DE69027750D1 - Überschallgeschoss mit Lenkung mittels paarweise wirkenden Luftbremsen - Google Patents
Überschallgeschoss mit Lenkung mittels paarweise wirkenden LuftbremsenInfo
- Publication number
- DE69027750D1 DE69027750D1 DE69027750T DE69027750T DE69027750D1 DE 69027750 D1 DE69027750 D1 DE 69027750D1 DE 69027750 T DE69027750 T DE 69027750T DE 69027750 T DE69027750 T DE 69027750T DE 69027750 D1 DE69027750 D1 DE 69027750D1
- Authority
- DE
- Germany
- Prior art keywords
- supersonic
- steering
- floor
- pairs
- air brakes
- 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
- F42B10/60—Steering arrangements
- F42B10/62—Steering by movement of flight surfaces
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)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8916406A FR2655722B1 (fr) | 1989-12-12 | 1989-12-12 | Missile supersonique a pilotage en couple par spouilers. |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69027750D1 true DE69027750D1 (de) | 1996-08-14 |
DE69027750T2 DE69027750T2 (de) | 1996-11-28 |
Family
ID=9388412
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69027750T Expired - Fee Related DE69027750T2 (de) | 1989-12-12 | 1990-12-03 | Überschallgeschoss mit Lenkung mittels paarweise wirkenden Luftbremsen |
Country Status (6)
Country | Link |
---|---|
US (1) | US5143320A (de) |
EP (1) | EP0433128B1 (de) |
CA (1) | CA2031283C (de) |
DE (1) | DE69027750T2 (de) |
ES (1) | ES2088999T3 (de) |
FR (1) | FR2655722B1 (de) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4239589A1 (de) * | 1992-11-25 | 1994-05-26 | Deutsche Aerospace | Vorrichtung zum Steuern von Flugkörpern mit einem aerodynamisch wirkenden Steuerkörper |
FR2702556B1 (fr) * | 1993-03-08 | 1995-04-28 | Giat Ind Sa | Tête militaire incendiaire. |
US5677508A (en) * | 1995-08-15 | 1997-10-14 | Hughes Missile Systems Company | Missile having non-cylindrical propulsion section |
GB9614133D0 (en) * | 1996-07-05 | 1997-03-12 | Secr Defence | Means for increasing the drag on a munition |
DE19839493C1 (de) * | 1998-08-29 | 1999-12-30 | Inst Franco Allemand De Rech D | Verfahren zur Steuerung eines Überschallflugkörpers sowie Überschallflugkörper |
AU2003209426A1 (en) * | 2002-01-30 | 2003-09-02 | Gulfstream Aerospace Corporation | Fuselage shaping and inclusion of spike on a supersonic aircraft for controlling and reducing sonic boom |
US6698684B1 (en) | 2002-01-30 | 2004-03-02 | Gulfstream Aerospace Corporation | Supersonic aircraft with spike for controlling and reducing sonic boom |
US6629668B1 (en) * | 2002-02-04 | 2003-10-07 | The United States Of America As Represented By The Secretary Of The Army | Jump correcting projectile system |
US6981672B2 (en) * | 2003-09-17 | 2006-01-03 | Aleiant Techsystems Inc. | Fixed canard 2-D guidance of artillery projectiles |
US7367530B2 (en) * | 2005-06-21 | 2008-05-06 | The Boeing Company | Aerospace vehicle yaw generating systems and associated methods |
CA3071172A1 (en) * | 2005-12-15 | 2008-04-17 | Gulfstream Aerospace Corporation | Isentropic compression inlet for supersonic aircraft |
US7611095B1 (en) * | 2006-04-28 | 2009-11-03 | The Boeing Company | Aerodynamic re-entry vehicle control with active and passive yaw flaps |
US8393158B2 (en) | 2007-10-24 | 2013-03-12 | Gulfstream Aerospace Corporation | Low shock strength inlet |
EP3025960B1 (de) * | 2008-05-30 | 2017-11-15 | Saab Ab | Anordnung und verfahren zum starten von gegenmassnahmen |
US8502126B2 (en) * | 2010-05-27 | 2013-08-06 | Raytheon Company | System and method for navigating an object |
