee
TDA Armements SAS
Thomson Brandt Armements 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 TDA Armements SAS, Thomson Brandt Armements SA filed Critical TDA Armements SAS
Publication of DE68906964D1 publication Critical patent/DE68906964D1/de
Application granted granted Critical
Publication of DE68906964T2 publication Critical patent/DE68906964T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00—Geometry
    • F05B2250/20—Geometry three-dimensional
    • F05B2250/22—Geometry three-dimensional parallelepipedic
DE89401562T 1988-06-10 1989-06-06 Vorrichtung zur Veränderung der Flugbahn eines Projektils durch pyrotechnische Impulsgeber. Expired - Fee Related DE68906964T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8807768A FR2632722B1 (fr) 1988-06-10 1988-06-10 Dispositif destine a modifier la trajectoire d'un projectile par impulseurs pyrotechniques

Publications (2)

Publication Number Publication Date
DE68906964D1 DE68906964D1 (de) 1993-07-15
DE68906964T2 true DE68906964T2 (de) 1993-12-02

Family

ID=9367164

Family Applications (1)

Application Number Title Priority Date Filing Date
DE89401562T Expired - Fee Related DE68906964T2 (de) 1988-06-10 1989-06-06 Vorrichtung zur Veränderung der Flugbahn eines Projektils durch pyrotechnische Impulsgeber.

Country Status (4)

Country Link
US (1) US5044156A (de)
EP (1) EP0346215B1 (de)
DE (1) DE68906964T2 (de)
FR (1) FR2632722B1 (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6178741B1 (en) * 1998-10-16 2001-01-30 Trw Inc. Mems synthesized divert propulsion system
IL167721A (en) 2005-03-29 2008-06-05 Israel Aerospace Ind Ltd Steering system and method for guided flying apparatus
FR2885213B1 (fr) 2005-05-02 2010-11-05 Giat Ind Sa Procede de commande d'une munition ou sous-munition, systeme d'attaque, munition et designateur mettant en oeuvre un tel procede
US9151581B2 (en) * 2005-09-07 2015-10-06 Omnitek Partners Llc Actuators for gun-fired projectiles and mortars
US7800031B2 (en) * 2005-09-07 2010-09-21 Omnitek Partners Llc Actuators for gun-fired projectiles and mortars
US8563910B2 (en) 2009-06-05 2013-10-22 The Charles Stark Draper Laboratory, Inc. Systems and methods for targeting a projectile payload
US11543835B2 (en) 2010-01-15 2023-01-03 Lockheed Martin Corporation Monolithic attitude control motor frame and system
US10914559B1 (en) 2016-11-21 2021-02-09 Lockheed Martin Corporation Missile, slot thrust attitude controller system, and method

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2613497A (en) * 1947-04-01 1952-10-14 Macdonald Gilmour Craig Controllable rocket thrust device
US3069846A (en) * 1959-09-28 1962-12-25 Clary Corp Thrust device
US3034434A (en) * 1960-03-08 1962-05-15 Frank H Swaim Thrust vector control system
US3099960A (en) * 1960-08-19 1963-08-06 George J Bryan Method of thrust vector control
US3263419A (en) * 1963-05-23 1966-08-02 Thiokol Chemical Corp Attitude control system for space vehicles
US3316719A (en) * 1965-03-11 1967-05-02 Curtiss Wright Corp Expansible rocket engines
US3328962A (en) * 1965-05-20 1967-07-04 Curtiss Wright Corp Orientation control system for space vehicles and ballistic missiles
US3380661A (en) * 1966-04-12 1968-04-30 United Aircraft Corp Thrust deflector
US3532297A (en) * 1967-01-23 1970-10-06 Rocket Research Corp Space vehicle attitude control by microrockets utilizing subliming solid propellants
FR2367659A2 (fr) * 1976-09-08 1978-05-12 Stauff Emile Dispositif de pilotage d'un projectile en autorotation
FR2450356A1 (fr) * 1979-02-27 1980-09-26 Aerospatiale Agencement de pilotage d'un propulseur d'engin a propergol solide
FR2469345A1 (fr) * 1979-11-09 1981-05-22 Thomson Brandt Procede de pilotage et de guidage de projectiles en phase terminale et projectiles comportant les moyens de mise en oeuvre de ce procede
US4444119A (en) * 1982-07-02 1984-04-24 The United States Of America As Represented By The Secretary Of The Army Fast response impulse generator
DE3521204A1 (de) * 1985-06-13 1986-12-18 Diehl GmbH & Co, 8500 Nürnberg Impulstriebwerk
DE3531686A1 (de) * 1985-09-05 1987-03-12 Rheinmetall Gmbh Steuerblock
FR2590973B1 (fr) * 1985-11-29 1988-02-12 France Etat Armement Dispositif de basculement de projectile sur trajectoire
USH236H (en) * 1986-07-14 1987-03-03 The United States Of America As Represented By The Secretary Of The Army Asymmetric side-exhausting nozzles
DE3708312A1 (de) * 1987-03-14 1988-09-22 Messerschmitt Boelkow Blohm Vorrichtung zum steuern eines flugkoerpers

Also Published As

Publication number Publication date
EP0346215B1 (de) 1993-06-09
FR2632722B1 (fr) 1993-09-03
FR2632722A1 (fr) 1989-12-15
EP0346215A1 (de) 1989-12-13
DE68906964D1 (de) 1993-07-15
US5044156A (en) 1991-09-03

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee