GB1188651A - Improvements in or relating to Missiles - Google Patents
Improvements in or relating to MissilesInfo
- Publication number
- GB1188651A GB1188651A GB848062A GB848062A GB1188651A GB 1188651 A GB1188651 A GB 1188651A GB 848062 A GB848062 A GB 848062A GB 848062 A GB848062 A GB 848062A GB 1188651 A GB1188651 A GB 1188651A
- Authority
- GB
- United Kingdom
- Prior art keywords
- missiles
- relating
- Prior art date
- Legal status (The legal status 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 status listed.)
- Expired
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
- F42B10/26—Stabilising arrangements using spin
-
- 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)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB848062A GB1188651A (en) | 1962-03-05 | 1962-03-05 | Improvements in or relating to Missiles |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB848062A GB1188651A (en) | 1962-03-05 | 1962-03-05 | Improvements in or relating to Missiles |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1188651A true GB1188651A (en) | 1970-04-22 |
Family
ID=9853275
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB848062A Expired GB1188651A (en) | 1962-03-05 | 1962-03-05 | Improvements in or relating to Missiles |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1188651A (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3776490A (en) * | 1971-08-20 | 1973-12-04 | Messerschmitt Boelkow Blohm | Missile with thrust vector and aerodynamic control |
EP0066715A2 (en) * | 1981-06-05 | 1982-12-15 | Hüls Troisdorf Aktiengesellschaft | Spin-stabilised training projectile |
US4624424A (en) * | 1984-11-07 | 1986-11-25 | The Boeing Company | On-board flight control drag actuator system |
US4699333A (en) * | 1984-11-07 | 1987-10-13 | The Boeing Company | On-board flight control panel system |
DE3915585A1 (en) * | 1989-05-12 | 1990-11-15 | Diehl Gmbh & Co | SUBMUNITION MISSILE |
FR2655722A1 (en) * | 1989-12-12 | 1991-06-14 | Aerospatiale | SUPERSONIC MISSILE WITH TORQUE DRIVING BY SPOUILERS. |
US5060574A (en) * | 1990-07-02 | 1991-10-29 | Honeywell Inc. | Projectile base plug with enhanced drag-producing separation capability |
GB2244118A (en) * | 1990-03-10 | 1991-11-20 | Atomic Energy Authority Uk | Reconnaissance device. |
DE4412687A1 (en) * | 1994-04-13 | 1995-10-19 | Diehl Gmbh & Co | Projectile remotely controllable using a laser beam |
WO1998046962A1 (en) * | 1997-04-11 | 1998-10-22 | Raytheon Company | Unlocking tail fin assembly for guided projectiles |
US6559370B1 (en) * | 2002-08-06 | 2003-05-06 | The United States Of America As Represented By The Secretary Of The Navy | Submarine countermeasure vehicle with folding propeller |
-
1962
- 1962-03-05 GB GB848062A patent/GB1188651A/en not_active Expired
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3776490A (en) * | 1971-08-20 | 1973-12-04 | Messerschmitt Boelkow Blohm | Missile with thrust vector and aerodynamic control |
EP0066715A2 (en) * | 1981-06-05 | 1982-12-15 | Hüls Troisdorf Aktiengesellschaft | Spin-stabilised training projectile |
EP0066715A3 (en) * | 1981-06-05 | 1983-03-30 | Dynamit Nobel Aktiengesellschaft | Spin-stabilised training projectile |
US4624424A (en) * | 1984-11-07 | 1986-11-25 | The Boeing Company | On-board flight control drag actuator system |
US4699333A (en) * | 1984-11-07 | 1987-10-13 | The Boeing Company | On-board flight control panel system |
US5031856A (en) * | 1989-05-12 | 1991-07-16 | Diehl Gmbh & Co. | Airborne submunition member |
DE3915585A1 (en) * | 1989-05-12 | 1990-11-15 | Diehl Gmbh & Co | SUBMUNITION MISSILE |
FR2655722A1 (en) * | 1989-12-12 | 1991-06-14 | Aerospatiale | SUPERSONIC MISSILE WITH TORQUE DRIVING BY SPOUILERS. |
EP0433128A1 (en) * | 1989-12-12 | 1991-06-19 | AEROSPATIALE Société Nationale Industrielle | Supersonic missile guided by a coupling action carried out by spoilers |
US5143320A (en) * | 1989-12-12 | 1992-09-01 | Societe Nationale Industrielle Et Aerospatiale | Spoiler torque controlled supersonic missile |
GB2244118A (en) * | 1990-03-10 | 1991-11-20 | Atomic Energy Authority Uk | Reconnaissance device. |
US5060574A (en) * | 1990-07-02 | 1991-10-29 | Honeywell Inc. | Projectile base plug with enhanced drag-producing separation capability |
DE4412687A1 (en) * | 1994-04-13 | 1995-10-19 | Diehl Gmbh & Co | Projectile remotely controllable using a laser beam |
DE4412687C2 (en) * | 1994-04-13 | 1999-06-24 | Diehl Stiftung & Co | Projectile remotely controllable using a laser beam |
WO1998046962A1 (en) * | 1997-04-11 | 1998-10-22 | Raytheon Company | Unlocking tail fin assembly for guided projectiles |
US6559370B1 (en) * | 2002-08-06 | 2003-05-06 | The United States Of America As Represented By The Secretary Of The Navy | Submarine countermeasure vehicle with folding propeller |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLNP | Patent lapsed through nonpayment of renewal fees |