DE1299541B - Launching device for rockets stored under the deck of a vehicle - Google Patents
Launching device for rockets stored under the deck of a vehicleInfo
- Publication number
- DE1299541B DE1299541B DEA48995A DEA0048995A DE1299541B DE 1299541 B DE1299541 B DE 1299541B DE A48995 A DEA48995 A DE A48995A DE A0048995 A DEA0048995 A DE A0048995A DE 1299541 B DE1299541 B DE 1299541B
- Authority
- DE
- Germany
- Prior art keywords
- cover plate
- deck
- rail
- missiles
- 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.)
- Pending
Links
- 235000015842 Hesperis Nutrition 0.000 title claims description 3
- 235000012633 Iberis amara Nutrition 0.000 title claims description 3
- 238000010276 construction Methods 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
Classifications
-
- 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
- F41A23/00—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles
- F41A23/20—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles for disappearing guns
-
- 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
- F41F3/0406—Rail launchers
-
- 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
- B63G1/00—Arrangements of guns or missile launchers; Vessels characterised thereby
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Conveying And Assembling Of Building Elements In Situ (AREA)
- Automatic Assembly (AREA)
Description
artige Tragrahmen stellen dann ein besonderes Kon- Die vorstehend beschriebene Abschußvorrichtung struktionsteil dar, das zusätzlichen Aufwand und vor 25 funktioniert auf folgende Weise: Wenn einer Deckallem zusätzlichen Raum erfordert. platte eine aus Abschußschiene und Rakete be- like support frames then provide a special con- The launching device described above Structural part, the extra effort and before 25 works in the following way: When a deck requires all the extra space. plate is loaded with a launching rail and a rocket
Die Erfindung hat die Aufgabe, die in diesem Zu- stehende Einheit zugeführt worden ist, wird diese in sammenhang bestehenden Nachteile und Schwierig- die gewünschte Stellung höhengerichtet, wonach die keiten zu beseitigen, und sie schlägt hierzu für die Rakete verschossen werden kann. Wenn der AbAusbildung eines Fahrzeugdecks vor, daß eine läng- 30 schuß beendet ist, wird die Deckplatte in ihre Ausliche Deckplatte vorgesehen ist, die in Ruhestellung gangsstellung gesenkt. Die Deckplatte führt dabei die mit dem übrigen Deck niveaugleich und um eine noch verbliebene Abschußschiene mit sich. In abQuerachse aufrichtbar ist, wobei sie die Führungs- gesenkter Stellung übernimmt das Magazin die leere einrichtungen für eine oder mehrere Raketen in an Abschußschiene und führt der Deckplatte eine neue sich bekannter Weise auf der Unterseite trägt. 35 Abschußschiene mit Rakete zu.The invention has the object that has been supplied in this state of the unit, this is in related disadvantages and difficulties- the desired position in elevation, after which the abilities to eliminate, and it suggests this for the missile can be fired. When the training of a vehicle deck that a longitudinal shot has ended, the cover plate is in its recess Cover plate is provided, the starting position lowered in the rest position. The cover plate guides the level with the rest of the deck and around a remaining launching rail with it. In the transverse axis is erectable, taking the guide lowered position, the magazine takes over the empty one facilities for one or more missiles in on launching rail and leads the cover plate a new one is known to wear on the underside. 35 launch rail with missile closed.
