GB793927A - Improvements relating to rocket containers for aircraft - Google Patents
Improvements relating to rocket containers for aircraftInfo
- Publication number
- GB793927A GB793927A GB1237352A GB1237352A GB793927A GB 793927 A GB793927 A GB 793927A GB 1237352 A GB1237352 A GB 1237352A GB 1237352 A GB1237352 A GB 1237352A GB 793927 A GB793927 A GB 793927A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- container
- rockets
- fired
- micro
- 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
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
- F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
-
- 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
- F41F3/06—Rocket or torpedo launchers for rockets from aircraft
- F41F3/065—Rocket pods, i.e. detachable containers for launching a plurality of rockets
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Emergency Lowering Means (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
793,927. Self-propelled missiles. FAIREY AVIATION CO., Ltd. Aug. 12, 1953 [May 15, 1952], No. 12373/52. Class 9(2) The combination of an aircraft with a container for a number of rockets is provided with means to release the container from the aircraft and means arranged to fire the rockets from the container after it has been released. As shown in Fig. 1, the container may comprise a nose fairing 11, a central portion 10 containing 20-30 rockets 14, and a tailpiece 12 containing a rocket propulsive unit 13 for propelling the complete unit with its load. An aircraft may carry two containers, one under each wing, and after a predetermined time after a container has been fired from the aircraft the nose fairing 11 may be released by the ignition of a cartridge (not shown); the release of the fairing closes a micro-switch which operates a riffle-firing selector switch so that the rockets 14 are fired at 5 micro-second intervals.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1237352A GB793927A (en) | 1952-05-15 | 1952-05-15 | Improvements relating to rocket containers for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1237352A GB793927A (en) | 1952-05-15 | 1952-05-15 | Improvements relating to rocket containers for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB793927A true GB793927A (en) | 1958-04-23 |
Family
ID=10003351
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1237352A Expired GB793927A (en) | 1952-05-15 | 1952-05-15 | Improvements relating to rocket containers for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB793927A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3048086A (en) * | 1959-06-17 | 1962-08-07 | Robert Roger Aime | Rocket-bomb firing apparatus |
US3374740A (en) * | 1965-12-08 | 1968-03-26 | Whirlpool Co | Projectile |
US3397638A (en) * | 1961-03-08 | 1968-08-20 | Mb Assoc | Rocket launcher |
DE3132190A1 (en) * | 1981-08-14 | 1983-03-03 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | CARRYING DEVICE FOR A DUMP LOAD ON A PLANE |
US4455917A (en) * | 1982-03-15 | 1984-06-26 | General Dynamics, Pomona Division | Shock wave end cap removal device |
EP0562831A1 (en) * | 1992-03-27 | 1993-09-29 | British Aerospace Public Limited Company | Air-vehicle launcher apparatus |
-
1952
- 1952-05-15 GB GB1237352A patent/GB793927A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3048086A (en) * | 1959-06-17 | 1962-08-07 | Robert Roger Aime | Rocket-bomb firing apparatus |
US3397638A (en) * | 1961-03-08 | 1968-08-20 | Mb Assoc | Rocket launcher |
US3374740A (en) * | 1965-12-08 | 1968-03-26 | Whirlpool Co | Projectile |
DE3132190A1 (en) * | 1981-08-14 | 1983-03-03 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | CARRYING DEVICE FOR A DUMP LOAD ON A PLANE |
US4447025A (en) * | 1981-08-14 | 1984-05-08 | Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung | Carrier for a dropload to be dropped from an aircraft |
US4455917A (en) * | 1982-03-15 | 1984-06-26 | General Dynamics, Pomona Division | Shock wave end cap removal device |
EP0562831A1 (en) * | 1992-03-27 | 1993-09-29 | British Aerospace Public Limited Company | Air-vehicle launcher apparatus |
US5363737A (en) * | 1992-03-27 | 1994-11-15 | British Aerospace Public Limited Company | Air-vehicle launcher apparatus |
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