DE3917480A1 - Submarine launch of guided missile - involves launch vehicle with hydrodynamic brakes - Google Patents
Submarine launch of guided missile - involves launch vehicle with hydrodynamic brakesInfo
- Publication number
- DE3917480A1 DE3917480A1 DE19893917480 DE3917480A DE3917480A1 DE 3917480 A1 DE3917480 A1 DE 3917480A1 DE 19893917480 DE19893917480 DE 19893917480 DE 3917480 A DE3917480 A DE 3917480A DE 3917480 A1 DE3917480 A1 DE 3917480A1
- Authority
- DE
- Germany
- Prior art keywords
- underwater vehicle
- submarine
- launching
- launch
- vehicle according
- 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.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
- B63G8/28—Arrangement of offensive or defensive equipment
- B63G8/30—Arrangement of offensive or defensive equipment of artillery or missile launching means
-
- 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
- F42B15/20—Missiles having a trajectory beginning below water surface
Abstract
Description
Die Erfindung betrifft ein Unterwasserfahrzeug gemäß den Merkmalen des Oberbegriffs von Anspruch 1.The invention relates to an underwater vehicle according to the Features of the preamble of claim 1.
Raketenabschüsse von einem U-Boot aus sind allgemein be kannt, wobei besonders bei Unterwasserabschüssen die bord eigenen Torpedorohre verwendet werden. Problematisch werden derartige Abschüsse, wenn torpedoähnliche Unterwasserfahr zeuge als Startplattformen benutzt werden sollen. Die auf tretenden Rückstoßkräfte der startenden Raketen bewirken rückwärtsgerichtete Beschleunigungen und Bewegungen dieser Unterwasserfahrzeuge, die die Abschußlagen in unerwünschter Weise verändern.Missile launches from a submarine are common knows, especially with underwater launches the board own torpedo tubes can be used. Become problematic such kills when torpedo-like underwater travel witnesses should be used as starting platforms. The on the recoil forces of the launching rockets backward accelerations and movements of these Submarine vehicles, the launch sites in undesirable Change wise.
Der Erfindung liegt die Aufgabe zugrunde, ein Unterwasser fahrzeug der eingangs genannten Art derart auszubilden, daß bei einem Raketenstart rückwärtsgerichtete Beschleunigungen und Bewegungen verhindert bzw. gedämpft werden.The invention has for its object an underwater Train vehicle of the type mentioned in such a way that backward accelerations at a rocket launch and movements are prevented or dampened.
Die Aufgabe wird erfindungsgemäß durch die kennzeichnenden Teilmerkmale von Anspruch 1 gelöst.The object is achieved by the characterizing Part features of claim 1 solved.
Ein wesentlicher Vorteil der Erfindung besteht darin, daß die im Moment eines Raketenstarts angeströmten Tragflächen bzw. Wirbelbremsflächen, wobei die entstehenden Kräfte zur Stabilisierung des Fahrzeugs dienen, während einer Unterwas serfahrt als Tragflächen zur Neutralisierung des Untertriebs verwendet werden können. Die Benutzung mehrerer Tragflächen gleichzeitig zur Erzeugung eines Gegenmomentes zur Pro pellerdrehrichtung sowie zur Steuerung des Fahrzeugs ist möglich.A major advantage of the invention is that the wings that are flown at the moment of a rocket launch or vortex braking surfaces, the resulting forces to Stabilize the vehicle while underwater serfahrt as wings to neutralize the underdrive can be used. The use of multiple wings at the same time to generate a counter torque to the Pro direction of rotation and control of the vehicle possible.
Ausgestaltungen der Erfindung sind in den Unteransprüchen 2 bis 7 beschrieben.Embodiments of the invention are in the subclaims 2 to 7 described.
In der Zeichnung ist ein Ausführungsbeispiel nach der Er findung dargestellt, und zwar zeigtIn the drawing is an embodiment according to the Er shown, namely shows
Fig. 1 den Startvorgang einer Rakete aus einem Unter wasserfahrzeug, und Fig. 1, the launch process of a rocket from an underwater vehicle, and
Fig. 2 eine aus einer Fahrzeugoberfläche ausschwenk bare Tragfläche im Halbschnitt. Fig. 2 a swing out of a vehicle surface bare wing in half section.
