IT9047997A0 - SYSTEM FOR THE DEPLOYMENT OF AERODYNAMIC SURFACES (AEROFOIL) ON PROJECTILES, MISSILES OR SIMILAR - Google Patents
SYSTEM FOR THE DEPLOYMENT OF AERODYNAMIC SURFACES (AEROFOIL) ON PROJECTILES, MISSILES OR SIMILARInfo
- Publication number
- IT9047997A0 IT9047997A0 IT9047997A IT4799790A IT9047997A0 IT 9047997 A0 IT9047997 A0 IT 9047997A0 IT 9047997 A IT9047997 A IT 9047997A IT 4799790 A IT4799790 A IT 4799790A IT 9047997 A0 IT9047997 A0 IT 9047997A0
- Authority
- IT
- Italy
- Prior art keywords
- missiles
- aerofoil
- projectiles
- deployment
- similar
- Prior art date
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)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB898912632A GB8912632D0 (en) | 1989-06-02 | 1989-06-02 | Aerofoil deployment system |
Publications (2)
Publication Number | Publication Date |
---|---|
IT9047997A0 true IT9047997A0 (en) | 1990-05-24 |
IT9047997A1 IT9047997A1 (en) | 1990-12-03 |
Family
ID=10657733
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT047997A IT9047997A1 (en) | 1989-06-02 | 1990-05-24 | SYSTEM FOR THE DISPOSAL OF AERODYNAMIC SURFACES (AEROFOIL) ON BULLETS, MISSILES OR SIMILAR |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE4017504A1 (en) |
GB (1) | GB8912632D0 (en) |
IT (1) | IT9047997A1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19941555C5 (en) * | 1999-09-01 | 2004-12-30 | Rheinmetall W & M Gmbh | missile |
FR2895071B1 (en) * | 2005-12-19 | 2008-01-18 | Giat Ind Sa | ANTI-REBOUND LOCKING DEVICE OF A DEPLOYABLE FIN OF A PROJECTILE. |
US8338769B1 (en) * | 2008-02-07 | 2012-12-25 | Simmonds Precision Products, Inc. | Pyrotechnic fin deployment and retention mechanism |
CN101973390B (en) * | 2010-09-25 | 2013-05-22 | 中国航天科工集团第二研究院二一〇所 | Unfolding mechanism for foldable double wing boards of aircraft |
CN103963960B (en) * | 2014-05-14 | 2016-08-24 | 北京航空航天大学 | A kind of semi-rigid inflated type opens up receipts wing automatically |
-
1989
- 1989-06-02 GB GB898912632A patent/GB8912632D0/en active Pending
-
1990
- 1990-05-24 IT IT047997A patent/IT9047997A1/en unknown
- 1990-05-31 DE DE4017504A patent/DE4017504A1/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
DE4017504A1 (en) | 1993-07-15 |
GB8912632D0 (en) | 1992-11-04 |
IT9047997A1 (en) | 1990-12-03 |
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