FR2453279A1 - Statoreacteur pour missiles teleguides - Google Patents

Statoreacteur pour missiles teleguides

Info

Publication number
FR2453279A1
FR2453279A1 FR8006536A FR8006536A FR2453279A1 FR 2453279 A1 FR2453279 A1 FR 2453279A1 FR 8006536 A FR8006536 A FR 8006536A FR 8006536 A FR8006536 A FR 8006536A FR 2453279 A1 FR2453279 A1 FR 2453279A1
Authority
FR
France
Prior art keywords
statoreactor
missiles
nozzle
control
thrust
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.)
Withdrawn
Application number
FR8006536A
Other languages
English (en)
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 Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2453279A1 publication Critical patent/FR2453279A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray Control Apparatus (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Testing Of Engines (AREA)

Abstract

Statoréacteur pour missiles téléguidés. Statoréacteur pour missiles téleguidés avec déflexion du jet de poussée en particulier supersonique, dans lequel la tuyère de poussée comporte, raccordé à son extrémité sortie, un prolongement élargi au-delà du rapport d'expansion correspondant à la pression environnante et dans lequel, pour la déviation du jet, des impulsions de commande agissant à chaque fois dans le sens de la déflexion voulue sont délivrées au niveau des ouvertures de commande réparties dans le sens périphérique de la tuyère. Les ouvertures de commande 24B, 28A débouchant dans une zone marginale de l'extrémité sortie 10 de la tuyère sont raccordées à un système d'injection 14 les alimentant en gaz comprimé ou en fluide faisant office de fluide de commande.
FR8006536A 1979-04-03 1980-03-24 Statoreacteur pour missiles teleguides Withdrawn FR2453279A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19792913350 DE2913350A1 (de) 1979-04-03 1979-04-03 Strahltriebwerk fuer lenkflugkoerper

Publications (1)

Publication Number Publication Date
FR2453279A1 true FR2453279A1 (fr) 1980-10-31

Family

ID=6067301

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8006536A Withdrawn FR2453279A1 (fr) 1979-04-03 1980-03-24 Statoreacteur pour missiles teleguides

Country Status (3)

Country Link
DE (1) DE2913350A1 (fr)
FR (1) FR2453279A1 (fr)
GB (1) GB2045704A (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997014873A1 (fr) * 1995-10-16 1997-04-24 Valentin Semenovich Gorelykh Procede de conversion d'energie et dispositif de mise en oeuvre
IL116668A (en) * 1996-01-03 1998-12-06 Univ Ramot Apparatus and method for controlling the motion of a solid body or fluid stream
CN111350615B (zh) * 2020-03-27 2023-09-05 惠州学院 一种适用于垂直发射飞行器的整体式转弯装置

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1316191A (fr) * 1962-02-26 1963-01-25 United Aircraft Corp Dispositif de commande pour appareil propulseur
GB947751A (en) * 1961-02-28 1964-01-29 United Aircraft Corp Improvements relating to navigation control for a propulsive vehicle
US3166897A (en) * 1961-08-21 1965-01-26 United Aircraft Corp Roll control and thrust vector control
US3221498A (en) * 1962-08-06 1965-12-07 Lester T Bankston Secondary fluid injection thrust vectoring methods and apparatus
US3266732A (en) * 1963-09-03 1966-08-16 United Aircraft Corp Roll control system

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB947751A (en) * 1961-02-28 1964-01-29 United Aircraft Corp Improvements relating to navigation control for a propulsive vehicle
US3166897A (en) * 1961-08-21 1965-01-26 United Aircraft Corp Roll control and thrust vector control
FR1316191A (fr) * 1962-02-26 1963-01-25 United Aircraft Corp Dispositif de commande pour appareil propulseur
US3221498A (en) * 1962-08-06 1965-12-07 Lester T Bankston Secondary fluid injection thrust vectoring methods and apparatus
US3266732A (en) * 1963-09-03 1966-08-16 United Aircraft Corp Roll control system

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
EXBK/73 *

Also Published As

Publication number Publication date
GB2045704A (en) 1980-11-05
DE2913350A1 (de) 1980-10-16

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Legal Events

Date Code Title Description
ST Notification of lapse