ES2031261T3 - Operculo trasero para contenedor de misiles. - Google Patents

Operculo trasero para contenedor de misiles.

Info

Publication number
ES2031261T3
ES2031261T3 ES88402343T ES88402343T ES2031261T3 ES 2031261 T3 ES2031261 T3 ES 2031261T3 ES 88402343 T ES88402343 T ES 88402343T ES 88402343 T ES88402343 T ES 88402343T ES 2031261 T3 ES2031261 T3 ES 2031261T3
Authority
ES
Spain
Prior art keywords
opercle
missile
missile container
operculo
superior
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
ES88402343T
Other languages
English (en)
Inventor
Pierre-Jacques Truyman
Michel Bouron
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
Original Assignee
Direction General pour lArmement DGA
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 filed Critical Direction General pour lArmement DGA
Application granted granted Critical
Publication of ES2031261T3 publication Critical patent/ES2031261T3/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)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Carbon And Carbon Compounds (AREA)

Abstract

EL OPERCULO CONSTA DE VARIOS ELEMENTOS (10) QUE ESTAN MONTADOS ENTRE DOS ORGANOS DE SOPORTE SUPERIORES (7) E INFERIORES (8), Y QUE PUEDEN DEFORMARSE EN UNA POSICION INICIAL DE CIERRE POR LOS GASES PRODUCIDOS TRAS EL ENCENDIDO DEL MISIL (2). SE CARACTERIZA PORQUE CADA ELEMENTO (10) DEL OPERCULO ES ELASTICO Y SE DEFORMA ALREDEDOR DE AL MENOS UNA PARTE REDONDEADA (19) SITUADA EN DICHO ORGANO INFERIOR (8). APLICACION, EN ESPECIAL, A LOS CONTENEDORES DE MISILES A BORDO DE BUQUES DE GUERRA.
ES88402343T 1987-09-17 1988-09-16 Operculo trasero para contenedor de misiles. Expired - Lifetime ES2031261T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8712862A FR2620808B1 (fr) 1987-09-17 1987-09-17 Opercule arriere pour conteneur de missile

Publications (1)

Publication Number Publication Date
ES2031261T3 true ES2031261T3 (es) 1992-12-01

Family

ID=9354974

Family Applications (1)

Application Number Title Priority Date Filing Date
ES88402343T Expired - Lifetime ES2031261T3 (es) 1987-09-17 1988-09-16 Operculo trasero para contenedor de misiles.

Country Status (3)

Country Link
EP (1) EP0308344B1 (es)
ES (1) ES2031261T3 (es)
FR (1) FR2620808B1 (es)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5194688A (en) * 1992-01-31 1993-03-16 Hughes Missile Systems Company Apparatus for limiting recirculation of rocket exhaust gases during missile launch
FR2926357B1 (fr) 2008-01-11 2013-10-25 Dcns Conteneur de missile multiple et lanceur polyvalent
FR2926360B1 (fr) 2008-01-11 2012-10-19 Dcns Opercule arriere deformable pour conteneur de missile, comportant un cadre de support aval
FR2926359B1 (fr) 2008-01-11 2010-02-12 Dcns Opercule arriere deformable a lames elastiques pour conteneur de missile
FR2926358B1 (fr) 2008-01-11 2010-01-15 Dcns Opercule aval deformable ameliore pour conteneur de missile
FR3039889B1 (fr) * 2015-08-05 2017-07-28 Mbda France Opercule flexible pour conteneur de missile

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2445423A (en) * 1946-03-06 1948-07-20 United Shoe Machinery Corp Safety container for rockets
DE2715704A1 (de) * 1976-04-08 1977-10-20 Mcevoy Oilfield Equipment Co Verbindungsanordnung fuer ein sich vom meeresboden zu einem schwimmenden bohrgeraet erstreckendes steigrohr
GB1540803A (en) * 1977-06-14 1979-02-14 Gen Dynamics Corp Rocket exhaust plenum flow control apparatus
US4134327A (en) * 1977-12-12 1979-01-16 General Dynamics Corporation Rocket launcher tube post-launch rear closure

Also Published As

Publication number Publication date
EP0308344A1 (fr) 1989-03-22
EP0308344B1 (fr) 1992-04-15
FR2620808A1 (fr) 1989-03-24
FR2620808B1 (fr) 1990-01-12

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