NO20030004L - Halestabilisert rakett - Google Patents

Halestabilisert rakett

Info

Publication number: NO20030004L
Authority: NO; Norway
Prior art keywords: stabilized rocket; tail; tail stabilized; rocket; stabilized
Prior art date: 2000-07-03

Application number

NO20030004A

Other languages

English (en)

Norwegian (no)

Other versions

NO20030004D0 (no

Inventor

Stig Johnsson

Ulf Hellman

Ulf Holmqvist

Original Assignee

Bofors Defence 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.)

2000-07-03

Filing date

2003-01-02

Publication date

2003-02-11

2003-01-02 Application filed by Bofors Defence Ab filed Critical Bofors Defence Ab

2003-01-02 Publication of NO20030004D0 publication Critical patent/NO20030004D0/no

2003-02-11 Publication of NO20030004L publication Critical patent/NO20030004L/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
- F42B10/18—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel using a longitudinally slidable support member
- 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
- F42B10/32—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)
Automotive Seat Belt Assembly (AREA)
Toys (AREA)
Prostheses (AREA)
Braking Systems And Boosters (AREA)
Air Bags (AREA)

NO20030004A 2000-07-03 2003-01-02 Halestabilisert rakett NO20030004L (no)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
SE0002487A SE518656C2 (sv)	2000-07-03	2000-07-03	Fenstabiliserad artillerigranat
PCT/SE2001/001332 WO2002006760A1 (en)	2000-07-03	2001-06-13	Fin-stabilized shell

Publications (2)

Publication Number	Publication Date
NO20030004D0 NO20030004D0 (no)	2003-01-02
NO20030004L true NO20030004L (no)	2003-02-11

Family

ID=20280335

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
NO20030004A NO20030004L (no)	2000-07-03	2003-01-02	Halestabilisert rakett

Country Status (11)

Country	Link
US (1)	US6886775B2 (sv)
EP (1)	EP1297293B1 (sv)
AU (1)	AU2001274733A1 (sv)
CA (1)	CA2415090C (sv)
DE (1)	DE60140540D1 (sv)
ES (1)	ES2336541T3 (sv)
IL (2)	IL153628A0 (sv)
NO (1)	NO20030004L (sv)
SE (1)	SE518656C2 (sv)
WO (1)	WO2002006760A1 (sv)
ZA (1)	ZA200210384B (sv)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB0111171D0 (en) *	2001-05-08	2001-06-27	Special Cartridge Company Ltd	Projictile
DE10130383A1 (de) *	2001-06-23	2003-01-09	Diehl Munitionssysteme Gmbh	Artillerie-Projektil mit austauschbarer Nutzlast
US7415931B2 (en) *	2005-07-20	2008-08-26	Textron Systems Corporation	Methods and apparatus for active deployment of a samara wing
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
US8193476B2 (en) *	2008-06-13	2012-06-05	Raytheon Company	Solid-fuel pellet thrust and control actuation system to maneuver a flight vehicle
US8158915B2 (en) *	2008-10-02	2012-04-17	Raytheon Company	Canard-centric missile support
WO2011014806A1 (en) *	2009-07-31	2011-02-03	Raytheon Company	Deployable fairing and method for reducing aerodynamic drag on a gun-launched artillery shell
DK2475575T3 (en) *	2009-09-09	2017-12-11	Aerovironment Inc	UAV with deployable wings and flight control method
DE102009057682A1 (de)	2009-12-04	2011-06-09	Frank Lehnen	Widerstandsstabilisiertes, flügelloses und angetriebenes Wuchtgeschoss
DE202009016713U1 (de)	2009-12-04	2010-04-08	Lehnen, Frank	Widerstandsstabilisiertes, flügelloses und angetriebenes Wuchtgeschoss
US8933383B2 (en) *	2010-09-01	2015-01-13	The United States Of America As Represented By The Secretary Of The Army	Method and apparatus for correcting the trajectory of a fin-stabilized, ballistic projectile using canards
WO2015179101A2 (en) *	2014-04-30	2015-11-26	Bae Systems Land & Armaments L.P.	Gun launched munition with strakes
US10184762B2 (en)	2015-12-01	2019-01-22	Raytheon Company	Base drag reduction fairing using shape memory materials
US11796291B2 (en) *	2022-01-11	2023-10-24	Raytheon Company	Effector having morphing airframe and method
FI130317B (sv) *	2022-06-02	2023-06-16	Moviator Oy	Projektil
IL294415B2 (en)	2022-06-29	2023-10-01	Israel Aerospace Ind Ltd	Air receiver module for the missile

