DE69627322D1 - Rakete mit gitterruder - Google Patents
Rakete mit gitterruderInfo
- Publication number
- DE69627322D1 DE69627322D1 DE69627322T DE69627322T DE69627322D1 DE 69627322 D1 DE69627322 D1 DE 69627322D1 DE 69627322 T DE69627322 T DE 69627322T DE 69627322 T DE69627322 T DE 69627322T DE 69627322 D1 DE69627322 D1 DE 69627322D1
- Authority
- DE
- Germany
- Prior art keywords
- grille
- rocket
- 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
- F42B10/143—Lattice or grid fins
-
- 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
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Vibration Dampers (AREA)
- Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)
- Photovoltaic Devices (AREA)
Applications Claiming Priority (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU95107199 | 1995-05-11 | ||
RU95107195 | 1995-05-11 | ||
RU95107195/11A RU2085440C1 (ru) | 1995-05-11 | 1995-05-11 | Решетчатая аэродинамическая поверхность |
RU95107199/11A RU2085826C1 (ru) | 1995-05-11 | 1995-05-11 | Ракета |
RU95107196 | 1995-05-11 | ||
RU95107196/11A RU2085825C1 (ru) | 1995-05-11 | 1995-05-11 | Ракета с нормальной аэродинамической схемой |
PCT/RU1996/000102 WO1996035613A1 (fr) | 1995-05-11 | 1996-04-29 | Fusee a gouvernes en treillis et gouverne en treillis pour fusee |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69627322D1 true DE69627322D1 (de) | 2003-05-15 |
DE69627322T2 DE69627322T2 (de) | 2004-02-12 |
Family
ID=27354155
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69627322T Expired - Fee Related DE69627322T2 (de) | 1995-05-11 | 1996-04-29 | Rakete mit gitterruder |
Country Status (5)
Country | Link |
---|---|
US (1) | US6073879A (de) |
EP (1) | EP0829424B1 (de) |
CN (1) | CN1073040C (de) |
DE (1) | DE69627322T2 (de) |
WO (1) | WO1996035613A1 (de) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7564220B2 (en) | 2000-09-21 | 2009-07-21 | O2Micro International Ltd. | Method and electronic circuit for efficient battery wake up charging |
ATE519672T1 (de) | 2004-06-01 | 2011-08-15 | Deutsch Zentr Luft & Raumfahrt | Trag- oder leitelement |
US7429017B2 (en) * | 2005-07-21 | 2008-09-30 | Raytheon Company | Ejectable aerodynamic stability and control |
US7854410B2 (en) * | 2006-05-15 | 2010-12-21 | Kazak Composites, Incorporated | Powered unmanned aerial vehicle |
US7800032B1 (en) * | 2006-11-30 | 2010-09-21 | Raytheon Company | Detachable aerodynamic missile stabilizing system |
US8438977B2 (en) * | 2008-12-25 | 2013-05-14 | Lockheed Martin Corporation | Projectile having deployable fin |
CN106800085B (zh) * | 2009-09-09 | 2020-08-18 | 威罗门飞行公司 | 升降副翼控制系统 |
CN105730678B (zh) * | 2016-02-18 | 2018-01-30 | 江西洪都航空工业集团有限责任公司 | 一种可折叠式格栅舵面 |
CN108216574A (zh) * | 2017-12-21 | 2018-06-29 | 北京有色金属研究总院 | 一种梯度结构栅格翼 |
CN108163134B (zh) * | 2017-12-29 | 2020-07-24 | 南京理工大学 | 用于超空泡水下航行体的自动触发式格栅尾翼结构 |
CN109454352B (zh) * | 2018-11-30 | 2021-03-02 | 上海航天精密机械研究所 | 弧面格栅结构及其制备方法 |
CN110260726B (zh) * | 2019-05-28 | 2021-09-03 | 上海宇航系统工程研究所 | 一种栅格舵装置 |
CN110979741B (zh) * | 2019-11-25 | 2021-02-09 | 北京宇航系统工程研究所 | 一种基于落区控制的锯齿台阶型变剖面栅格舵结构 |
CN110906807B (zh) * | 2019-12-13 | 2021-11-16 | 北京中科宇航探索技术有限公司 | 一种火箭用嵌入式气动控制舵面 |
CN111516909B (zh) * | 2020-04-30 | 2022-02-25 | 北京星际荣耀空间科技股份有限公司 | 一种火箭姿态控制系统 |