US8525090B1 (en) * | 2010-06-23 | 2013-09-03 | The United States Of America As Represented By The Secretary Of The Army | Pneumatically actuated control surface for airframe body |
RU2580376C2 (ru) * | 2014-07-29 | 2016-04-10 | Николай Евгеньевич Староверов | Крылатая ракета, в частности - противокорабельная (варианты) |
RU2690236C1 (ru) * | 2018-04-03 | 2019-05-31 | Сергей Евгеньевич Угловский | Сверхзвуковая вращающаяся ракета |
DE102018005480A1 (de) * | 2018-07-11 | 2020-01-16 | Mbda Deutschland Gmbh | Flugkörper |
RU2703017C1 (ru) * | 2018-09-24 | 2019-10-15 | Сергей Евгеньевич Угловский | Сверхзвуковая вращающаяся ракета |
CN109823515B (zh) * | 2019-01-24 | 2020-12-15 | 北京理工大学 | 设置在制导飞行器上的扰流板系统及应用其的方法 |
CN113830290B (zh) * | 2021-09-03 | 2022-04-26 | 中国空气动力研究与发展中心低速空气动力研究所 | 一种伸缩式涡流发生器及其构成的桨毂 |
CN114486159A (zh) * | 2021-12-30 | 2022-05-13 | 中国航天空气动力技术研究院 | 内埋武器机弹分离相容性前缘锯齿扰流板控制及验证方法 |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR496912A (fr) * | 1916-08-08 | 1919-11-20 | Charles Leopold Mayer | Procédé pour faire du tir plongeant sans diminuer la charge |
US2922600A (en) * | 1956-04-18 | 1960-01-26 | John B Craft | Automatic guidance system |
US3305194A (en) * | 1960-03-08 | 1967-02-21 | Robert G Conard | Wind-insensitive missile |
GB1188651A (en) * | 1962-03-05 | 1970-04-22 | British Aircraft Corp Ltd | Improvements in or relating to Missiles |
US3136250A (en) * | 1962-05-04 | 1964-06-09 | Samuel A Humphrey | Integrated auxiliary power unit |
US3188958A (en) * | 1963-03-11 | 1965-06-15 | James D Burke | Range control for a ballistic missile |
CH480613A (de) * | 1967-09-11 | 1969-10-31 | Oerlikon Buehrle Ag | Geschoss mit Bremsflügeln |
US3759466A (en) * | 1972-01-10 | 1973-09-18 | Us Army | Cruise control for non-ballistic missiles by a special arrangement of spoilers |
GB1523963A (en) * | 1976-02-26 | 1978-09-06 | Hawker Siddeley Dynamics Ltd | Method and means for auxiliary control of vehicle direction |
AU524255B2 (en) * | 1978-12-29 | 1982-09-09 | Commonwealth Of Australia, The | Deployable wing |
US4327884A (en) * | 1980-01-23 | 1982-05-04 | The United States Of America As Represented By The Secretary Of The Air Force | Advanced air-to-surface weapon |
US4497460A (en) * | 1983-03-25 | 1985-02-05 | The United States Of America As Represented By The Secretary Of The Navy | Erodale spin turbine for tube-launched missiles |
US4699333A (en) * | 1984-11-07 | 1987-10-13 | The Boeing Company | On-board flight control panel system |
DE3628129C1 (de) * | 1986-08-19 | 1988-03-03 | Rheinmetall Gmbh | Flugkoerper |
-
1989
- 1989-12-12 FR FR8916406A patent/FR2655722B1/fr not_active Expired - Fee Related
-
1990
- 1990-11-30 CA CA002031283A patent/CA2031283C/en not_active Expired - Fee Related
- 1990-12-03 EP EP90403430A patent/EP0433128B1/de not_active Expired - Lifetime
- 1990-12-03 ES ES90403430T patent/ES2088999T3/es not_active Expired - Lifetime
- 1990-12-03 DE DE69027750T patent/DE69027750T2/de not_active Expired - Fee Related
- 1990-12-12 US US07/626,510 patent/US5143320A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
ES2088999T3 (es) | 1996-10-01 |
DE69027750T2 (de) | 1996-11-28 |
US5143320A (en) | 1992-09-01 |
CA2031283A1 (en) | 1991-06-13 |
CA2031283C (en) | 2001-05-29 |
EP0433128B1 (de) | 1996-07-10 |
FR2655722A1 (fr) | 1991-06-14 |
FR2655722B1 (fr) | 1992-03-13 |
EP0433128A1 (de) | 1991-06-19 |
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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 |