EP0418636A3 - Projectile with trajectory control system - Google Patents
Projectile with trajectory control system Download PDFInfo
- Publication number
- EP0418636A3 EP0418636A3 EP19900116937 EP90116937A EP0418636A3 EP 0418636 A3 EP0418636 A3 EP 0418636A3 EP 19900116937 EP19900116937 EP 19900116937 EP 90116937 A EP90116937 A EP 90116937A EP 0418636 A3 EP0418636 A3 EP 0418636A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile
- control system
- trajectory control
- trajectory
- control
- 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.)
- Granted
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
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)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3931173 | 1989-09-19 | ||
DE3931173 | 1989-09-19 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0418636A2 EP0418636A2 (en) | 1991-03-27 |
EP0418636A3 true EP0418636A3 (en) | 1991-04-17 |
EP0418636B1 EP0418636B1 (en) | 1993-12-29 |
Family
ID=6389691
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP90116937A Expired - Lifetime EP0418636B1 (en) | 1989-09-19 | 1990-09-04 | Projectile with trajectory control system |
Country Status (3)
Country | Link |
---|---|
US (1) | US5054712A (en) |
EP (1) | EP0418636B1 (en) |
DE (1) | DE59004020D1 (en) |
Families Citing this family (39)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4036166A1 (en) * | 1990-11-14 | 1992-05-21 | Diehl Gmbh & Co | RAILWAY CORRECTABLE PROJECT |
DE4408085C2 (en) * | 1994-03-10 | 1999-08-12 | Rheinmetall W & M Gmbh | Device for guiding a missile not rotating about its longitudinal axis |
DE4410326C2 (en) * | 1994-03-25 | 1998-07-02 | Rheinmetall Ind Ag | Projectile with a device for trajectory correction |
US5669581A (en) * | 1994-04-11 | 1997-09-23 | Aerojet-General Corporation | Spin-stabilized guided projectile |
US6254031B1 (en) * | 1994-08-24 | 2001-07-03 | Lockhead Martin Corporation | Precision guidance system for aircraft launched bombs |
US5647558A (en) * | 1995-02-14 | 1997-07-15 | Bofors Ab | Method and apparatus for radial thrust trajectory correction of a ballistic projectile |
DE19540378C1 (en) * | 1995-10-30 | 1997-01-23 | Daimler Benz Aerospace Ag | Release device for rocket pipes, especially for aggressive propellants |
EP0950165A4 (en) | 1997-01-02 | 2000-03-22 | Tibor G Horwath | Reticle for use in a guidance seeker for a spinning projectile |
US6722609B2 (en) | 1998-02-13 | 2004-04-20 | James M. Linick | Impulse motor and apparatus to improve trajectory correctable munitions including cannon launched munitions, glide bombs, missiles, rockets and the like |
US6308911B1 (en) * | 1998-10-30 | 2001-10-30 | Lockheed Martin Corp. | Method and apparatus for rapidly turning a vehicle in a fluid medium |
FR2795135B1 (en) * | 1999-06-16 | 2001-08-31 | Centre Nat Etd Spatiales | POWDER MICROPROPULSION SYSTEM AND METHOD FOR PRODUCING SUCH A MICROPROPULSION SYSTEM |
US6695251B2 (en) * | 2001-06-19 | 2004-02-24 | Space Systems/Loral, Inc | Method and system for synchronized forward and Aft thrust vector control |
DE10141169A1 (en) † | 2001-08-22 | 2003-03-13 | Diehl Munitionssysteme Gmbh | artillery rocket |
US6752351B2 (en) * | 2002-11-04 | 2004-06-22 | The United States Of America As Represented By The Secretary Of The Navy | Low mass flow reaction jet |
US7795567B2 (en) * | 2005-04-05 | 2010-09-14 | Raytheon Company | Guided kinetic penetrator |