Die längliche Deckplatte des Fahrzeugdecks stellt Bei einer Abschußvorrichtung der vorstehend beein
Konstruktionselement dar, das vom Platzaufwand schriebenen Art ist es besonders vorteilhaft, ein
her gesehen zum Fahrzeugdeck gehört und deshalb horizontales Trommelmagazin anzuwenden, das
in jedem Fall vorhanden ist. Es erübrigt sich also einen Magazinrotor mit zwei Rotorgabeln enthält. In
eine zusätzliche Tragvorrichtung od. dgl., und es ist 40 dem Magazin ruht die Rakete mit Abschußschiene in
nur erforderlich, das betreffende Stück des Fahrzeug- am Umkreis liegenden Fächern, und zwar so, daß
decks aufrichtbar zu lagern. Die längliche Deckplatte jede Einheit nur mit den Enden der Abschußschiene
hat somit eine Doppelfunktion. Vorteilhaft ist es in den Rotorgabeln des Magazinrotors ruht. Die
ferner, daß die längliche Deckplatte wegen ihres leere Abschußschiene wird von dem Magazin aufniveaugleichen
Abschlusses mit dem Fahrzeugdeck 45 genommen, das danach bei einer Weiterdrehung um
kaum erkennbar ist, d, h., daß sie eine optimale eine Stufe eine neue Abschußschiene mit Rakete der
Tarnung für eine Raketenabschußvorrichtung dar- Führung 6 der Deckplatte 3 zuführt,
stellt. Ebenfalls vorteilhaft ist aber auch die Tatsache, daß bei einem begehbaren Fahrzeugdeck die Patentansprüche:
Raketenabschußvorrichtung im Ruhezustand über- 50The elongated cover plate of the vehicle deck is in a launching device of the above-mentioned construction element, the type described in terms of space requirements, it is particularly advantageous to use a seen from the vehicle deck and therefore use a horizontal drum magazine, which is present in any case. There is therefore no need for a magazine rotor with two rotor forks. In an additional support device or the like, and it is 40 the magazine rests the rocket with launching rail in only necessary to store the relevant piece of the vehicle on the periphery of the compartments, in such a way that decks can be erected. The elongated cover plate of each unit with only the ends of the launching rail thus has a double function. It is advantageous that it rests in the rotor forks of the magazine rotor. Furthermore, that the elongated cover plate, because of its empty launching rail, is taken from the magazine level with the vehicle deck 45, which is then barely noticeable when you turn it further, i.e. that it is an optimal one step a new launching rail with rocket Camouflage for a rocket launcher dar- guide 6 of the cover plate 3 supplies,
represents. However, it is also advantageous that, in the case of a vehicle deck that can be walked on, the claims:
Missile launcher at rest over 50
haupt nicht stört, d. h., daß die Bewegungsfreiheit 1. Abschußvorrichtung für unter dem Deckdoesn't bother at all, d. That is, the freedom of movement 1. Launching device for below deck
auf dem Fahrzeugdeck nicht beeinträchtigt ist. eines Fahrzeugs gespeicherte Raketen, dadurchon the vehicle deck is not impaired. missiles stored in a vehicle, thereby
Bei einer solchen Deckplatte ist auch das Be- gekennzeichnet, daß eine längliche Deckfestigen einer Rakete und ihrer Abschußschiene sehr platte (2,3) vorgesehen ist, die in Ruhestellung einfach. Für eine solche Befestigung, die meist im 55 mit dem übrigen Deck niveaugleich und um eine Ruhezustand der Deckplatte, also von dem unter Querachse aufrichtbar ist, wobei sie die Fühdem Deck liegenden Magazin aus, vorgenommen rungseinrichtungen (7, 8,9,10,11) für eine oder wird, wird besonders wenig Arbeitsraum bean- mehrere Raketen (12) in an sich bekannter Weise spracht, wenn Rakete und Abschußschiene eine Ein- auf der Unterseite trägt.Such a cover plate is also characterized by the fact that an elongate cover is strengthened a rocket and its launch rail very plate (2,3) is provided in the rest position simple. For such an attachment, which is usually at the same level in the 55 as the rest of the deck and around one Idle state of the cover plate, that is to say from which it can be erected under the transverse axis, with the Fühdem Deck lying magazine from, made approximately devices (7, 8,9,10,11) for one or is, particularly little work space is required. Several rockets (12) in a manner known per se spoke when the rocket and launch rail have an insert on the underside.
heit bilden, die an die Deckplatte durch eine Be- 60 2. Abschußvorrichtung nach Anspruch 1, dawegung ansetzbar ist, die parallel zum Deck und durch gekennzeichnet, daß Rakete (12) und Abrechtwinklig zur Längsachse der Rakete verläuft. schußschiene (11) eine Einheit bilden, die an dieunit that is attached to the cover plate by a loading 60 2. launching device according to claim 1, dawegung can be attached, which is parallel to the deck and characterized in that rocket (12) and Abrechtwinkelig runs to the longitudinal axis of the missile. weft rail (11) form a unit that is attached to the
Nachfolgend wird ein Ausführungsbeispiel der Er- Deckplatte (2, 3) durch eine Bewegung ansetzbarIn the following, an embodiment of the Er cover plate (2, 3) can be attached by a movement
findung für die Anwendung bei einem Schiffsdeck an ist, die parallel zum Deck (1) und rechtwinkligFinding for use on a ship deck is parallel to the deck (1) and at right angles
Hand der Zeichnung beschrieben. 65 zur Längsachse der Rakete verläuft.Hand outlined drawing. 65 runs to the longitudinal axis of the missile.
