ES2061209T3 - Dispositivo de cierre y de proteccion de un sistema de evacuacion de gases de un modulo de lanzamiento vertical. - Google Patents

Dispositivo de cierre y de proteccion de un sistema de evacuacion de gases de un modulo de lanzamiento vertical.

Info

Publication number
ES2061209T3
ES2061209T3 ES91402702T ES91402702T ES2061209T3 ES 2061209 T3 ES2061209 T3 ES 2061209T3 ES 91402702 T ES91402702 T ES 91402702T ES 91402702 T ES91402702 T ES 91402702T ES 2061209 T3 ES2061209 T3 ES 2061209T3
Authority
ES
Spain
Prior art keywords
closing
protection device
evacuation system
gas evacuation
launch module
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
ES91402702T
Other languages
English (en)
Inventor
Jacques-Pierre Truyman
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.)
Direction General pour lArmement DGA
Etat Francais
Original Assignee
Direction General pour lArmement DGA
Etat Francais
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 Direction General pour lArmement DGA, Etat Francais filed Critical Direction General pour lArmement DGA
Application granted granted Critical
Publication of ES2061209T3 publication Critical patent/ES2061209T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00—Rocket or torpedo launchers
    • F41F3/04—Rocket or torpedo launchers for rockets
    • F41F3/0413—Means for exhaust gas disposal, e.g. exhaust deflectors, gas evacuation systems

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Emergency Lowering Means (AREA)
  • Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Safety Valves (AREA)

Abstract

SE CARACTERIZA EN QUE COMPRENDE AL MENOS UN ELEMENTO DE CIERRE MONTADO SOBRE UN EJE DE CIERRE MONTADO SOBRE UN EJE DE ROTACION (16) QUE ATRAVIESA UN SOPORTE QUE ESTA DISPUESTO ALREDEDOR Y CERCA DEL EXTREMO SUPERIOR (9'') DEL CONDUCTO DE EVACUACION (9).
ES91402702T 1990-10-18 1991-10-10 Dispositivo de cierre y de proteccion de un sistema de evacuacion de gases de un modulo de lanzamiento vertical. Expired - Lifetime ES2061209T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9012877A FR2668254B1 (fr) 1990-10-18 1990-10-18 Dispositif de fermeture et de protection d'un systeme d'evacuation de gaz d'un module de lancement vertical.

Publications (1)

Publication Number Publication Date
ES2061209T3 true ES2061209T3 (es) 1994-12-01

Family

ID=9401340

Family Applications (1)

Application Number Title Priority Date Filing Date
ES91402702T Expired - Lifetime ES2061209T3 (es) 1990-10-18 1991-10-10 Dispositivo de cierre y de proteccion de un sistema de evacuacion de gases de un modulo de lanzamiento vertical.

Country Status (3)

Country Link
EP (1) EP0481851B1 (es)
ES (1) ES2061209T3 (es)
FR (1) FR2668254B1 (es)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2930817B1 (fr) * 2008-04-30 2011-07-01 Dcns Systeme d'obturation d'un conduit d'evacuation des gaz d'un lanceur de missiles

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4173919A (en) * 1977-12-12 1979-11-13 General Dynamics Corporation Two-way rocket plenum for combustion suppression
GB8825195D0 (en) * 1988-10-27 1989-04-19 British Aerospace Impingement pressure regulator

Also Published As

Publication number Publication date
EP0481851A1 (fr) 1992-04-22
FR2668254B1 (fr) 1993-07-23
FR2668254A1 (fr) 1992-04-24
EP0481851B1 (fr) 1994-07-20

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