NO20056127L - Missil med oddetall symmetrifinner - Google Patents
Missil med oddetall symmetrifinnerInfo
- Publication number
- NO20056127L NO20056127L NO20056127A NO20056127A NO20056127L NO 20056127 L NO20056127 L NO 20056127L NO 20056127 A NO20056127 A NO 20056127A NO 20056127 A NO20056127 A NO 20056127A NO 20056127 L NO20056127 L NO 20056127L
- Authority
- NO
- Norway
- Prior art keywords
- missile
- odd number
- finder
- viewfinder
- fins
- Prior art date
Links
- 230000010355 oscillation Effects 0.000 abstract 2
- 238000003384 imaging method Methods 0.000 abstract 1
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
- F42B10/02—Stabilising arrangements
- F42B10/04—Stabilising arrangements using fixed fins
- F42B10/06—Tail fins
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)
- Radar Systems Or Details Thereof (AREA)
- Waveguide Aerials (AREA)
- Inorganic Insulating Materials (AREA)
- Crystals, And After-Treatments Of Crystals (AREA)
Abstract
Et missil (10) en et drevet missil eller et ikke-drevet prosjektil, innbefatter en fiitt mllende bakre endeenhet (14) som har et oddeantall finner (32). Og ha et oddeantall finner kan redusere oscillasjoner forårsaket av rotasjonen til den fiitt roterende halen. Dette kan danne en mer stabil plattform for en søker (22), slik som en ikke-kjølt fijktalpunktrekke eller annen bildedaimende infrarød (IIR) eller millimeterbølgeradiofrekvens (MMW) søker, i legemet til missiler. Minimalisering av oscillasjon ved å bruke et oddeantall finne kan også forenkle styring av missilet.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/444,653 US6869044B2 (en) | 2003-05-23 | 2003-05-23 | Missile with odd symmetry tail fins |
PCT/US2004/015795 WO2005022075A2 (en) | 2003-05-23 | 2004-05-20 | Missile with odd symmetry fins |
Publications (2)
Publication Number | Publication Date |
---|---|
NO20056127L true NO20056127L (no) | 2005-12-22 |
NO331135B1 NO331135B1 (no) | 2011-10-17 |
Family
ID=33450709
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO20056127A NO331135B1 (no) | 2003-05-23 | 2005-12-22 | Missil med oddetall symmetrifinner |
Country Status (9)
Country | Link |
---|---|
US (1) | US6869044B2 (no) |
EP (1) | EP1627200B1 (no) |
JP (1) | JP4740125B2 (no) |
AT (1) | ATE516477T1 (no) |
IL (1) | IL169563A (no) |
NO (1) | NO331135B1 (no) |
RU (1) | RU2395783C2 (no) |
WO (1) | WO2005022075A2 (no) |
ZA (1) | ZA200505388B (no) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
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US7530315B2 (en) | 2003-05-08 | 2009-05-12 | Lone Star Ip Holdings, Lp | Weapon and weapon system employing the same |
US6978717B1 (en) * | 2004-08-16 | 2005-12-27 | The United States Of America As Represented By The Secretary Of The Army | Infrared camera deployed by grenade launcher |
US7412930B2 (en) * | 2004-09-30 | 2008-08-19 | General Dynamic Ordnance And Tactical Systems, Inc. | Frictional roll control apparatus for a spinning projectile |
WO2006088687A1 (en) * | 2005-02-07 | 2006-08-24 | Bae Systems Information And Electronic Systems Integration Inc. | Optically guided munition |
US7354017B2 (en) * | 2005-09-09 | 2008-04-08 | Morris Joseph P | Projectile trajectory control system |
US7895946B2 (en) * | 2005-09-30 | 2011-03-01 | Lone Star Ip Holdings, Lp | Small smart weapon and weapon system employing the same |
US7690304B2 (en) | 2005-09-30 | 2010-04-06 | Lone Star Ip Holdings, Lp | Small smart weapon and weapon system employing the same |
SE528624C2 (sv) * | 2005-11-15 | 2007-01-09 | Bae Systems Bofors Ab | Underkalibrerad granat med lång räckvidd |
US8541724B2 (en) | 2006-09-29 | 2013-09-24 | Lone Star Ip Holdings, Lp | Small smart weapon and weapon system employing the same |
US8117955B2 (en) | 2006-10-26 | 2012-02-21 | Lone Star Ip Holdings, Lp | Weapon interface system and delivery platform employing the same |