CN111731467A (zh) * | 2020-06-30 | 2020-10-02 | 北京星际荣耀空间科技有限公司 | 一种栅格舵和飞行器 |
CN113247238B (zh) * | 2021-06-24 | 2022-04-26 | 湖北三江航天红阳机电有限公司 | 一种格栅翼及飞行器 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2846165A (en) * | 1956-06-25 | 1958-08-05 | John A Axelson | Aircraft control system |
US3064930A (en) * | 1959-09-08 | 1962-11-20 | Nord Aviation | Roll control surfaces |
US3047259A (en) * | 1959-11-25 | 1962-07-31 | George J Tatnall | Speed brake retarding mechanism for an air-dropped store |
DE1800776C3 (de) * | 1968-10-03 | 1975-12-11 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | RückstoBgetrlebener Flugkörper |
FR2109502A1 (de) * | 1970-10-28 | 1972-05-26 | Europ Propulsion | |
FR2221707B1 (de) * | 1973-03-14 | 1976-04-30 | France Etat | |
DE2944743C2 (de) * | 1979-11-06 | 1982-07-29 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Tragflügel für ein schnellfliegendes Flugzeug |
US4560121A (en) * | 1983-05-17 | 1985-12-24 | The Garrett Corporation | Stabilization of automotive vehicle |
IL72000A (en) * | 1984-06-04 | 1989-09-10 | Israel State | Projectile stabilization system |
DE3441534A1 (de) * | 1984-11-14 | 1986-05-15 | Diehl GmbH & Co, 8500 Nürnberg | Lageranordnung fuer das ruderblatt eines flugkoerpers |
US4884766A (en) * | 1988-05-25 | 1989-12-05 | The United States Of America As Represented By The Secretary Of The Air Force | Automatic fin deployment mechanism |
US5048773A (en) * | 1990-06-08 | 1991-09-17 | The United States Of America As Represented By The Secretary Of The Army | Curved grid fin |
DE4020897C2 (de) * | 1990-06-30 | 1993-11-11 | Diehl Gmbh & Co | Einrichtung zum Entriegeln und Ausschwenken der Ruderblätter eines Projektiles |
US5192037A (en) * | 1991-08-23 | 1993-03-09 | Mcdonnell Douglas Corporation | Double-pivoting deployment system for aerosurfaces |
IL107844A (en) * | 1993-12-02 | 1996-06-18 | Ministry Of Defence Armaments | Flying object control system |
US5549065A (en) * | 1995-03-27 | 1996-08-27 | The United States Of America As Represented By The Secretary Of The Navy | Water vehicle and a directional control device therefor |
US5551364A (en) * | 1995-03-27 | 1996-09-03 | The United States Of America As Represented By The Secretary Of The Navy | Underwater vehicle and combination directional control and cable interconnect device |
US5642867A (en) * | 1995-06-06 | 1997-07-01 | Hughes Missile Systems Company | Aerodynamic lifting and control surface and control system using same |
-
1996
- 1996-04-29 US US08/930,076 patent/US6073879A/en not_active Expired - Lifetime
- 1996-04-29 EP EP96915252A patent/EP0829424B1/de not_active Expired - Lifetime
- 1996-04-29 CN CN96194706A patent/CN1073040C/zh not_active Expired - Fee Related
- 1996-04-29 DE DE69627322T patent/DE69627322T2/de not_active Expired - Fee Related
- 1996-04-29 WO PCT/RU1996/000102 patent/WO1996035613A1/ru active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
CN1187794A (zh) | 1998-07-15 |
EP0829424A1 (de) | 1998-03-18 |
EP0829424B1 (de) | 2003-04-09 |
EP0829424A4 (de) | 1999-05-19 |
WO1996035613A1 (fr) | 1996-11-14 |
CN1073040C (zh) | 2001-10-17 |
US6073879A (en) | 2000-06-13 |
DE69627322T2 (de) | 2004-02-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |