NO327539B1 - Halestabilisert styrbart missil - Google Patents

Halestabilisert styrbart missil Download PDF

Info

Publication number
NO327539B1
NO327539B1 NO20030005A NO20030005A NO327539B1 NO 327539 B1 NO327539 B1 NO 327539B1 NO 20030005 A NO20030005 A NO 20030005A NO 20030005 A NO20030005 A NO 20030005A NO 327539 B1 NO327539 B1 NO 327539B1
Authority
NO
Norway
Prior art keywords
missile
tail
ball bearing
main part
bearing
Prior art date
Application number
NO20030005A
Other languages
English (en)
Norwegian (no)
Other versions
NO20030005D0 (no
NO20030005L (no
Inventor
Stig Johnsson
Ulf Hellman
Ulf Holmqvist
Original Assignee
Bae Systems Bofors Ab
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 Bae Systems Bofors Ab filed Critical Bae Systems Bofors Ab
Publication of NO20030005D0 publication Critical patent/NO20030005D0/no
Publication of NO20030005L publication Critical patent/NO20030005L/no
Publication of NO327539B1 publication Critical patent/NO327539B1/no

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
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/16—Wrap-around fins
    • 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
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • 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
    • F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
    • F42B10/38—Range-increasing arrangements
    • F42B10/40—Range-increasing arrangements with combustion of a slow-burning charge, e.g. fumers, base-bleed projectiles

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)
  • Toys (AREA)
NO20030005A 2000-07-03 2003-01-02 Halestabilisert styrbart missil NO327539B1 (no)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE0002480A SE518657C2 (sv) 2000-07-03 2000-07-03 Fenstabiliserad styrbar projektil
PCT/SE2001/001333 WO2002006761A1 (fr) 2000-07-03 2001-06-13 Missile a guidage a derive stabilisee

Publications (3)

Publication Number Publication Date
NO20030005D0 NO20030005D0 (no) 2003-01-02
NO20030005L NO20030005L (no) 2003-02-19
NO327539B1 true NO327539B1 (no) 2009-08-03

Family

ID=20280328

Family Applications (1)

Application Number Title Priority Date Filing Date
NO20030005A NO327539B1 (no) 2000-07-03 2003-01-02 Halestabilisert styrbart missil

Country Status (11)

Country Link
US (1) US6796525B2 (fr)
EP (1) EP1299688B1 (fr)
AU (1) AU2001274734A1 (fr)
CA (1) CA2414793C (fr)
DE (1) DE60142740D1 (fr)
ES (1) ES2347415T3 (fr)
IL (2) IL153629A0 (fr)
NO (1) NO327539B1 (fr)
SE (1) SE518657C2 (fr)
WO (1) WO2002006761A1 (fr)
ZA (1) ZA200210383B (fr)

Families Citing this family (45)

