GB939806A - Improvements in rocket-bomb firing apparatus - Google Patents
Improvements in rocket-bomb firing apparatusInfo
- Publication number
- GB939806A GB939806A GB20442/60A GB2044260A GB939806A GB 939806 A GB939806 A GB 939806A GB 20442/60 A GB20442/60 A GB 20442/60A GB 2044260 A GB2044260 A GB 2044260A GB 939806 A GB939806 A GB 939806A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rockets
- tubes
- aircraft
- june
- casing
- 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
- 238000010304 firing Methods 0.000 title 1
- 235000015842 Hesperis Nutrition 0.000 abstract 5
- 235000012633 Iberis amara Nutrition 0.000 abstract 5
- 239000000463 material Substances 0.000 abstract 3
- 241000239290 Araneae Species 0.000 abstract 1
- 229920005830 Polyurethane Foam Polymers 0.000 abstract 1
- 238000007599 discharging Methods 0.000 abstract 1
- 239000006260 foam Substances 0.000 abstract 1
- 238000005192 partition Methods 0.000 abstract 1
- 239000011496 polyurethane foam Substances 0.000 abstract 1
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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
939,806. Releasing rockets from aircraft. R. A. ROBERT, and P. P. MATGE. June 10, 1960 [June 17, 1959], No. 20442/60. Class 9 (2). Apparatus for discharging rockets comprises a easing 10 to be releasably suspended from an aircraft and contains a plurality of rockets 13 together with a propulsion unit 25 whereby the apparatus can be self-propelled toward a target prior to the discharge of the rockets as in Specification 793,927. The casing 10 is provided with tail fins 12 and is closed at the forward end by a fairing 11 of breakable material such as polyurethane foam. This material may also fill the gaps between tubes 14 containing the rockets and an axial tube 16. Partitions 15 hold the tubes 14 in position and behind these tubes a sleeve 17 mounted on the tube 16 has a deflector surface 18 registering with arcuate openings 20 in the casing 10. The openings 20 are covered with breakable material such as the aforesaid foam. Beyond a transverse bulkhead 23, the unit 25 is supported by spiders 26, 27 and ends in a nozzle 28. The apparatus may be provided with a homing device.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR797786A FR1318601A (en) | 1959-06-17 | 1959-06-17 | Advanced training in rocket bomb launching devices |
Publications (1)
Publication Number | Publication Date |
---|---|
GB939806A true GB939806A (en) | 1963-10-16 |
Family
ID=8716155
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB20442/60A Expired GB939806A (en) | 1959-06-17 | 1960-06-10 | Improvements in rocket-bomb firing apparatus |
Country Status (3)
Country | Link |
---|---|
US (1) | US3048086A (en) |
FR (1) | FR1318601A (en) |
GB (1) | GB939806A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2310800A1 (en) * | 1972-03-08 | 1973-09-13 | Ciba Geigy Ag | POLYOLEFINS STABILIZED WITH ORGANIC HYDRAZINE COMPOUNDS AND PHENOLIC ANTIOXYDANTS |
FR2707751A1 (en) * | 1984-04-17 | 1995-01-20 | Short Brothers Plc | Girl missile release device. |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3397638A (en) * | 1961-03-08 | 1968-08-20 | Mb Assoc | Rocket launcher |
DE1254998B (en) * | 1964-04-20 | 1967-11-23 | Dornier System Gmbh | Altitude research rocket |
US3670621A (en) * | 1969-10-31 | 1972-06-20 | Alsco Inc | Rocket launcher fairing |
US3710678A (en) * | 1971-04-21 | 1973-01-16 | Saab Scania Ab | Jettisonable pod for aircraft carried rocket missiles |
US3841197A (en) * | 1972-12-13 | 1974-10-15 | Us Air Force | Foam structured rocket dispenser |
US4522356A (en) * | 1973-11-12 | 1985-06-11 | General Dynamics, Pomona Division | Multiple target seeking clustered munition and system |
US4342252A (en) * | 1980-03-25 | 1982-08-03 | General Dynamics, Pomona Division | Tandem rocket launcher |
CA1243897A (en) * | 1984-07-09 | 1988-11-01 | Charles J. Shea | Compact molded bulkhead for a tube-cluster rocket launcher |
US4604939A (en) * | 1984-08-20 | 1986-08-12 | The United States Of America As Represented By The Secretary Of The Army | Lightweight composite launcher pod |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB793927A (en) * | 1952-05-15 | 1958-04-23 | Fairey Aviat Co Ltd | Improvements relating to rocket containers for aircraft |
US2763189A (en) * | 1952-08-30 | 1956-09-18 | Northrop Aircraft Inc | Rocket and fuel pod |
US2844073A (en) * | 1954-04-16 | 1958-07-22 | Royal Industries | Launching device |
-
1959
- 1959-06-17 FR FR797786A patent/FR1318601A/en not_active Expired
-
1960
- 1960-06-10 GB GB20442/60A patent/GB939806A/en not_active Expired
- 1960-06-14 US US36074A patent/US3048086A/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2310800A1 (en) * | 1972-03-08 | 1973-09-13 | Ciba Geigy Ag | POLYOLEFINS STABILIZED WITH ORGANIC HYDRAZINE COMPOUNDS AND PHENOLIC ANTIOXYDANTS |
FR2707751A1 (en) * | 1984-04-17 | 1995-01-20 | Short Brothers Plc | Girl missile release device. |
Also Published As
Publication number | Publication date |
---|---|
US3048086A (en) | 1962-08-07 |
FR1318601A (en) | 1963-02-22 |
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