In Fig. 1 befindet sich ein torpedoähnliches Unterwasser fahrzeug 1 in etwa senkrechter Abschußlage zu einer Wasser oberfläche. Dieses Unterwasserfahrzeug 1 kann aus einem Torpedorohr eines zeichnerisch nicht dargestellten U-Bootes verbringbar sein, es ist über eine Signalleitung 2, vorzugs weise einen Lichtwellenleiter, mit dem U-Boot verbunden, von wo aus die Fortbewegung des Unterwasserfahrzeuges 1 und/oder ein Raketenstartvorgang steuerbar ist. Es ist auch möglich, daß das Unterwasserfahrzeug 1 ein Ziel selbständig ansteuert und/oder einen Raketensteuervorgang selbständig durchführt.In Fig. 1 is a torpedo-like underwater vehicle 1 in an approximately vertical launch position to a water surface. This underwater vehicle 1 can be brought out of a torpedo tube of a submarine (not shown in the drawing); it is connected to the submarine via a signal line 2 , preferably an optical waveguide, from where the movement of the underwater vehicle 1 and / or a rocket launch process can be controlled is. It is also possible for the underwater vehicle 1 to independently target a target and / or to carry out a rocket control process independently.
Die startende Rakete 3 erzeugt eine durch einen Pfeil gekennzeichnete Rückstoßkraft auf das Unterwasserfahrzeug 1. Um der durch den Rückstoß verursachten Bewegung des Unter wasserfahrzeuges 1 entgegenzuwirken und das Unterwasser fahrzeug im Verlauf des Raketenstarts in seiner Abschußlage zu stabilisieren, befinden sich mehrere an dem Unterwasser fahrzeug 1 angeordnete hydrodynamisch-profilierte Tragflächen 4 im ausgefahrenen Zustand. Dieses bedeutet, daß die Trag flächen 4 unter einem durch die Rückstoßkraft der startenden Rakete bestimmten Anstellwinkel α gegenüber der Fahrzeug oberfläche anstehen, was aus Fig. 2 in vergrößerter Dar stellung zu entnehmen ist. Die Tragflächen 4 können in die Oberfläche des Unterwasserfahrzeuges eingefahren werden, beispielsweise durch Verschwenkung um eine Achse 5 oder durch Drehung um ein oder mehrere Achsen, so daß sie prak tisch in die Oberfläche integriert sind und eine ungewollte Behinderung bei einer Fortbewegung des Unterwasserfahrzeuges 1 verhindert wird.The launching rocket 3 generates a recoil force on the underwater vehicle 1 indicated by an arrow. To counteract the movement of the underwater vehicle 1 caused by the recoil and to stabilize the underwater vehicle in the course of the rocket launch in its firing position, there are several hydrodynamically profiled wings 4 arranged on the underwater vehicle 1 in the extended state. This means that the support surfaces 4 are at a certain angle of attack by the recoil force of the rocket launching α against the vehicle surface, which can be seen from Fig. 2 in an enlarged Dar position. The wings 4 can be retracted into the surface of the underwater vehicle, for example by pivoting about an axis 5 or by rotation about one or more axes, so that they are practically integrated into the surface and an unwanted obstacle to the locomotion of the underwater vehicle 1 is prevented .
