ES8606634A1 - Una disposicion de sujeccion de misiles en vacio - Google Patents
Una disposicion de sujeccion de misiles en vacioInfo
- 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
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)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (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.
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 |
---|---|
ES8606634A1 true ES8606634A1 (es) | 1986-04-01 |
ES535138A0 ES535138A0 (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)
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)
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 |
-
1983
- 1983-09-16 US US06/532,743 patent/US4550640A/en not_active Expired - Lifetime
-
1984
- 1984-07-12 EP EP84108203A patent/EP0158701B1/en not_active Expired
- 1984-07-12 DE DE8484108203T patent/DE3467925D1/de not_active Expired
- 1984-07-19 CA CA000459293A patent/CA1244281A/en not_active Expired
- 1984-08-07 NO NO843157A patent/NO156103C/no unknown
- 1984-08-10 IL IL72639A patent/IL72639A/xx not_active IP Right Cessation
- 1984-08-14 ES ES535138A patent/ES8606634A1/es not_active Expired
- 1984-09-14 DK DK441384A patent/DK158117C/da not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
NO156103B (no) | 1987-04-13 |
DE3467925D1 (en) | 1988-01-14 |
EP0158701B1 (en) | 1987-12-02 |
DK158117C (da) | 1990-08-20 |
EP0158701A3 (en) | 1986-04-30 |
DK441384D0 (da) | 1984-09-14 |
IL72639A (en) | 1989-12-15 |
US4550640A (en) | 1985-11-05 |
DK158117B (da) | 1990-03-26 |
CA1244281A (en) | 1988-11-08 |
EP0158701A2 (en) | 1985-10-23 |
ES535138A0 (es) | 1986-04-01 |
DK441384A (da) | 1985-03-17 |
NO843157L (no) | 1985-03-18 |
NO156103C (no) | 1987-07-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FD1A | Patent lapsed |
Effective date: 20010301 |