US7800032B1 (en) * | 2006-11-30 | 2010-09-21 | Raytheon Company | Detachable aerodynamic missile stabilizing system |
US7755012B2 (en) * | 2007-01-10 | 2010-07-13 | Hr Textron, Inc. | Eccentric drive control actuation system |
GB0803282D0 (en) * | 2008-02-22 | 2008-04-02 | Qinetiq Ltd | Control of projectiles or the like |
US8158915B2 (en) * | 2008-10-02 | 2012-04-17 | Raytheon Company | Canard-centric missile support |
US8071928B2 (en) * | 2008-10-24 | 2011-12-06 | Raytheon Company | Projectile with filler material between fins and fuselage |
WO2010083517A1 (en) * | 2009-01-16 | 2010-07-22 | Bae Systems Land & Armaments L.P. | Munition and guidance navigation and control unit |
EP2433084B1 (en) * | 2009-05-19 | 2013-05-08 | Raytheon Company | Guided missile |
JP5626768B2 (ja) * | 2010-05-28 | 2014-11-19 | 株式会社Ihiエアロスペース | 飛翔体 |
IL207800B (en) * | 2010-08-25 | 2018-12-31 | Bae Systems Rokar Int Ltd | Control apparatus for guiding a cannon shell in flight and method of using same |
US8939084B2 (en) * | 2011-03-15 | 2015-01-27 | Anthony Joseph Cesaroni | Surface skimming munition |
US9068803B2 (en) | 2011-04-19 | 2015-06-30 | Lone Star Ip Holdings, Lp | Weapon and weapon system employing the same |
US20140312160A1 (en) * | 2011-06-07 | 2014-10-23 | Raytheon Company | Flight vehicles including scribed frangible seals and methods for the manufacture thereof |
US8816261B1 (en) | 2011-06-29 | 2014-08-26 | Raytheon Company | Bang-bang control using tangentially mounted surfaces |
SE535991C2 (sv) * | 2011-07-07 | 2013-03-19 | Bae Systems Bofors Ab | Rotationsstabiliserad styrbar projektil och förfarande därför |
KR101389133B1 (ko) | 2013-10-14 | 2014-04-25 | 엘아이지넥스원 주식회사 | 유도조종장치 |
WO2015179101A2 (en) * | 2014-04-30 | 2015-11-26 | Bae Systems Land & Armaments L.P. | Gun launched munition with strakes |
US9464876B2 (en) * | 2014-05-30 | 2016-10-11 | General Dynamics Ordnance and Tacital Systems, Inc. | Trajectory modification of a spinning projectile by controlling the roll orientation of a decoupled portion of the projectile that has actuated aerodynamic surfaces |
US9410779B1 (en) * | 2014-09-25 | 2016-08-09 | The United States Of America As Represented By The Secretary Of The Army | Breakaway fin ring for projectile |
US10254097B2 (en) | 2015-04-15 | 2019-04-09 | Raytheon Company | Shape memory alloy disc vent cover release |
FR3041744B1 (fr) * | 2015-09-29 | 2018-08-17 | Nexter Munitions | Projectile d'artillerie ayant une phase pilotee. |
US11555679B1 (en) | 2017-07-07 | 2023-01-17 | Northrop Grumman Systems Corporation | Active spin control |
US11578956B1 (en) | 2017-11-01 | 2023-02-14 | Northrop Grumman Systems Corporation | Detecting body spin on a projectile |
US11300389B1 (en) * | 2018-05-04 | 2022-04-12 | The United States Of America As Represented By The Secretary Of The Army | Slip baseplate |
KR101981625B1 (ko) * | 2018-10-16 | 2019-09-02 | 엘아이지넥스원 주식회사 | 레이저를 이용한 금속 접합방법 및 그 방법을 이용하여 생성된 부속품을 포함하는 고속 발사체 |
DE102020105188B4 (de) | 2020-02-27 | 2023-08-31 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Flugkörper-Finnenausklappeinrichtung, Flugkörper und Verfahren zum Betrieb eines Flugkörpers |
US11555678B2 (en) | 2020-06-01 | 2023-01-17 | Raytheon Company | Small body dynamics control method |
US11543220B2 (en) * | 2020-06-01 | 2023-01-03 | Raytheon Company | Small body dynamics control method |
US11573069B1 (en) | 2020-07-02 | 2023-02-07 | Northrop Grumman Systems Corporation | Axial flux machine for use with projectiles |
SE2100079A1 (sv) * | 2021-05-19 | 2022-11-20 | Bae Systems Bofors Ab | Projektil samt tändrör med fena |
CN114234734A (zh) * | 2021-12-24 | 2022-03-25 | 中国工程物理研究院总体工程研究所 | 一种微小型导弹气动布局 |
CN114432625B (zh) * | 2022-02-16 | 2022-10-04 | 宇称智控(北京)科技有限公司 | 一种远距离精确制导灭火弹 |