Claims (7)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19893917480 DE3917480A1 (en) | 1989-05-30 | 1989-05-30 | Submarine launch of guided missile - involves launch vehicle with hydrodynamic brakes |
FR9006562A FR2647747A1 (en) | 1989-05-30 | 1990-05-28 | UNDERWATER VEHICLE USING LAUNCHING PLATFORM FOR MISSILES |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19893917480 DE3917480A1 (en) | 1989-05-30 | 1989-05-30 | Submarine launch of guided missile - involves launch vehicle with hydrodynamic brakes |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3917480A1 true DE3917480A1 (en) | 1990-12-06 |
Family
ID=6381626
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19893917480 Withdrawn DE3917480A1 (en) | 1989-05-30 | 1989-05-30 | Submarine launch of guided missile - involves launch vehicle with hydrodynamic brakes |
Country Status (2)
Country | Link |
---|---|
DE (1) | DE3917480A1 (en) |
FR (1) | FR2647747A1 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1617168A1 (en) * | 2004-07-15 | 2006-01-18 | LFK-Lenkflugkörpersysteme GmbH | Hydrodynamic device on a floating coil body |
DE102005041177A1 (en) * | 2004-09-08 | 2006-06-22 | Christoph Gerstenhauer | Floating launch system for spacecraft has tube that is closed at the bottom floating upright or inclined in water as launch system for spacecraft, is held stable by grid construction |
RU2521447C1 (en) * | 2013-04-11 | 2014-06-27 | Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | Launching of drone from submarine |
RU2532279C1 (en) * | 2013-04-11 | 2014-11-10 | Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | Submarine |
CN116202378A (en) * | 2023-04-03 | 2023-06-02 | 北京理工大学 | Water-beating rebound lift-increasing device for anti-ship missile |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2950026A1 (en) * | 2009-08-25 | 2011-03-18 | Univ Sud Toulon Var | METHOD AND SYSTEM FOR LAUNCHING TACTICAL OR STRATEGIC DEVICES HAVING AN AIRSPACE FROM THE SUBMARINE ENVIRONMENT |
CN112455674B (en) * | 2020-11-10 | 2022-06-10 | 南京航空航天大学 | Working method of aircraft water-based take-off and landing platform based on vector propulsion |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3087386A (en) * | 1961-03-23 | 1963-04-30 | Robert D Rung | Adapter for missile launcher |
US3499364A (en) * | 1959-11-19 | 1970-03-10 | Us Navy | Apparatus for submerged launching of missiles |
DE2634462C1 (en) * | 1976-07-31 | 1983-11-17 | Licentia Gmbh | Submarine weapon system |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1072883A (en) * | 1964-11-27 | 1967-06-21 | Burndept Electronics Ltd | Radio rescue beacon |
-
1989
- 1989-05-30 DE DE19893917480 patent/DE3917480A1/en not_active Withdrawn
-
1990
- 1990-05-28 FR FR9006562A patent/FR2647747A1/en not_active Withdrawn
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3499364A (en) * | 1959-11-19 | 1970-03-10 | Us Navy | Apparatus for submerged launching of missiles |
US3087386A (en) * | 1961-03-23 | 1963-04-30 | Robert D Rung | Adapter for missile launcher |
DE2634462C1 (en) * | 1976-07-31 | 1983-11-17 | Licentia Gmbh | Submarine weapon system |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1617168A1 (en) * | 2004-07-15 | 2006-01-18 | LFK-Lenkflugkörpersysteme GmbH | Hydrodynamic device on a floating coil body |
DE102005041177A1 (en) * | 2004-09-08 | 2006-06-22 | Christoph Gerstenhauer | Floating launch system for spacecraft has tube that is closed at the bottom floating upright or inclined in water as launch system for spacecraft, is held stable by grid construction |
RU2521447C1 (en) * | 2013-04-11 | 2014-06-27 | Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | Launching of drone from submarine |
RU2532279C1 (en) * | 2013-04-11 | 2014-11-10 | Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | Submarine |
CN116202378A (en) * | 2023-04-03 | 2023-06-02 | 北京理工大学 | Water-beating rebound lift-increasing device for anti-ship missile |
CN116202378B (en) * | 2023-04-03 | 2024-04-09 | 北京理工大学 | Water-beating rebound lift-increasing device for anti-ship missile |
Also Published As
Publication number | Publication date |
---|---|
FR2647747A1 (en) | 1990-12-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8110 | Request for examination paragraph 44 | ||
8127 | New person/name/address of the applicant |
Owner name: STN SYSTEMTECHNIK NORD GMBH, 2800 BREMEN, DE |
|
8139 | Disposal/non-payment of the annual fee |