Hierzu 1 Blatt Zeichnungen1 sheet of drawings
Claims (1)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE561964 | 1964-05-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE1299541B true DE1299541B (en) | 1969-07-17 |
Family
ID=20266846
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DEA48995A Pending DE1299541B (en) | 1964-05-06 | 1965-04-21 | Launching device for rockets stored under the deck of a vehicle |
Country Status (2)
Country | Link |
---|---|
US (1) | US3340768A (en) |
DE (1) | DE1299541B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3101729A1 (en) * | 1981-01-21 | 1982-08-05 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Device for firing missiles on a helicopter |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1299542B (en) * | 1964-05-06 | 1969-07-17 | Bofors Ab | Missile launcher |
US4471684A (en) * | 1981-09-14 | 1984-09-18 | Fmc Corporation | Transom missile launcher module |
IL169481A (en) * | 2005-06-30 | 2011-11-30 | Rafael Advanced Defense Sys | Mobile carrier for a projectile launcher |
US7854189B1 (en) * | 2007-10-16 | 2010-12-21 | The United States Of America As Represented By The Secretary Of The Navy | Modular missile launching assembly |
FR2934041B1 (en) * | 2008-07-17 | 2011-07-01 | Dcns | ARMS SYSTEM, IN PARTICULAR FOR MISSILES, INTENDED TO BE INTEGRATED INTO A COMBAT PLATFORM AND CORRESPONDING COMBAT PLATFORM |
FR3013031B1 (en) * | 2013-11-12 | 2016-08-26 | Dcns | NAVAL PLATFORM EQUIPPED WITH AT LEAST ONE CONTAINER FORMING ROCKET LOADER |
RU2701366C2 (en) * | 2017-11-14 | 2019-09-25 | Борис Никифорович Сушенцев | Delivery rocket carrier (embodiments), highly manoeuvrable aircraft (embodiments) and method of contactless combat operations |
ES2904307T3 (en) * | 2019-02-21 | 2022-04-04 | John Cockerill Defense S A | Stealth vehicle with integrated rapid deployment weapon system |
CN113218246B (en) * | 2021-05-20 | 2022-11-08 | 鲁东大学 | Offshore rocket thermal launching erecting device and erecting method |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2549778A (en) * | 1945-12-14 | 1951-04-24 | Crawley Blick | Projectile launching |
DE920403C (en) * | 1951-06-26 | 1954-11-22 | Bofors Ab | Holding device for missiles |
GB730754A (en) * | 1953-07-09 | 1955-05-25 | Georges Even | Improvements in or relating to armoured vehicles |
US2981150A (en) * | 1954-06-15 | 1961-04-25 | Jr Arthur H Miller | Launcher |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2568455A (en) * | 1945-03-28 | 1951-09-18 | Frederick C Lindvall | Rocket launcher |
US2624946A (en) * | 1946-04-30 | 1953-01-13 | John M Miller | Telescope gun sight mount |
US2709947A (en) * | 1949-03-10 | 1955-06-07 | Bell Aircraft Corp | Aircraft and armament therefor |
US2978959A (en) * | 1953-05-27 | 1961-04-11 | Robert E Carlberg | Self-aligning guide for loading in missile launching systems |
US3099936A (en) * | 1961-02-27 | 1963-08-06 | Arthur J Gaborc | Self-aligning loading rail |
US3215040A (en) * | 1963-03-26 | 1965-11-02 | Robert L Kossan | Adapter rail |
-
1965
- 1965-04-21 DE DEA48995A patent/DE1299541B/en active Pending
- 1965-05-03 US US452821A patent/US3340768A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2549778A (en) * | 1945-12-14 | 1951-04-24 | Crawley Blick | Projectile launching |
DE920403C (en) * | 1951-06-26 | 1954-11-22 | Bofors Ab | Holding device for missiles |
GB730754A (en) * | 1953-07-09 | 1955-05-25 | Georges Even | Improvements in or relating to armoured vehicles |
US2981150A (en) * | 1954-06-15 | 1961-04-25 | Jr Arthur H Miller | Launcher |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3101729A1 (en) * | 1981-01-21 | 1982-08-05 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Device for firing missiles on a helicopter |
Also Published As
Publication number | Publication date |
---|---|
US3340768A (en) | 1967-09-12 |
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