ES8606634A1 - Una disposicion de sujeccion de misiles en vacio - Google Patents

Una disposicion de sujeccion de misiles en vacio

Info

Publication number
ES8606634A1
ES8606634A1 ES535138A ES535138A ES8606634A1 ES 8606634 A1 ES8606634 A1 ES 8606634A1 ES 535138 A ES535138 A ES 535138A ES 535138 A ES535138 A ES 535138A ES 8606634 A1 ES8606634 A1 ES 8606634A1
Authority
ES
Spain
Prior art keywords
missile
latch member
rocket motor
seal
releasing
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
Application number
ES535138A
Other languages
English (en)
Other versions
ES535138A0 (es
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.)
Rheinmetall Air Defence AG
Original Assignee
Werkzeugmaschinenfabrik Oerlikon Buhrle 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 Werkzeugmaschinenfabrik Oerlikon Buhrle AG filed Critical Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Publication of ES535138A0 publication Critical patent/ES535138A0/es
Publication of ES8606634A1 publication Critical patent/ES8606634A1/es
Expired 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
    • F41F3/052—Means for securing the rocket in the launching apparatus

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Clamps And Clips (AREA)

Abstract

DISPOSICION DE SUJECION DE MISILES EN VACIO, PARA LIBERAR PRONTAMENTE DE SU RECIPIENTE DE LANZAMIENTO UN MISIL PROPULSADO POR COHETE, TRAS LA IGNICION DE SU MOTOR DE COHETE Y LA EXPULSION DE UN OBTURADOR DE TOBERA DESDE SU TOBERA DE MOTOR DE COHETE. CONSTA DE UNOS MEDIOS DE ANCLAJE ADECUADOS, TALES COMO UN CANCAMO (16) ATORNILLADO A LA PORCION DE BASE (18) DEL MISIL (10), QUE RETIENEN EL MISIL EN UNA POSICION FIJA DENTRO DEL RECIPIENTE TUBULAR (12); DE UN MIEMBRO DE BASE (30) MONTADO FIRMEMENTE EN LA PARTE POSTERIOR DEL RECIPIENTE (12), EL CUAL SOPORTA EL MIEMBRO GIRATORIO (20) DE ENGANCHE.
ES535138A 1983-09-16 1984-08-14 Una disposicion de sujeccion de misiles en vacio Expired ES8606634A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/532,743 US4550640A (en) 1983-09-16 1983-09-16 Missile canister restraint device

Publications (2)

Publication Number Publication Date
ES535138A0 ES535138A0 (es) 1986-04-01
ES8606634A1 true ES8606634A1 (es) 1986-04-01

Family

ID=24122980

Family Applications (1)

Application Number Title Priority Date Filing Date
ES535138A Expired ES8606634A1 (es) 1983-09-16 1984-08-14 Una disposicion de sujeccion de misiles en vacio

Country Status (8)

Country Link
US (1) US4550640A (es)
EP (1) EP0158701B1 (es)
CA (1) CA1244281A (es)
DE (1) DE3467925D1 (es)
DK (1) DK158117C (es)
ES (1) ES8606634A1 (es)
IL (1) IL72639A (es)
NO (1) NO156103C (es)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3937344A1 (de) * 1989-11-09 1991-05-16 Dynamit Nobel Ag Raketenhalterung in einer startvorrichtung
US5074187A (en) * 1991-03-08 1991-12-24 The United States Of America As Represented By The Secretary Of The Navy Rocket nozzle shield
US5125318A (en) * 1991-12-18 1992-06-30 United States Government As Represented By The Secretary Of The Navy Inflatable device for excluding sea water from a rocket motor
KR0141405B1 (ko) * 1995-09-29 1998-06-15 배문한 미사일 구속장치
KR0156674B1 (ko) * 1995-12-15 1998-10-15 배문한 미사일 구속 및 해제 장치
KR100277213B1 (ko) * 1998-12-08 2001-01-15 최동환 강체구를 이용한 미사일 구속 및 해제 장치
US6895850B2 (en) * 2003-09-09 2005-05-24 The United States Of America As Represented By The Secretary Of The Navy Pressure-released brake assembly for restraining projectile in launch tube
US7340986B1 (en) * 2005-03-28 2008-03-11 Lockheed Martin Corporation Apparatus comprising a release system for canistered munitions
ITRM20050166A1 (it) * 2005-04-07 2005-07-07 Mbda italia spa Lanciatore terrestre per missili a lancio verticale.
US7624669B2 (en) * 2005-05-03 2009-12-01 Lockheed Martin Corporation Apparatus comprising a passively-actuated snubber
US7506570B1 (en) 2007-12-10 2009-03-24 The United States Of America As Represented By The Secretary Of The Navy Mechanism to hold and release
CN111664747A (zh) * 2020-05-18 2020-09-15 上海机电工程研究所 后置式机械固弹装置
RU2757568C1 (ru) * 2020-10-26 2021-10-18 Российская Федерация в лице Министерства обороны РФ Механизм удержания ракеты в контейнере
CN114459289B (zh) * 2021-08-06 2023-08-22 北京天兵科技有限公司 一种火箭箭角连接装置

