FR2891359B1 - Nouveau dispositif embarque de generation de decharge(s) plasma pour le pilotage d'un engin supersonique ou hypersonique. - Google Patents

Nouveau dispositif embarque de generation de decharge(s) plasma pour le pilotage d'un engin supersonique ou hypersonique.

Info

Publication number
FR2891359B1
FR2891359B1 FR0509831A FR0509831A FR2891359B1 FR 2891359 B1 FR2891359 B1 FR 2891359B1 FR 0509831 A FR0509831 A FR 0509831A FR 0509831 A FR0509831 A FR 0509831A FR 2891359 B1 FR2891359 B1 FR 2891359B1
Authority
FR
France
Prior art keywords
hypersonic
supersonic
controlling
plasma discharge
discharge generating
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
Application number
FR0509831A
Other languages
English (en)
Other versions
FR2891359A1 (fr
Inventor
Patrick Gnemmi
Christian Rey
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.)
Institut Franco Allemand de Recherches de Saint Louis ISL
Original Assignee
Institut Franco Allemand de Recherches de Saint Louis ISL
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 Institut Franco Allemand de Recherches de Saint Louis ISL filed Critical Institut Franco Allemand de Recherches de Saint Louis ISL
Priority to FR0509831A priority Critical patent/FR2891359B1/fr
Priority to DE602006006767T priority patent/DE602006006767D1/de
Priority to EP06291486A priority patent/EP1767894B1/fr
Priority to US11/525,169 priority patent/US7645969B2/en
Priority to CA2560520A priority patent/CA2560520C/fr
Publication of FR2891359A1 publication Critical patent/FR2891359A1/fr
Application granted granted Critical
Publication of FR2891359B1 publication Critical patent/FR2891359B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/668—Injection of a fluid, e.g. a propellant, into the gas shear in a nozzle or in the boundary layer at the outer surface of a missile, e.g. to create a shock wave in a supersonic flow

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Plasma Technology (AREA)
FR0509831A 2005-09-27 2005-09-27 Nouveau dispositif embarque de generation de decharge(s) plasma pour le pilotage d'un engin supersonique ou hypersonique. Expired - Fee Related FR2891359B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR0509831A FR2891359B1 (fr) 2005-09-27 2005-09-27 Nouveau dispositif embarque de generation de decharge(s) plasma pour le pilotage d'un engin supersonique ou hypersonique.
DE602006006767T DE602006006767D1 (de) 2005-09-27 2006-09-21 Im Innern eines Flugkörpers angebrachte Plasmaentladungen erzeugende Vorrichtung zur Steuerung eines supersonischen oder hypersonischen Flugkörpers
EP06291486A EP1767894B1 (fr) 2005-09-27 2006-09-21 Dispositif embarqué de génération de décharges plasma pour le pilotage d'un engin supersonique ou hypersonique
US11/525,169 US7645969B2 (en) 2005-09-27 2006-09-22 Low voltage device for the generation of plasma discharge to operate a supersonic or hypersonic apparatus
CA2560520A CA2560520C (fr) 2005-09-27 2006-09-22 Dispositif embarque a courant basse tension pour la generation de decharge(s) plasma pour le pilotage d'un engin supersonique ou hypersonique

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0509831A FR2891359B1 (fr) 2005-09-27 2005-09-27 Nouveau dispositif embarque de generation de decharge(s) plasma pour le pilotage d'un engin supersonique ou hypersonique.

Publications (2)

Publication Number Publication Date
FR2891359A1 FR2891359A1 (fr) 2007-03-30
FR2891359B1 true FR2891359B1 (fr) 2007-12-14

Family

ID=36579580

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0509831A Expired - Fee Related FR2891359B1 (fr) 2005-09-27 2005-09-27 Nouveau dispositif embarque de generation de decharge(s) plasma pour le pilotage d'un engin supersonique ou hypersonique.

Country Status (5)

Country Link
US (1) US7645969B2 (fr)
EP (1) EP1767894B1 (fr)
CA (1) CA2560520C (fr)
DE (1) DE602006006767D1 (fr)
FR (1) FR2891359B1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7988103B2 (en) 2007-01-19 2011-08-02 John Hopkins University Solid state supersonic flow actuator and method of use
US8119956B2 (en) * 2008-10-02 2012-02-21 Raytheon Company Multi-stage hyper-velocity kinetic energy missile
US8502126B2 (en) * 2010-05-27 2013-08-06 Raytheon Company System and method for navigating an object
US9329007B2 (en) 2013-02-01 2016-05-03 Orbital Atk, Inc. Charged projectiles and related assemblies, systems and methods
US10914559B1 (en) 2016-11-21 2021-02-09 Lockheed Martin Corporation Missile, slot thrust attitude controller system, and method
US10113844B1 (en) * 2016-11-21 2018-10-30 Lockheed Martin Corporation Missile, chemical plasm steering system, and method
CN112937912B (zh) * 2021-01-21 2023-08-15 南京南华航空产业有限公司 一种基于阵列式等离子体的旋成体侧向力控制实验装置

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3151259A (en) 1959-08-18 1964-09-29 Gen Electric Plasma accelerator system
US3176227A (en) * 1959-09-23 1965-03-30 Bendix Corp Control of ions in ionic media for communication and other purposes
US3325123A (en) * 1961-05-19 1967-06-13 Fay E Null Magnetohydrodynamic control
US3392941A (en) * 1966-09-22 1968-07-16 Army Usa Magnetohydrodynamic rudder for reentry device
IL92477A (en) * 1989-11-28 1993-08-18 Israel State Electrothermic projectile launching device
US5273237A (en) * 1992-11-02 1993-12-28 The United States Of America As Represented By The Secretary Of The Air Force Forebody nozzle for aircraft directional control
US6145298A (en) * 1997-05-06 2000-11-14 Sky Station International, Inc. Atmospheric fueled ion engine
US6247671B1 (en) * 1998-09-23 2001-06-19 Accurate Automation Corporation Ion doping apparatus and method for aerodynamic flow control
US6367735B1 (en) * 2000-02-10 2002-04-09 Quantic Industries, Inc. Projectile diverter
FR2846081B1 (fr) 2002-10-17 2005-01-07 Saint Louis Inst Pilotage d'un projectile par decharge plasma

Also Published As

Publication number Publication date
US7645969B2 (en) 2010-01-12
CA2560520C (fr) 2014-03-25
US20070200028A1 (en) 2007-08-30
EP1767894B1 (fr) 2009-05-13
DE602006006767D1 (de) 2009-06-25
EP1767894A1 (fr) 2007-03-28
CA2560520A1 (fr) 2007-03-27
FR2891359A1 (fr) 2007-03-30

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20110531