ZA200905069B - Guided missile with a sleeve for mountig a guiding system - Google Patents
Guided missile with a sleeve for mountig a guiding systemInfo
- Publication number
- ZA200905069B ZA200905069B ZA200905069A ZA200905069A ZA200905069B ZA 200905069 B ZA200905069 B ZA 200905069B ZA 200905069 A ZA200905069 A ZA 200905069A ZA 200905069 A ZA200905069 A ZA 200905069A ZA 200905069 B ZA200905069 B ZA 200905069B
- Authority
- ZA
- South Africa
- Prior art keywords
- sleeve
- guiding system
- nose
- mountig
- guided missile
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/01—Arrangements thereon for guidance or control
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Forklifts And Lifting Vehicles (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
- Chair Legs, Seat Parts, And Backrests (AREA)
- Toys (AREA)
- Steering Devices For Bicycles And Motorcycles (AREA)
- Vibration Dampers (AREA)
Abstract
The projectile (1) has a cylindrical body (10) terminated at its front by an ogive shaped nose (20). A removable cylindrical sleeve (30) allows assembly of a guiding system e.g. laser guiding equipment, at the front of the body, and is fixed on a cylindrical connection part (25) of the nose, where the guiding system conforms to OTAN standard. The connection part carries an outer thread co-operating with an inner thread formed in a rear part (31) of the sleeve. The sleeve is made of low-resilience material e.g. brittle steel, and the nose is made of rigid material e.g. steel.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0655787A FR2910613B1 (en) | 2006-12-21 | 2006-12-21 | GUIDE PROJECTILE HAVING A SLEEVE FOR MOUNTING A GUIDE SYSTEM |
Publications (1)
Publication Number | Publication Date |
---|---|
ZA200905069B true ZA200905069B (en) | 2010-07-28 |
Family
ID=38476853
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ZA200905069A ZA200905069B (en) | 2006-12-21 | 2009-07-10 | Guided missile with a sleeve for mountig a guiding system |
Country Status (8)
Country | Link |
---|---|
EP (1) | EP2095060B1 (en) |
KR (1) | KR20090112653A (en) |
CN (1) | CN101578493B (en) |
AT (1) | ATE512347T1 (en) |
BR (1) | BRPI0720585A2 (en) |
FR (1) | FR2910613B1 (en) |
WO (1) | WO2008102069A2 (en) |
ZA (1) | ZA200905069B (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2158443B1 (en) * | 2007-06-08 | 2014-11-12 | Raytheon Company | Methods and apparatus for attachment adapter for a projectile |
US8291827B2 (en) | 2009-09-28 | 2012-10-23 | Raytheon Company | Rocket guidance adapter |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6254031B1 (en) * | 1994-08-24 | 2001-07-03 | Lockhead Martin Corporation | Precision guidance system for aircraft launched bombs |
DK1038152T3 (en) * | 1997-12-11 | 2004-12-13 | Lockheed Corp | Clothed airplane bomb |
US6276277B1 (en) * | 1999-04-22 | 2001-08-21 | Lockheed Martin Corporation | Rocket-boosted guided hard target penetrator |
AUPQ776300A0 (en) * | 2000-05-25 | 2000-08-10 | Metal Storm Limited | Missile control |
FR2845763B1 (en) * | 2002-10-11 | 2006-12-01 | Tda Armements Sas | AUTONOMOUS GUIDING SYSTEM FOR ARTILLERY MUNITION AND GUIDED ARTILLERY MUNITION |
CN2656930Y (en) * | 2003-12-04 | 2004-11-17 | 罗林桂 | 78 type platform force less cannon inner bore cannon and its analogue cannon ball |
DE102005039902A1 (en) * | 2005-02-04 | 2006-08-10 | Rheinmetall Waffe Munition Gmbh | Device for increasing the precision of tail-wing stabilized ammunition |
-
2006
- 2006-12-21 FR FR0655787A patent/FR2910613B1/en not_active Expired - Fee Related
-
2007
- 2007-12-20 KR KR1020097014835A patent/KR20090112653A/en not_active Application Discontinuation
- 2007-12-20 WO PCT/FR2007/002142 patent/WO2008102069A2/en active Application Filing
- 2007-12-20 CN CN2007800472388A patent/CN101578493B/en not_active Expired - Fee Related
- 2007-12-20 AT AT07872426T patent/ATE512347T1/en not_active IP Right Cessation
- 2007-12-20 BR BRPI0720585-6A2A patent/BRPI0720585A2/en not_active IP Right Cessation
- 2007-12-20 EP EP07872426A patent/EP2095060B1/en not_active Not-in-force
-
2009
- 2009-07-10 ZA ZA200905069A patent/ZA200905069B/en unknown
Also Published As
Publication number | Publication date |
---|---|
WO2008102069A8 (en) | 2009-07-30 |
KR20090112653A (en) | 2009-10-28 |
WO2008102069A3 (en) | 2008-10-30 |
CN101578493B (en) | 2012-08-29 |
ATE512347T1 (en) | 2011-06-15 |
EP2095060A2 (en) | 2009-09-02 |
FR2910613B1 (en) | 2009-10-02 |
EP2095060B1 (en) | 2011-06-08 |
CN101578493A (en) | 2009-11-11 |
FR2910613A1 (en) | 2008-06-27 |
BRPI0720585A2 (en) | 2014-10-07 |
WO2008102069A2 (en) | 2008-08-28 |
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