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SE521445C2 (sv) * 2001-03-20 2003-11-04 Bofors Defence Ab Sätt att synkronisera fenutfällningen vid en fenstabiliserad artillerigranat samt en i enlighet därmed utformad artillerigranat
GB0111171D0 (en) * 2001-05-08 2001-06-27 Special Cartridge Company Ltd Projictile
DE10205043C5 (de) * 2002-02-07 2010-06-17 Diehl Bgt Defence Gmbh & Co. Kg Aus einem Rohr zu verschließender Flugkörper mit überkalibrigem Leitwerk
US6869044B2 (en) * 2003-05-23 2005-03-22 Raytheon Company Missile with odd symmetry tail fins
SE527067C2 (sv) * 2003-12-01 2005-12-13 Atlas Copco Tools Ab Impulsmutterdragare med vinkelavkännande organ
SE526964C2 (sv) * 2003-12-29 2005-11-29 Atlas Copco Tools Ab Metod för funktionsstyrning av en pneumatisk impulsmutterdragare samt ett kraftskruvdragarsystem
FR2882430B1 (fr) * 2005-02-21 2007-03-30 Giat Ind Sa Projectile d'artillerie comportant une ceinture
DE102005035829B4 (de) * 2005-07-30 2007-06-06 Diehl Bgt Defence Gmbh & Co. Kg Rollentkoppeltes Leitwerk für ein Artilleriegeschoss
SE528624C2 (sv) * 2005-11-15 2007-01-09 Bae Systems Bofors Ab Underkalibrerad granat med lång räckvidd
US7829830B1 (en) * 2007-10-19 2010-11-09 Woodward Hrt, Inc. Techniques for controlling access through a slot on a projectile
EP2304383A4 (fr) * 2008-07-09 2014-01-01 Bae Sys Land & Armaments Lp Palier d'isolation rouleau
JP4882099B2 (ja) * 2008-09-25 2012-02-22 防衛省技術研究本部長 飛しょう体
KR101069245B1 (ko) 2009-05-19 2011-10-04 국방과학연구소 날개 조립체 및 그를 구비하는 비행체 발사 장치
US8026465B1 (en) * 2009-05-20 2011-09-27 The United States Of America As Represented By The Secretary Of The Navy Guided fuse with variable incidence panels
US8312813B2 (en) * 2009-07-31 2012-11-20 Raytheon Company Deployable fairing and method for reducing aerodynamic drag on a gun-launched artillery shell
DE102010019384A1 (de) 2010-05-04 2011-11-10 Rheinmetall Waffe Munition Gmbh Geschoss mit einem Flügelleitwerk
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
RU2448321C1 (ru) * 2010-11-26 2012-04-20 Федеральное Государственное унитарное предприятие "Государственное научно-производственное предприятие "Сплав" Реактивный снаряд
US8552349B1 (en) * 2010-12-22 2013-10-08 Interstate Electronics Corporation Projectile guidance kit
SE535991C2 (sv) * 2011-07-07 2013-03-19 Bae Systems Bofors Ab Rotationsstabiliserad styrbar projektil och förfarande därför
US8530809B2 (en) 2011-08-03 2013-09-10 Raytheon Company Ring gear control actuation system for air-breathing rocket motors
US8866057B2 (en) * 2011-10-17 2014-10-21 Raytheon Company Fin deployment method and apparatus
US8596199B2 (en) * 2012-02-14 2013-12-03 Simmonds Precision Products, Inc. Projectile bearing system
RU2502042C1 (ru) * 2012-05-22 2013-12-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Тульский государственный университет" (ТулГУ) Управляемый реактивный снаряд
US9593922B2 (en) * 2013-03-14 2017-03-14 Bae Systems Land & Armaments L.P. Fin deployment system
RU2544447C1 (ru) * 2014-01-22 2015-03-20 Виктор Андреевич Павлов Способ полета вращающейся ракеты
RU2544446C1 (ru) * 2014-01-22 2015-03-20 Виктор Андреевич Павлов Вращающаяся крылатая ракета
RU2542692C1 (ru) * 2014-02-03 2015-02-20 Открытое акционерное общество "Конструкторское бюро приборостроения им. академика А.Г. Шипунова" Управляемый снаряд
RU2541552C1 (ru) * 2014-03-27 2015-02-20 Открытое акционерное общество "Научно-производственное объединение "СПЛАВ" Блок системы управления реактивного снаряда, запускаемого из трубчатой направляющей
RU2540291C1 (ru) * 2014-03-27 2015-02-10 Открытое акционерное общество "Научно-производственное объединение "СПЛАВ" Ракетная часть со стабилизатором реактивного снаряда
WO2015179101A2 (fr) * 2014-04-30 2015-11-26 Bae Systems Land & Armaments L.P. Munition tirée par un pistolet et dotée de listons
RU2563302C1 (ru) * 2014-09-03 2015-09-20 Открытое акционерное общество "Научно-производственное объединение "СПЛАВ" Хвостовой блок управляемого реактивного снаряда, запускаемого из трубчатой направляющей
FR3041744B1 (fr) * 2015-09-29 2018-08-17 Nexter Munitions Projectile d'artillerie ayant une phase pilotee.
RU2713546C2 (ru) * 2017-02-02 2020-02-05 Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации Крылатая ракета и способ ее боевого применения
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
RU2671015C1 (ru) * 2017-11-27 2018-10-29 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Способ управления полетом баллистического летательного аппарата
RU2722329C1 (ru) * 2019-07-25 2020-05-29 Акционерное общество "Машиностроительное конструкторское бюро "Факел" имени Академика П.Д. Грушина" Ракета
CN111854541A (zh) * 2020-06-23 2020-10-30 西北工业大学 一种折叠翼微型导弹平台
US11573069B1 (en) 2020-07-02 2023-02-07 Northrop Grumman Systems Corporation Axial flux machine for use with projectiles
TR202013182A2 (tr) * 2020-08-20 2022-03-21 Roketsan Roket Sanayi Ve Ticaret Anonim Sirketi Dönü yalitimli rulman komplesi̇
DE102020006629A1 (de) * 2020-10-29 2022-05-05 Diehl Defence Gmbh & Co. Kg Lagereinheit für ein Geschoss und Geschoss
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
CN115355769B (zh) * 2022-08-23 2023-12-29 中国空气动力研究与发展中心高速空气动力研究所 一种变静稳定性战术导弹气动布局及其应用