US7416154B2 (en) * | 2005-09-16 | 2008-08-26 | The United States Of America As Represented By The Secretary Of The Army | Trajectory correction kit |
DE102005052474B3 (en) * | 2005-11-03 | 2007-07-12 | Junghans Feinwerktechnik Gmbh & Co. Kg | Spiked artillery projectile |
US7851732B2 (en) * | 2006-03-07 | 2010-12-14 | Raytheon Company | System and method for attitude control of a flight vehicle using pitch-over thrusters |
IL178840A0 (en) * | 2006-10-24 | 2007-09-20 | Rafael Advanced Defense Sys | System |
DE102007059397A1 (en) | 2007-12-10 | 2009-06-18 | Diehl Bgt Defence Gmbh & Co. Kg | swash detonator |
US7872215B2 (en) * | 2008-02-29 | 2011-01-18 | Raytheon Company | Methods and apparatus for guiding a projectile |
US8618455B2 (en) * | 2009-06-05 | 2013-12-31 | Safariland, Llc | Adjustable range munition |
WO2011088277A1 (en) * | 2010-01-15 | 2011-07-21 | Lockheed Martin Corporation | Monolithic attitude control motor frame and system |
US8735788B2 (en) * | 2011-02-18 | 2014-05-27 | Raytheon Company | Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control |
US9170070B2 (en) | 2012-03-02 | 2015-10-27 | Orbital Atk, Inc. | Methods and apparatuses for active protection from aerial threats |
US11947349B2 (en) | 2012-03-02 | 2024-04-02 | Northrop Grumman Systems Corporation | Methods and apparatuses for engagement management of aerial threats |
US9551552B2 (en) | 2012-03-02 | 2017-01-24 | Orbital Atk, Inc. | Methods and apparatuses for aerial interception of aerial threats |
US11313650B2 (en) | 2012-03-02 | 2022-04-26 | Northrop Grumman Systems Corporation | Methods and apparatuses for aerial interception of aerial threats |
US9501055B2 (en) | 2012-03-02 | 2016-11-22 | Orbital Atk, Inc. | Methods and apparatuses for engagement management of aerial threats |
US9018572B2 (en) * | 2012-11-06 | 2015-04-28 | Raytheon Company | Rocket propelled payload with divert control system within nose cone |
US20140137539A1 (en) * | 2012-11-19 | 2014-05-22 | Raytheon Company | Thrust-producing device with detonation motor |
US9068808B2 (en) * | 2013-01-17 | 2015-06-30 | Raytheon Company | Air vehicle with bilateral steering thrusters |
US9377279B2 (en) * | 2014-04-22 | 2016-06-28 | Raytheon Company | Rocket cluster divert and attitude control system |
DE102014014950A1 (en) * | 2014-10-08 | 2016-04-28 | Mbda Deutschland Gmbh | missile |
DE102014014952B4 (en) * | 2014-10-08 | 2016-05-25 | Mbda Deutschland Gmbh | missile |
US10914559B1 (en) * | 2016-11-21 | 2021-02-09 | Lockheed Martin Corporation | Missile, slot thrust attitude controller system, and method |
RU2687827C1 (en) * | 2018-11-23 | 2019-05-16 | Акционерное общество "Научно-производственное предприятие "Дельта" | Method for increasing firing range by means of corrected artillery ammunition |
RU2702035C1 (en) * | 2019-03-21 | 2019-10-03 | Акционерное общество "Научно-производственное предприятие "Дельта" | Method of correction of ellipse of scattering of artillery rotating projectiles |
RU2767645C1 (en) * | 2020-10-19 | 2022-03-18 | Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации | Anti-aircraft guided missile 9m96 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3028807A (en) * | 1959-08-24 | 1962-04-10 | Mcdonnell Aircraft Corp | Guidance system |
US3034434A (en) * | 1960-03-08 | 1962-05-15 | Frank H Swaim | Thrust vector control system |