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE2264338A1 (de) *	1972-12-30	1974-07-04	Dynamit Nobel Ag	Ausklappbares leitwerk, insbesondere fuer raketen
US3819132A (en) *	1973-02-21	1974-06-25	Sarmac Sa	Self propelled projectile with fins
SE428058B (sv) *	1981-10-08	1983-05-30	Foerenade Fabriksverken	Styrverk for projektil
DE3344402A1 (de)	1983-12-08	1985-06-13	Diehl GmbH & Co, 8500 Nürnberg	Flugkoerper
GB2265443B (en) *	1988-04-14	1994-03-23	British Aerospace	Fin assembly for a projectile
US4944226A (en) *	1988-08-19	1990-07-31	General Dynamics Corp., Pomona Div.	Expandable telescoped missile airframe
USH905H (en) *	1990-09-13	1991-04-02	The United States Of America As Represented By The Secretary Of The Army	Fin assembly
US6126109A (en) *	1997-04-11	2000-10-03	Raytheon Company	Unlocking tail fin assembly for guided projectiles
DE10015514B4 (de) *	2000-03-30	2007-10-04	Rheinmetall Waffe Munition Gmbh	Flügelstabilisiertes Geschoß
US6571715B1 (en) *	2002-03-11	2003-06-03	Raytheon Company	Boot mechanism for complex projectile base survival

2000
- 2000-07-03 SE SE0002487A patent/SE518656C2/sv not_active IP Right Cessation
2001
- 2001-06-13 CA CA002415090A patent/CA2415090C/en not_active Expired - Fee Related
- 2001-06-13 AU AU2001274733A patent/AU2001274733A1/en not_active Abandoned
- 2001-06-13 US US10/312,667 patent/US6886775B2/en not_active Expired - Lifetime
- 2001-06-13 IL IL15362801A patent/IL153628A0/xx unknown
- 2001-06-13 WO PCT/SE2001/001332 patent/WO2002006760A1/en active Application Filing
- 2001-06-13 EP EP01941374A patent/EP1297293B1/en not_active Expired - Lifetime
- 2001-06-13 DE DE60140540T patent/DE60140540D1/de not_active Expired - Lifetime
- 2001-06-13 ES ES01941374T patent/ES2336541T3/es not_active Expired - Lifetime
2002
- 2002-12-20 ZA ZA200210384A patent/ZA200210384B/en unknown
- 2002-12-24 IL IL153628A patent/IL153628A/en not_active IP Right Cessation
2003
- 2003-01-02 NO NO20030004A patent/NO20030004L/no unknown

Also Published As

Publication number	Publication date
IL153628A0 (en)	2003-07-06
CA2415090A1 (en)	2002-01-24
SE0002487L (sv)	2002-01-04
NO20030004D0 (no)	2003-01-02
ES2336541T3 (es)	2010-04-14
US20040011919A1 (en)	2004-01-22
EP1297293A1 (en)	2003-04-02
ZA200210384B (en)	2004-02-10
EP1297293B1 (en)	2009-11-18
CA2415090C (en)	2009-02-10
WO2002006760A1 (en)	2002-01-24
AU2001274733A1 (en)	2002-01-30
SE0002487D0 (sv)	2000-07-03
DE60140540D1 (de)	2009-12-31
US6886775B2 (en)	2005-05-03
SE518656C2 (sv)	2002-11-05
IL153628A (en)	2013-05-30

Publication	Publication Date	Title
NO20030005D0 (no)	2003-01-02	Halestabilisert styrbart missil
DE50105915D1 (de)	2005-05-19	Schutzhülle
NO20013926L (no)	2002-02-15	Undersjöisk intervensjon
DE60111319D1 (de)	2005-07-14	Pyrotechnischer Aktuator
DE60124596D1 (de)	2006-12-28	Durchgangstülle
NL1019181A1 (nl)	2002-04-18	Gestabiliseerd metalloceen-polypropeen.
NO20030004D0 (no)	2003-01-02	Halestabilisert rakett
DE60128630D1 (de)	2007-07-12	Durchführungstülle
DE60119664D1 (de)	2006-06-22	Kabelbaum
NO20021020L (no)	2002-05-23	Kanalgjennomlöpende farkost
DE60022950D1 (de)	2006-02-16	Feststoffraketentreibsatz
DE60122554D1 (de)	2006-10-05	Inline-druckgeber
NO20001294D0 (no)	2000-03-13	Måler for skyvekraft
DE59913732D1 (de)	2006-09-14	Flugkörper
DE50108077D1 (de)	2005-12-22	Gefechtskopf
NO20024322L (no)	2002-09-10	Sekvens
ATE385306T1 (de)	2008-02-15	Mauerzerbrechender gefechtskopf
DE60107637D1 (de)	2005-01-13	Kabelbaum
NO20005773D0 (no)	2000-11-14	Pyroteknisk struktur
DE69930998D1 (de)	2006-06-01	Treibmittel
DE60125897D1 (de)	2007-02-22	Raketendüse
DE60107525D1 (de)	2005-01-05	Durchführungstülle
NO20023723L (no)	2002-10-09	Drag
DE60112022D1 (de)	2005-08-25	Lenksäulenverkleidung
DE60102534D1 (de)	2004-05-06	Durchgangstülle