EP2090859A3 - Launcher with at least one start tube for rocket-propelled missiles - Google Patents
Launcher with at least one start tube for rocket-propelled missiles Download PDFInfo
- Publication number
- EP2090859A3 EP2090859A3 EP20090002082 EP09002082A EP2090859A3 EP 2090859 A3 EP2090859 A3 EP 2090859A3 EP 20090002082 EP20090002082 EP 20090002082 EP 09002082 A EP09002082 A EP 09002082A EP 2090859 A3 EP2090859 A3 EP 2090859A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- gas generator
- launcher
- rocket
- pipe
- serving
- 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.)
- Granted
Links
- 239000006096 absorbing agent Substances 0.000 abstract 1
- 230000001133 acceleration Effects 0.000 abstract 1
- 230000035939 shock Effects 0.000 abstract 1
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
- F41F3/0413—Means for exhaust gas disposal, e.g. exhaust deflectors, gas evacuation systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A1/00—Missile propulsion characterised by the use of explosive or combustible propellant charges
- F41A1/08—Recoilless guns, i.e. guns having propulsion means producing no recoil
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A25/00—Gun mountings permitting recoil or return to battery, e.g. gun cradles; Barrel buffers or brakes
- F41A25/06—Friction-operated systems
-
- 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
- F41F3/042—Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Werfer mit mindestens einem Startrohr (12) für raketenbetriebene Flugkörper, die ihre Startbeschleunigung und einen Anfangsdrall mittels eines im axial gefesselten Startrohr (12) befindlichen Gasgenerator (15)(Booster) erhalten, mit einer am abgewandtem Ende des Startrohres (12) dem Austritt des Gasvolumenstromes des Gasgenerators dienenden Lavaldüse (13) mit nachgeordneter Lavaldüsen-Anordnung (30) und mit einem dem Gasgenerator zugeordneten der Rückstoßkompensation des Startrohres (12) dienenden gestellfesten Schockabsorbers (17) aus zwei koaxialen Führungshülsen (18, 19), von denen die eine (18) gestellfest und die zweite, relativ dazu beweglich gelagert ist, zwischen denen ein Rücklaufweg und -zeit bestimmende Reibungs-Ringfeder (20)sich befindet. Launcher with at least one launch tube (12) for rocket - propelled missiles, which receive their start acceleration and an initial twist by means of a gas generator (15) (booster) located in the axially bounded start pipe (12), with one at the opposite end of the start pipe (12) the exit of the Gas volume flow of the gas generator serving Laval nozzle (13) with downstream Laval nozzle arrangement (30) and with a gas generator associated the recoil compensation of the starting pipe (12) serving frame-fixed shock absorber (17) of two coaxial guide sleeves (18, 19), of which the one ( 18) fixed to the frame and the second, is movably mounted relative thereto, between which a return path and time-determining friction ring spring (20) is located.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200810009638 DE102008009638B3 (en) | 2008-02-18 | 2008-02-18 | Launcher with at least one launch tube for rocket-propelled missiles |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2090859A2 EP2090859A2 (en) | 2009-08-19 |
EP2090859A3 true EP2090859A3 (en) | 2013-05-29 |
EP2090859B1 EP2090859B1 (en) | 2015-06-03 |
Family
ID=40578863
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP09002082.7A Active EP2090859B1 (en) | 2008-02-18 | 2009-02-14 | Launcher with at least one start tube for rocket-propelled missiles |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP2090859B1 (en) |
DE (1) | DE102008009638B3 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102010006493B4 (en) * | 2010-02-02 | 2012-04-26 | Diehl Bgt Defence Gmbh & Co. Kg | Container for a jet-propelled missile |
CN112644801A (en) * | 2020-09-21 | 2021-04-13 | 中山市哈工朗德智能科技有限公司 | Novel horizontal sealing guide device |
CN116006360B (en) * | 2022-12-03 | 2024-04-09 | 中国科学院力学研究所 | Special-shaped Laval micro-spray pipe |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE695584C (en) * | 1933-11-05 | 1940-08-28 | Mauser Werke Ag | Machine gun with movable barrel |
DE716385C (en) * | 1939-03-04 | 1942-01-19 | Mauser Werke Ag | Friction ring spring with enlarged work destruction, especially for the weapon industry |
DE1428637C1 (en) * | 1964-02-26 | 1975-02-20 | Messerschmitt Boelkow Blohm | Tubular launcher for projectiles, especially for missiles |
US4106389A (en) * | 1976-05-14 | 1978-08-15 | British Aircraft Corporation | Aircraft weapon mountings |
GB2121149A (en) * | 1982-05-27 | 1983-12-14 | British Aerospace | Missile housing and launch arrangement |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH450228A (en) * | 1965-10-22 | 1968-01-15 | Transurvey Holding Company Inc | Device for launching a projectile |
US6352030B1 (en) * | 1998-11-12 | 2002-03-05 | Cordant Technologies Inc. | Gas generating eject motor |
-
2008
- 2008-02-18 DE DE200810009638 patent/DE102008009638B3/en not_active Expired - Fee Related
-
2009
- 2009-02-14 EP EP09002082.7A patent/EP2090859B1/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE695584C (en) * | 1933-11-05 | 1940-08-28 | Mauser Werke Ag | Machine gun with movable barrel |
DE716385C (en) * | 1939-03-04 | 1942-01-19 | Mauser Werke Ag | Friction ring spring with enlarged work destruction, especially for the weapon industry |
DE1428637C1 (en) * | 1964-02-26 | 1975-02-20 | Messerschmitt Boelkow Blohm | Tubular launcher for projectiles, especially for missiles |
US4106389A (en) * | 1976-05-14 | 1978-08-15 | British Aircraft Corporation | Aircraft weapon mountings |
GB2121149A (en) * | 1982-05-27 | 1983-12-14 | British Aerospace | Missile housing and launch arrangement |
Also Published As
Publication number | Publication date |
---|---|
EP2090859A2 (en) | 2009-08-19 |
DE102008009638B3 (en) | 2009-09-03 |
EP2090859B1 (en) | 2015-06-03 |
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