WO2008143707A3 - Course correcting fuze - Google Patents
Course correcting fuze Download PDFInfo
- Publication number
- WO2008143707A3 WO2008143707A3 PCT/US2007/086798 US2007086798W WO2008143707A3 WO 2008143707 A3 WO2008143707 A3 WO 2008143707A3 US 2007086798 W US2007086798 W US 2007086798W WO 2008143707 A3 WO2008143707 A3 WO 2008143707A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- fuze
- artillery
- fins
- course correcting
- power
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42C—AMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
- F42C19/00—Details of fuzes
-
- 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
- F42B10/48—Range-reducing, destabilising or braking arrangements, e.g. impact-braking arrangements; Fall-retarding means, e.g. balloons, rockets for braking or fall-retarding
- F42B10/54—Spin braking means
-
- 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
- F42B10/62—Steering by movement of flight surfaces
- F42B10/64—Steering by movement of flight surfaces of fins
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Fuel Cell (AREA)
- Motorcycle And Bicycle Frame (AREA)
Abstract
A course correcting fuze for use in artillery warheads or other military projectiles. Mechanisms are provided whereby air brake fins and spin control fins can be deployed and retracted under computer control during projectile flight to improve targeting accuracy. Power is supplied by an innovative fuel cell module that allows for long term storage of the fuze, rapid activated during launch of the artillery shell, and sufficient power for use by the electronics and actuator motors during operation.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US87347806P | 2006-12-07 | 2006-12-07 | |
US60/873,478 | 2006-12-07 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2008143707A2 WO2008143707A2 (en) | 2008-11-27 |
WO2008143707A3 true WO2008143707A3 (en) | 2009-01-15 |
Family
ID=40032320
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2007/086798 WO2008143707A2 (en) | 2006-12-07 | 2007-12-07 | Course correcting fuze |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2008143707A2 (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
US8319164B2 (en) | 2009-10-26 | 2012-11-27 | Nostromo, Llc | Rolling projectile with extending and retracting canards |
SE540036C2 (en) * | 2013-10-10 | 2018-03-06 | Bae Systems Bofors Ab | Fen-precipitation mechanism and method for fen-precipitation |
KR101421127B1 (en) * | 2014-01-15 | 2014-07-22 | 국방과학연구소 | Course correction fuze |
SE542272C2 (en) * | 2017-11-28 | 2020-03-31 | Bae Systems Bofors Ab | Spark plug with reversible air brake |
CN109753750B (en) * | 2019-01-16 | 2023-01-10 | 北京航天嘉诚精密科技发展有限公司 | Sleeve assembly for installing trajectory correction fuse in fixed rudder trajectory correction fuse semi-physical simulation system |
US11835319B2 (en) * | 2021-06-07 | 2023-12-05 | The Boeing Company | Guided projectile and countermeasure systems and methods for use therewith |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5585592A (en) * | 1994-05-31 | 1996-12-17 | Motorola, Inc. | Shock tolerant fuze |
US6057915A (en) * | 1996-06-21 | 2000-05-02 | Thermotrex Corporation | Projectile tracking system |
US6378801B1 (en) * | 1998-08-11 | 2002-04-30 | Nekton Technologies, Inc. | Devices and methods for orienting and steering in three-dimensional space |
US6762291B1 (en) * | 1999-03-16 | 2004-07-13 | Exelixis, Inc. | Insect p53 tumor suppressor genes and proteins |
-
2007
- 2007-12-07 WO PCT/US2007/086798 patent/WO2008143707A2/en active Application Filing
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5585592A (en) * | 1994-05-31 | 1996-12-17 | Motorola, Inc. | Shock tolerant fuze |
US6057915A (en) * | 1996-06-21 | 2000-05-02 | Thermotrex Corporation | Projectile tracking system |
US6378801B1 (en) * | 1998-08-11 | 2002-04-30 | Nekton Technologies, Inc. | Devices and methods for orienting and steering in three-dimensional space |
US6762291B1 (en) * | 1999-03-16 | 2004-07-13 | Exelixis, Inc. | Insect p53 tumor suppressor genes and proteins |
Also Published As
Publication number | Publication date |
---|---|
WO2008143707A2 (en) | 2008-11-27 |
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