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US2611317A (en) * 1946-03-08 1952-09-23 Africano Alfred Rotating nozzle for rockets
US2981188A (en) * 1955-10-10 1961-04-25 Henry S Lipinski Spin-stabilized projectile with nonrotating shaped charge
SE377719C (sv) * 1970-04-30 1978-11-09 Hawker Siddeley Dynamics Ltd Anordning for styrning och framatdrivande av suft- eller rymdfarkost
CH574095A5 (fr) * 1973-12-21 1976-03-31 Oerlikon Buehrle Ag
US4373688A (en) * 1981-01-19 1983-02-15 The United States Of America As Represented By The Secretary Of The Army Canard drive mechanism latch for guided projectile
US4690350A (en) * 1985-12-19 1987-09-01 Raytheon Company Despinning mechanism
US4752052A (en) * 1986-12-17 1988-06-21 The Marquardt Company Projectile
GB2265443B (en) 1988-04-14 1994-03-23 British Aerospace Fin assembly for a projectile
JPH0250097A (ja) * 1988-08-09 1990-02-20 Mitsubishi Electric Corp 誘導飛しょう体
US6126109A (en) * 1997-04-11 2000-10-03 Raytheon Company Unlocking tail fin assembly for guided projectiles
NO308716B1 (no) * 1999-06-04 2000-10-16 Nammo Raufoss As Fremførings- og lÕsemekanisme i missil
US6474594B1 (en) * 2001-05-11 2002-11-05 Raytheon Company Output shaft assembly for a missile control actuation unit

Also Published As

Publication number Publication date
CA2414793C (fr) 2009-09-15
CA2414793A1 (fr) 2002-01-24
ZA200210383B (en) 2004-02-13
US20040011920A1 (en) 2004-01-22
NO20030005D0 (no) 2003-01-02
US6796525B2 (en) 2004-09-28
ES2347415T3 (es) 2010-10-29
SE518657C2 (sv) 2002-11-05
SE0002480L (sv) 2002-01-04
IL153629A (en) 2008-07-08
IL153629A0 (en) 2003-07-06
DE60142740D1 (de) 2010-09-16
EP1299688B1 (fr) 2010-08-04
WO2002006761A1 (fr) 2002-01-24
AU2001274734A1 (en) 2002-01-30
SE0002480D0 (sv) 2000-07-03
EP1299688A1 (fr) 2003-04-09
NO20030005L (no) 2003-02-19

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