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2831400A (en) * 1954-05-20 1958-04-22 Brevets Aero Mecaniques Devices for releasably holding the rear ends of rockets
DE1141210B (de) * 1959-06-09 1962-12-13 Boelkow Entwicklungen Kg Starteinrichtung fuer rueckstossgetriebene Flugkoerper
FR1265331A (fr) * 1960-05-19 1961-06-30 France Etat Dispositif de verrouillage d'un projectile autopropulsé à l'intérieur de sa caisse de lancement
CH388139A (de) * 1961-10-27 1965-02-15 Contraves Ag Lösbare Verriegelungsvorrichtung zum Sichern von in Raketenwerfern aufgehängten Raketen
FR1340562A (fr) * 1961-12-06 1963-10-18 Brevets Aero Mecaniques Perfectionnements apportés aux installations lance-roquettes à tubes de lancement, notamment à celles pour aérodynes
AT248290B (de) * 1963-10-16 1966-07-25 Bofors Ab Vorrichtung zur Befestigung eines Geschosses in einem Gehäuse
DE1428642A1 (de) * 1964-12-28 1968-11-28 Dynamit Nobel Ag Befestigung von Raketen in ihrer Abschussvorrichtung
GB1182275A (en) * 1967-04-13 1970-02-25 Dynamit Nobel Ag Means for Retaining Rockets in Rocket Launchers.
FR1528732A (fr) * 1967-04-20 1968-06-14 Dynamit Nobel Ag Mécanisme servant à retenir jusqu'à leur mise à feu des roquettes dans leur dispositif de lancement
CH527405A (fr) * 1970-07-10 1972-08-31 Sarmac Sa Ensemble comprenant un projectile autopropulsé empenné et son étui
BE772649A (fr) * 1971-09-16 1972-03-16 Zeebrugge Forges Sa Mecanisme d'armement pour tube de lancement de projectile du type roquette.
US3811360A (en) * 1972-11-28 1974-05-21 Us Army Rocket hold back and tube closure
US4132150A (en) * 1977-08-08 1979-01-02 The Unites States Of America As Represented By The Secretary Of The Army Blast actuated detent
US4336740A (en) * 1978-12-29 1982-06-29 Hughes Aircraft Company Automatic blast actuated positive release missile detent
US4304170A (en) * 1979-04-16 1981-12-08 The Boeing Company Locking assembly for a rocket and launch tube

Also Published As

Publication number Publication date
DE3467925D1 (en) 1988-01-14
DK158117B (da) 1990-03-26
IL72639A (en) 1989-12-15
EP0158701A2 (en) 1985-10-23
CA1244281A (en) 1988-11-08
DK158117C (da) 1990-08-20
EP0158701B1 (en) 1987-12-02
ES535138A0 (es) 1986-04-01
EP0158701A3 (en) 1986-04-30
NO156103C (no) 1987-07-22
US4550640A (en) 1985-11-05
DK441384D0 (da) 1984-09-14
NO843157L (no) 1985-03-18
NO156103B (no) 1987-04-13
DK441384A (da) 1985-03-17

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 20010301