GB1008595A (en) * | 1963-07-08 | 1965-10-27 | Fike Metal Prod Corp | A rupture plate adapted to control the flow of fluid from a container |
FR2232721A1 (en) * | 1973-06-08 | 1975-01-03 | Barker Geoffrey | |
US3964390A (en) * | 1971-03-31 | 1976-06-22 | Imperial Chemical Industries Limited | Bursting disc assembly |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE331435B (en) * | 1969-04-23 | 1970-12-21 | Bofors Ab | |
CA1009370A (en) * | 1972-01-03 | 1977-04-26 | Ship Systems | Laser guided projectile |
SE429064B (en) * | 1976-04-02 | 1983-08-08 | Bofors Ab | FINAL PHASE CORRECTION OF ROTATING PROJECTILE |
FR2386802A1 (en) * | 1977-04-08 | 1978-11-03 | Thomson Brandt | CONTROL DEVICE FOR PROJECTILE OF THE MISSILE GENUS, AND PROJECTILE EQUIPPED WITH THIS DEVICE |
FR2469345A1 (en) * | 1979-11-09 | 1981-05-22 | Thomson Brandt | METHOD FOR DRIVING AND GUIDING TERMINAL PROJECTILES AND PROJECTILES INCLUDING MEANS FOR CARRYING OUT SAID METHOD |
FR2504703B1 (en) * | 1981-04-24 | 1986-09-05 | Stauff Emile | SYSTEM FOR CONTROLLING A PROJECTILE TO AN AXIAL REFERENCE TO ELIMINATE THE WIND EFFECT |
US4503773A (en) * | 1982-12-27 | 1985-03-12 | Thiokol Corporation | Aft end igniter for full, head-end web solid propellant rocket motors |
DE3521204A1 (en) * | 1985-06-13 | 1986-12-18 | Diehl GmbH & Co, 8500 Nürnberg | IMPULSE ENGINE |
GB8822282D0 (en) * | 1988-09-22 | 1989-04-19 | British Aerospace | Course correction unit |
-
1990
- 1990-09-04 DE DE90116937T patent/DE59004020D1/en not_active Expired - Fee Related
- 1990-09-04 EP EP90116937A patent/EP0418636B1/en not_active Expired - Lifetime
- 1990-09-10 US US07/580,333 patent/US5054712A/en not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3028807A (en) * | 1959-08-24 | 1962-04-10 | Mcdonnell Aircraft Corp | Guidance system |
US3034434A (en) * | 1960-03-08 | 1962-05-15 | Frank H Swaim | Thrust vector control system |
GB1008595A (en) * | 1963-07-08 | 1965-10-27 | Fike Metal Prod Corp | A rupture plate adapted to control the flow of fluid from a container |
US3964390A (en) * | 1971-03-31 | 1976-06-22 | Imperial Chemical Industries Limited | Bursting disc assembly |
FR2232721A1 (en) * | 1973-06-08 | 1975-01-03 | Barker Geoffrey |
Also Published As
Publication number | Publication date |
---|---|
EP0418636A2 (en) | 1991-03-27 |
US5054712A (en) | 1991-10-08 |
EP0418636B1 (en) | 1993-12-29 |
DE59004020D1 (en) | 1994-02-10 |
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Legal Events
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PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
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17Q | First examination report despatched |
Effective date: 19920902 |
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RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: DEUTSCH-FRANZOESISCHES FORSCHUNGSINSTITUT SAINT-L Owner name: DIEHL GMBH & CO. |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: LEHR, HARMUTH Inventor name: SCHIRM, VOLKER Inventor name: WIESE, ULRICH Inventor name: LEHRIEDER, GUENTHER Inventor name: BAER, KLAUS |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: LEHR, HARTMUTH Inventor name: SCHIRM, VOLKER Inventor name: WIESE, ULRICH Inventor name: LEHRIEDER, GUENTHER Inventor name: BAER, KLAUS |
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