IT1002569B - IMPROVEMENT IN FLEECE FOR ROCKETS AND SIMILAR - Google Patents
IMPROVEMENT IN FLEECE FOR ROCKETS AND SIMILARInfo
- Publication number
- IT1002569B IT1002569B IT54663/73A IT5466373A IT1002569B IT 1002569 B IT1002569 B IT 1002569B IT 54663/73 A IT54663/73 A IT 54663/73A IT 5466373 A IT5466373 A IT 5466373A IT 1002569 B IT1002569 B IT 1002569B
- Authority
- IT
- Italy
- Prior art keywords
- rockets
- fleece
- improvement
- 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
- F42B10/20—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces
-
- 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
- F42B10/18—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel using a longitudinally slidable support member
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Engines (AREA)
- Toys (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2264338A DE2264338A1 (en) | 1972-12-30 | 1972-12-30 | FOLD-OUT TAIL, ESPECIALLY FOR MISSILE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| IT1002569B true IT1002569B (en) | 1976-05-20 |
Family
ID=5865891
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT54663/73A IT1002569B (en) | 1972-12-30 | 1973-12-28 | IMPROVEMENT IN FLEECE FOR ROCKETS AND SIMILAR |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3861627A (en) |
| DE (1) | DE2264338A1 (en) |
| FR (1) | FR2212528B1 (en) |
| IT (1) | IT1002569B (en) |
Families Citing this family (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SE444612B (en) * | 1984-12-13 | 1986-04-21 | Ffv Affersverket | GUIDELINES FOR FENOR EXPOSURE OF PROJECTIL |
| DE3712704A1 (en) * | 1987-04-14 | 1988-11-03 | Diehl Gmbh & Co | MISSILE WITH FOLD-OUT WINGS |
| US5417139A (en) * | 1993-10-01 | 1995-05-23 | Unisys Corporation | Delivery system and method for flexible array |
| FR2721702B1 (en) * | 1994-06-28 | 1996-08-14 | Luchaire Defense Sa | Device for deploying a projectile fin. |
| US5671899A (en) * | 1996-02-26 | 1997-09-30 | Lockheed Martin Corporation | Airborne vehicle with wing extension and roll control |
| US5927643A (en) * | 1997-11-05 | 1999-07-27 | Atlantic Research Corporation | Self-deploying airfoil for missile or the like |
| US6224013B1 (en) * | 1998-08-27 | 2001-05-01 | Lockheed Martin Corporation | Tail fin deployment device |
| DE19960738C1 (en) * | 1999-12-16 | 2001-08-23 | Lfk Gmbh | Rudder connection for guided missiles |
| SE518656C2 (en) * | 2000-07-03 | 2002-11-05 | Bofors Defence Ab | Fine stabilized artillery grenade |
| US7513454B2 (en) * | 2003-09-05 | 2009-04-07 | Selex Sensors And Airborne Systems Limited | Drag-producing devices |
| US7262394B2 (en) * | 2004-03-05 | 2007-08-28 | The Boeing Company | Mortar shell ring tail and associated method |
| US7475846B2 (en) * | 2005-10-05 | 2009-01-13 | General Dynamics Ordnance And Tactical Systems, Inc. | Fin retention and deployment mechanism |
| ES2532733T3 (en) * | 2009-07-31 | 2015-03-31 | Raytheon Company | Folding fairing and method to reduce aerodynamic drag in an artillery projectile launched by cannon |
| US8754352B2 (en) * | 2010-04-07 | 2014-06-17 | Bae Systems Information And Electronic Systems Integration Inc. | Compression spring wing deployment initiator |
| CN104833276B (en) * | 2015-05-18 | 2016-09-14 | 中国船舶重工集团公司第七○二研究所 | Lattice fin synchronous expansion mechanism |
| CN105424314B (en) * | 2015-12-18 | 2018-02-09 | 中国航天空气动力技术研究院 | Free flight model rudder face deploys flow tunnel testing device |
| CN107421403A (en) * | 2017-09-20 | 2017-12-01 | 成都云鼎智控科技有限公司 | A kind of more bar coordinated type fold mechanisms for longitudinal folding missile wing |
| CN109141143A (en) * | 2018-07-26 | 2019-01-04 | 重庆长安工业(集团)有限责任公司 | A kind of folded surface locking mechanism |
| CN109696088B (en) * | 2018-12-07 | 2021-06-08 | 上海机电工程研究所 | Compact missile wing contraction and expansion mechanism and missile |
| US11340052B2 (en) | 2019-08-27 | 2022-05-24 | Bae Systems Information And Electronic Systems Integration Inc. | Wing deployment initiator and locking mechanism |
| CN110906807B (en) * | 2019-12-13 | 2021-11-16 | 北京中科宇航探索技术有限公司 | Embedded pneumatic control surface for rocket |
| US11852211B2 (en) | 2020-09-10 | 2023-12-26 | Bae Systems Information And Electronic Systems Integration Inc. | Additively manufactured elliptical bifurcating torsion spring |
| CN114216647B (en) * | 2021-12-16 | 2024-06-14 | 中国航天空气动力技术研究院 | A rudder wing transient extension and retraction device for wind tunnel test |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1187193A (en) * | 1957-11-15 | 1959-09-08 | Hotchkiss Brandt | Deployable stabilizer for projectile |
| NL266892A (en) * | 1960-07-11 | |||
| FR1418696A (en) * | 1963-12-28 | 1965-11-19 | Breda Mecc Bresciana | Folding wing rudder for rockets |
| CH493819A (en) * | 1968-07-11 | 1970-07-15 | Oerlikon Buehrle Ag | Twist-free projectile with launch tube |
| DE1906028C3 (en) * | 1969-02-07 | 1973-12-06 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Tail unit for projectiles and missiles with a device for moving the fins of the tail unit into their effective position |
-
1972
- 1972-12-30 DE DE2264338A patent/DE2264338A1/en active Pending
-
1973
- 1973-12-20 FR FR7345852A patent/FR2212528B1/fr not_active Expired
- 1973-12-28 US US429271A patent/US3861627A/en not_active Expired - Lifetime
- 1973-12-28 IT IT54663/73A patent/IT1002569B/en active
Also Published As
| Publication number | Publication date |
|---|---|
| US3861627A (en) | 1975-01-21 |
| DE2264338A1 (en) | 1974-07-04 |
| FR2212528B1 (en) | 1977-08-19 |
| FR2212528A1 (en) | 1974-07-26 |
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