DE59205195D1 - Projectile with fold-out tail - Google Patents
Projectile with fold-out tailInfo
- Publication number
- DE59205195D1 DE59205195D1 DE59205195T DE59205195T DE59205195D1 DE 59205195 D1 DE59205195 D1 DE 59205195D1 DE 59205195 T DE59205195 T DE 59205195T DE 59205195 T DE59205195 T DE 59205195T DE 59205195 D1 DE59205195 D1 DE 59205195D1
- Authority
- DE
- Germany
- Prior art keywords
- projectile
- fold
- out tail
- tail
- 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 - Fee Related
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
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)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE4105142A DE4105142A1 (en) | 1991-02-20 | 1991-02-20 | PROJECTILE WITH FOLD-OUT PAD |
Publications (1)
Publication Number | Publication Date |
---|---|
DE59205195D1 true DE59205195D1 (en) | 1996-03-14 |
Family
ID=6425398
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE4105142A Withdrawn DE4105142A1 (en) | 1991-02-20 | 1991-02-20 | PROJECTILE WITH FOLD-OUT PAD |
DE59205195T Expired - Fee Related DE59205195D1 (en) | 1991-02-20 | 1992-02-08 | Projectile with fold-out tail |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE4105142A Withdrawn DE4105142A1 (en) | 1991-02-20 | 1991-02-20 | PROJECTILE WITH FOLD-OUT PAD |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP0499907B1 (en) |
DE (2) | DE4105142A1 (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2797946B1 (en) | 1999-08-31 | 2002-10-04 | Aerospatiale Matra Missiles | DEVICE FOR MOUNTING A RIGID APPENDIX ON A MACHINE SUITABLE TO BE LAUNCHED FROM THE TUBE, AND CORRESPONDING MACHINE |
GB0109277D0 (en) * | 2001-04-12 | 2001-05-30 | Olympic Technologies Ltd | Small arms projectile |
DE102007002948B4 (en) * | 2007-01-19 | 2009-04-02 | Diehl Bgt Defence Gmbh & Co. Kg | Device for wing deployment |
CN107933887B (en) * | 2017-10-23 | 2023-10-20 | 四川大学 | Rudder sheet unfolding mechanism |
FR3094475B1 (en) * | 2019-03-27 | 2022-08-12 | Nexter Munitions | Cowling and projectile comprising such a cowling |
CN111220032B (en) * | 2019-11-18 | 2022-05-27 | 中国空空导弹研究院 | Four-channel linkage unlocking mechanism of small folding control surface |
CN114485287B (en) * | 2021-12-30 | 2023-11-07 | 北京动力机械研究所 | Self-locking bearing structure of folding rudder |
CN114963884A (en) * | 2022-03-01 | 2022-08-30 | 宁波天擎航天科技有限公司 | Pneumatic controllable unfolding mechanism for target projectile rudder piece and target projectile with pneumatic controllable unfolding mechanism |
CN115014132A (en) * | 2022-03-01 | 2022-09-06 | 宁波天擎航天科技有限公司 | Controllable unfolding mechanism for target missile rudder piece and target missile provided with same |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE565999A (en) * | 1953-02-06 | |||
FR1191519A (en) * | 1958-02-13 | 1959-10-20 | Hotchkiss Brandt | Deploying tail for artillery projectile |
FR1405380A (en) * | 1964-05-28 | 1965-07-09 | Soc Tech De Rech Ind | Improvements to deploying stabilizers for projectiles |
FR1490554A (en) * | 1966-05-03 | 1967-08-04 | Ruggieri Ets | Development of deploying rocket stabilizers |
DE2603756A1 (en) * | 1976-01-31 | 1977-08-04 | Rheinmetall Gmbh | LOWER CALIBER FLOOR WITH STABILIZING WINGS |
DE2623582C2 (en) * | 1976-05-26 | 1985-06-13 | Rheinmetall GmbH, 4000 Düsseldorf | Rocket projectile with folding tail and sabot |
IL66624A (en) * | 1982-02-10 | 1986-04-29 | Gen Dynamics Corp | Wing housing and cover release assembly for self-erecting wing of a structure such as missile |
DE3432614A1 (en) * | 1984-09-05 | 1986-03-13 | Rheinmetall GmbH, 4000 Düsseldorf | MISSILE |
US4691880A (en) * | 1985-11-14 | 1987-09-08 | Grumman Aerospace Corporation | Torsion spring powered missile wing deployment system |
DE3608109A1 (en) * | 1986-03-12 | 1987-09-17 | Diehl Gmbh & Co | BRAKE DEVICE FOR A SPIN-STABILIZED PROJECTILE |
US4869442A (en) * | 1988-09-02 | 1989-09-26 | Aerojet-General Corporation | Self-deploying airfoil |
-
1991
- 1991-02-20 DE DE4105142A patent/DE4105142A1/en not_active Withdrawn
-
1992
- 1992-02-08 EP EP92102112A patent/EP0499907B1/en not_active Expired - Lifetime
- 1992-02-08 DE DE59205195T patent/DE59205195D1/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP0499907A2 (en) | 1992-08-26 |
EP0499907B1 (en) | 1996-01-31 |
EP0499907A3 (en) | 1993-03-31 |
DE4105142A1 (en) | 1992-08-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: DIEHL STIFTUNG & CO., 90478 NUERNBERG, DE |
|
8339 | Ceased/non-payment of the annual fee |