GB1282609A - Improvements in and relating to missile apparatus - Google Patents
Improvements in and relating to missile apparatusInfo
- Publication number
- GB1282609A GB1282609A GB56838/69A GB5683869A GB1282609A GB 1282609 A GB1282609 A GB 1282609A GB 56838/69 A GB56838/69 A GB 56838/69A GB 5683869 A GB5683869 A GB 5683869A GB 1282609 A GB1282609 A GB 1282609A
- Authority
- GB
- United Kingdom
- Prior art keywords
- missile
- fuselage
- motor
- launching
- secured
- 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
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
1282609 Self-propelling missile and launching means therefor; rockets PHILCO-FORD CORP 20 Nov 1969 [20 Nov 1968] 56838/69 Heading F3A and F3C A self-propelled missile, for use as a target, and its launching means, comprises a tubular fuselarge section 11 (Fig. 2) fitted over a launching tube 15 and secured thereto by frangible screws which break when a predetermined gas pressure is developed by a launching motor 32. A blast shield 16 is provided on the launching tube. Glass-fibre reinforced plastic fins 13 are secured to the fuselage by straps (17, Fig. 5, not shown) and contain further rocker motors 22 in their base portions. The fins are slightly inclined so as to rotate the missile in flight. The frangible screws 27, Fig. 3, extend between an annular member 33 fastened to the motor 32 and an annular member 31 threaded in an extension 26 of the launching tube. The motor 32 is secured in the fuselage 11 by a clamp 37 which pulls the member 33 against a wooden block 34 fast with the fuselage. The fuselage is made of cardboard lined with a thermally protective layer of aluminium. The motor 32 is electrically ignited and as the missile moves away from the launching tube plugs are withdrawn from an electrical circuit which then ignites the motors 22.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US77725068A | 1968-11-20 | 1968-11-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1282609A true GB1282609A (en) | 1972-07-19 |
Family
ID=25109712
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB56838/69A Expired GB1282609A (en) | 1968-11-20 | 1969-11-20 | Improvements in and relating to missile apparatus |
Country Status (4)
Country | Link |
---|---|
US (1) | US3605549A (en) |
DE (1) | DE1958355C3 (en) |
FR (1) | FR2023662A1 (en) |
GB (1) | GB1282609A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2239695A (en) * | 1986-07-01 | 1991-07-10 | Gen Electric | A round of ammunition |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA1131946A (en) * | 1977-09-07 | 1982-09-21 | Donald L. Smith | Shear pin release system |
US4333382A (en) * | 1979-12-26 | 1982-06-08 | The United States Of America As Represented By The Secretary Of The Navy | Boost assisted missile launcher |
RU2557125C2 (en) * | 2013-06-24 | 2015-07-20 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева | Aft body of aircraft with annular location of jet engine nozzles on its bottom protection (versions) |
CN114184091A (en) * | 2021-04-08 | 2022-03-15 | 西安龙飞电气技术有限公司 | Infrared radar dual-mode digital processing method for air-to-air missile seeker |
CN113218244A (en) * | 2021-05-11 | 2021-08-06 | 北京空天技术研究所 | Windproof locking mechanism |
-
1968
- 1968-11-20 US US777250A patent/US3605549A/en not_active Expired - Lifetime
-
1969
- 1969-10-07 FR FR6934190A patent/FR2023662A1/fr not_active Withdrawn
- 1969-11-20 GB GB56838/69A patent/GB1282609A/en not_active Expired
- 1969-11-20 DE DE1958355A patent/DE1958355C3/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2239695A (en) * | 1986-07-01 | 1991-07-10 | Gen Electric | A round of ammunition |
GB2239695B (en) * | 1986-07-01 | 1991-10-23 | Gen Electric | A round of ammunition. |
Also Published As
Publication number | Publication date |
---|---|
US3605549A (en) | 1971-09-20 |
DE1958355C3 (en) | 1974-08-22 |
DE1958355B2 (en) | 1974-01-24 |
DE1958355A1 (en) | 1970-05-27 |
FR2023662A1 (en) | 1970-08-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2310547A1 (en) | Missile with secondary charge ahead of main charge - has small charge on nose cone positioned not to disturb main explosion | |
GB1059356A (en) | A ground vehicle attack system | |
GB1262165A (en) | Hollow explosive charge missile | |
GB1282609A (en) | Improvements in and relating to missile apparatus | |
GB1522018A (en) | Assembly of a rocket-propelled missile and a retardation device | |
GB1174464A (en) | Device for Preventing Rotation of an Object in Space. | |
GB1296346A (en) | ||
GB1103580A (en) | Fairing | |
FR2308903A1 (en) | Mortar bomb having target guidance system - with shrapnel-forming shell and explosive charge and separate propellant charges | |
US3827655A (en) | Short range guided missile | |
GB1100354A (en) | Shaped charge device | |
GB938739A (en) | Improvements in systems comprising a cluster of rockets carried by a launching machine | |
GB961001A (en) | Improvements in propulsion units having a plurality of reaction propulsion nozzles | |
GB1108382A (en) | Self-propelled projectile | |
JPS52100800A (en) | Electric fuse | |
GB1135541A (en) | Improvements in rockets | |
GB1112260A (en) | A frangible high-altitude propulsion motor | |
FR1202054A (en) | Propulsion device for explosive projectile fired from a rifle | |
ES349178A1 (en) | A Hollow-Charge Missile. | |
US2986974A (en) | Ramming case for rockets in rifled naval guns | |
GB1029240A (en) | High-altitude research rocket | |
GB1011460A (en) | Improvements in an explosive shell or projectile with directed explosive effect | |
GB1085177A (en) | Improvements in rocket projectiles having a war-head | |
GB1352479A (en) | Rocket engine | |
FR2349817A1 (en) | Solid fuelled rocket charge ignition device - has arming charge to remove end of sleeve housing primary ignition charge |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PLNP | Patent lapsed through nonpayment of renewal fees |