ES2088999T3 - Misiles supersonicos con pilotado en par mediante espoilers. - Google Patents

Misiles supersonicos con pilotado en par mediante espoilers.

Info

Publication number
ES2088999T3
ES2088999T3 ES90403430T ES90403430T ES2088999T3 ES 2088999 T3 ES2088999 T3 ES 2088999T3 ES 90403430 T ES90403430 T ES 90403430T ES 90403430 T ES90403430 T ES 90403430T ES 2088999 T3 ES2088999 T3 ES 2088999T3
Authority
ES
Spain
Prior art keywords
fuselage
espoilers
piloted
pair
supersonic
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 - Lifetime
Application number
ES90403430T
Other languages
English (en)
Inventor
Leon Boyadjian
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2088999T3 publication Critical patent/ES2088999T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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)

Abstract

MISIL SUPERSONICO GUIADO QUE COMPRENDE UN FUSELAJE (2, 2'', 2"), TERMINADO EN LA PARTE ANTERIOR POR UNA NARIZ (3, 3'', 3") Y EN LA PARTE TRASERA POR UN CASQUILLO (4, 4'', 4") Y PROVISTO EXTERIORMENTE DE ALETASTRASEROS FIJOS (5, 5'', 5") CARACTERIZADO POR EL HECHO DE QUE TIENE, LONGITUDINALMENTE A DISTANCIA DEL CENTRO DE GRAVEDAD (G1) AL MENOS UN ALERON (7, 7'', 7") MOVIL, LLAMADO SPOILER, ENTRE UNA CONFIGURACION BORRADA EN EL INTERIOR DEL FUSELAJE Y UNA CONFIGURACION DESPLEGADA TRANSVERSALMENTE EN LA CUAL EL ALERON VIENE LATERALMENTE EN PROTUBERANCIA EN FRENTE DE ESE FUSELAJE.
ES90403430T 1989-12-12 1990-12-03 Misiles supersonicos con pilotado en par mediante espoilers. Expired - Lifetime ES2088999T3 (es)

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 (1)

Publication Number Publication Date
ES2088999T3 true ES2088999T3 (es) 1996-10-01

Family

ID=9388412

Family Applications (1)

Application Number Title Priority Date Filing Date
ES90403430T Expired - Lifetime ES2088999T3 (es) 1989-12-12 1990-12-03 Misiles supersonicos con pilotado en par mediante espoilers.

Country Status (6)

Country Link
US (1) US5143320A (es)
EP (1) EP0433128B1 (es)
CA (1) CA2031283C (es)
DE (1) DE69027750T2 (es)
ES (1) ES2088999T3 (es)
FR (1) FR2655722B1 (es)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
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
US6698684B1 (en) 2002-01-30 2004-03-02 Gulfstream Aerospace Corporation Supersonic aircraft with spike for controlling and reducing sonic boom
WO2003064254A2 (en) * 2002-01-30 2003-08-07 Gulfstream Aerospace Corporation Fuselage shaping and inclusion of spike on a supersonic aircraft 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
CN101384486A (zh) 2005-12-15 2009-03-11 湾流航空公司 用于超音速飞行器的等熵压缩入口
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
WO2009145687A1 (en) * 2008-05-30 2009-12-03 Saab Ab Arrangement and method for launching counter-measures
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
CA2031283C (en) 2001-05-29
CA2031283A1 (en) 1991-06-13
FR2655722B1 (fr) 1992-03-13
EP0433128B1 (fr) 1996-07-10
EP0433128A1 (fr) 1991-06-19
DE69027750D1 (de) 1996-08-14
DE69027750T2 (de) 1996-11-28
US5143320A (en) 1992-09-01
FR2655722A1 (fr) 1991-06-14

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