GB1221461A - Device for interlocking a container with a missile to a launching device - Google Patents

Device for interlocking a container with a missile to a launching device

Info

Publication number
GB1221461A
GB1221461A GB24720/68A GB2472068A GB1221461A GB 1221461 A GB1221461 A GB 1221461A GB 24720/68 A GB24720/68 A GB 24720/68A GB 2472068 A GB2472068 A GB 2472068A GB 1221461 A GB1221461 A GB 1221461A
Authority
GB
United Kingdom
Prior art keywords
claws
tube
bridge
pair
launching
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
GB24720/68A
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm 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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB1221461A publication Critical patent/GB1221461A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets
    • F41F3/052Means for securing the rocket in the launching apparatus
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/30Command link guidance systems
    • F41G7/301Details

Abstract

1,221,461. Releasable fastenings. MESSER SCHMITT-BOLKOW BLOHM. G.m.b.H. 23 May, 1968 [24 May, 1967], No. 24720/68. Heading E2A. [Also in. Divisions F3 and F4] A device 1 for mounting a launching tube for a guided missile on a launching device comprises a receiver 2 having two pairs of claws 30, 31; 32, 33, one pair at each end. The claws of each pair being mounted for movement towards and away from one another such that they may grip and release a launching. tube. The claws 30, 31, 32 33 are preferably resiliently mounted as on the ends of ap air of torsion bars 16 and are actuated to grip the firing tube under the action of energy storage means, e.g. springs 53. The claws in their movement from the open to the locking position pass through an intermediate position in which the claws may be held by a spring loaded ball and socket device (Fig. 4, not shown) in the actuating linkage and a bearing 20 of the receiver respectively. A firing tube having a longitudinal bead containing the service connections to the rocket end with a wedge shaped forward, and can, in the intermediate position of the claws, be urged between the claws to position the claws in cut out portions of the bead (Fig. 6, not shown). Electrical coupling means is also provided. In the construction shown the actuating means comprises a bridge 40 secured to a traction tube 47 and having pins 42, 44 which ride in diametrically opposite driving grooves 23, 24 in a pair of cylinders 22, one cylinder being connected to each torsion bar 16. The bridge 40 is moved between its two end positions by a manual actuating device and is held in both positions by a releasable catch 56 which co-operates with a guide ring 72 in the claw open position when a pressure plate by the action of a pin of the traction tube compresses springs 53. The bridge is further secured to a pair of guide bars 76 which through the sliding connection of 4 pins 81 of an electrical connecting plug 75 and slots 78 therein raises the plug 75 to provide the electrical coupling. The driving groove engaging pins 42, 44 may be actuated by fluid pressure operated, opposed pistons (Fig. 5, not shown) microswitches controlling the actuation by operated cam bars connected to the bridge. A lever may be provided on a claw at each end of the device to allow a locked tube to be removed from the device.
GB24720/68A 1967-05-24 1968-05-23 Device for interlocking a container with a missile to a launching device Expired GB1221461A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEB0092689 1967-05-24

Publications (1)

Publication Number Publication Date
GB1221461A true GB1221461A (en) 1971-02-03

Family

ID=6986530

Family Applications (1)

Application Number Title Priority Date Filing Date
GB24720/68A Expired GB1221461A (en) 1967-05-24 1968-05-23 Device for interlocking a container with a missile to a launching device

Country Status (4)

Country Link
US (1) US3459100A (en)
FR (1) FR1565969A (en)
GB (1) GB1221461A (en)
SE (1) SE332765B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2102839A5 (en) * 1970-08-25 1972-04-07 Even Georges
US4470336A (en) * 1982-08-05 1984-09-11 General Dynamics, Pomona Division Armored missile launch/shipping container
FR2638227B1 (en) * 1988-10-21 1993-11-05 Thomson Brandt Armements ON-BOARD UNDER-AMMUNITION HOLDING SYSTEM
US5129308A (en) * 1989-03-21 1992-07-14 Fuereder Georg F Combat vehicle with extendible combat platform
US8181906B2 (en) * 2009-04-02 2012-05-22 Raytheon Company Method and apparatus for ram deceleration in a launch system
RU193224U1 (en) * 2019-02-11 2019-10-17 Акционерное общество "Научно-производственное предприятие "Старт" им. А.И. Яскина" RUNNING-CLOSING DEVICE FOR RUNNING UNIT COVER

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2972933A (en) * 1957-12-23 1961-02-28 Gen Dynamics Corp Missile hand launching system
DE1266665B (en) * 1966-06-15 1968-04-18 Boelkow Gmbh Launching and steering device for recoil-propelled missiles starting from launch tubes with detachable visor carrier

Also Published As

Publication number Publication date
SE332765B (en) 1971-02-15
US3459100A (en) 1969-08-05
DE1553987A1 (en) 1971-05-19
FR1565969A (en) 1969-05-02

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