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US3177809A (en) * | 1962-07-24 | 1965-04-13 | Budd Co | Semi-fixed artillery round |
US5439188A (en) * | 1964-09-04 | 1995-08-08 | Hughes Missile Systems Company | Control system |
US4522356A (en) * | 1973-11-12 | 1985-06-11 | General Dynamics, Pomona Division | Multiple target seeking clustered munition and system |
DE2520238C3 (de) * | 1975-05-07 | 1979-09-27 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Um seine Längsachse rollendes lenkbares Geschoß |
FR2321723A1 (fr) * | 1975-07-29 | 1977-03-18 | Thomson Brandt | Systeme de controle d'attitude et engin equipe d'un tel systeme |
DE3009775A1 (de) * | 1980-03-14 | 1981-10-01 | Mauser-Werke Oberndorf Gmbh, 7238 Oberndorf | Fluegelstabilisiertes pfeilgeschoss |
US4752052A (en) * | 1986-12-17 | 1988-06-21 | The Marquardt Company | Projectile |
FR2655720A1 (fr) * | 1989-12-08 | 1991-06-14 | Thomson Brandt Armements | Aile galbee deployable pour engin volant. |
US5029773A (en) * | 1990-01-24 | 1991-07-09 | Grumman Aerospace Corporation | Cable towed decoy with collapsible fins |
US5323987A (en) * | 1993-03-04 | 1994-06-28 | The Boeing Company | Missile seeker system and method |
US6126109A (en) * | 1997-04-11 | 2000-10-03 | Raytheon Company | Unlocking tail fin assembly for guided projectiles |
US6144030A (en) | 1997-10-28 | 2000-11-07 | Raytheon Company | Advanced small pixel high fill factor uncooled focal plane array |
US6100841A (en) | 1998-06-19 | 2000-08-08 | Raytheon Company | Radio frequency receiving circuit |
US6247666B1 (en) * | 1998-07-06 | 2001-06-19 | Lockheed Martin Corporation | Method and apparatus for non-propulsive fin control in an air or sea vehicle using planar actuation |
SE518657C2 (sv) * | 2000-07-03 | 2002-11-05 | Bofors Defence Ab | Fenstabiliserad styrbar projektil |
US6392213B1 (en) * | 2000-10-12 | 2002-05-21 | The Charles Stark Draper Laboratory, Inc. | Flyer assembly |
US6443391B1 (en) * | 2001-05-17 | 2002-09-03 | The United States Of America As Represented By The Secretary Of The Army | Fin-stabilized projectile with improved aerodynamic performance |
US6588700B2 (en) * | 2001-10-16 | 2003-07-08 | Raytheon Company | Precision guided extended range artillery projectile tactical base |
US6571715B1 (en) * | 2002-03-11 | 2003-06-03 | Raytheon Company | Boot mechanism for complex projectile base survival |
US6695252B1 (en) * | 2002-09-18 | 2004-02-24 | Raytheon Company | Deployable fin projectile with outflow device |
-
2003
- 2003-05-23 US US10/444,653 patent/US6869044B2/en not_active Expired - Lifetime
-
2004
- 2004-05-20 EP EP04801953A patent/EP1627200B1/en not_active Expired - Lifetime
- 2004-05-20 AT AT04801953T patent/ATE516477T1/de not_active IP Right Cessation
- 2004-05-20 WO PCT/US2004/015795 patent/WO2005022075A2/en active Search and Examination
- 2004-05-20 JP JP2006514908A patent/JP4740125B2/ja not_active Expired - Lifetime
- 2004-05-20 ZA ZA200505388A patent/ZA200505388B/en unknown
- 2004-05-20 RU RU2005140376/02A patent/RU2395783C2/ru not_active IP Right Cessation
-
2005
- 2005-07-06 IL IL169563A patent/IL169563A/en active IP Right Grant
- 2005-12-22 NO NO20056127A patent/NO331135B1/no not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
JP4740125B2 (ja) | 2011-08-03 |
WO2005022075A3 (en) | 2005-06-02 |
RU2395783C2 (ru) | 2010-07-27 |
JP2006526132A (ja) | 2006-11-16 |
US20040232278A1 (en) | 2004-11-25 |
ATE516477T1 (de) | 2011-07-15 |
EP1627200B1 (en) | 2011-07-13 |
IL169563A (en) | 2011-05-31 |
WO2005022075A2 (en) | 2005-03-10 |
EP1627200A2 (en) | 2006-02-22 |
RU2005140376A (ru) | 2006-05-10 |
ZA200505388B (en) | 2006-09-27 |
NO331135B1 (no) | 2011-10-17 |
WO2005022075B1 (en) | 2005-09-15 |
US6869044B2 (en) | 2005-03-22 |
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MM1K | Lapsed by not paying the annual fees |