9M96E2-2 type ground-to-air missile launch canister

Abstract

A launch canister comprises a housing in which a 9M96E (2) ground-to-air missile, an upper fixing strap, a lower fixing strap and an external connector are arranged, the structure, the size and the position of the housing are the same as those of straps and connectors of transport launch containers (TLC) of 5B55E, 48H6E and 40H6E missiles, and a base, transport launch containers for supporting a load on the ground during launch of a missile from a launch canister. The external connector of the 9M96E (2) missile is coupled with the external connector of the launch canister through a switching device, and the switching device comprises a multiplexing channel splitter used for transmitting information to the missiles in the launch canister and a distribution board used for setting identification numbers of the missiles in the 35P6E and 40P6E missile systems through jumpers. According to the launch canister, at most four transportation launch containers of ground-to-air missiles with 9M96E (2) can be integrated into a box, and the box is installed for a single installation module of the transportation launch containers of 5E55E, 48H6E and 40H6E missiles. The method has the technical effect that the ammunition cardinal number of 35P6E and 40P6E missile systems is increased by four times.

Description

Technical Field

[0001] The present invention relates to the field of military technology, specifically to guided projectiles and missiles, and can be used in the development of guided projectiles and missiles. Background Art

[0002] The following domestic surface-to-air missiles (SAMs) are known: 1Д...22Д, В-800, В-850, В-1000, 5Я23, 5Я26, 5Я27, 5В21, 5В24, 5В27, 5В28, 5В29, 5В55, 48Н6, 9МЗЗ, 9М330, 9М331, 4К60, 4К90, 4К91, 5В61, 51Т6, 53Т6, 55Т6, and foreign missiles RIM-7, RIM-66C, M, RIM-67C, RIM-116A, RIM-156A, RIM-162, RIM-300, Aster-15, 30, Sea Dart Mk2, HQ-65, Masurca, Sea Wolf VL, Sea Strike, MIKA-VL.

[0003] The relevant technical content of these missiles is recorded in the following documents with different degrees of publicity: "History of Aviation Weapons" (Minsk, 1999), "Torch Missile" (Moscow, Design Bureau "Torch" of Academician P.D. Grushin, 2003), "Analysis and Review of Naval Shipbuilding and Weaponry" No. 3(152) (Naval Military Education and Research Center "Naval Academy named after Admiral of the Soviet Navy N.G. Kuznetsov", St. Petersburg, 2013), "Surface-to-Air Missiles" (Russian Weaponry, 2010), and http: / / military.russia.ru, http: / / pvo.guns.ru, also seen in "Air Defense Missile Design" (Moscow: Moscow Aviation Institute, 1999), "Wings of the Motherland", No. 8, 1993, "Technology and Weaponry. Yesterday. Today. Tomorrow..." No. 5-6, 1999 and other publications.

[0004] The main feature of all existing surface-to-air missiles is that a specially designed dedicated launcher is used to carry out the launch operation of this type of missile.

[0005] The technical solution for realizing the sharing of launchers by multiple types of missiles for the first time is seen in the 5П85Е and 51П6Е launchers configured in the 35Р6Е and 40Р6Е systems. The technical feasibility stems from the fact that the 48Н6Е, 48Н6Е2, 48Н6Е3, and 40Н6Е missiles are all improved models of the 5В55Е missile, mainly upgrading the on-board equipment. The above-mentioned missiles adopt a unified aerodynamic layout design, have similar mass and dimension characteristics, and use the same transportation and launch tube (TLC) and launch mechanism design scheme, thus enabling them to be launched from the same launch tube.

[0006] The 9M334E launcher, as the closest prior art to the present invention, uses a single unit containing four 9M330E (9M331E) missiles. This missile was developed specifically for the Tor missile system. This launcher is used to increase the reload speed of the missile system launcher. However, whether loaded singly or as part of a canister, the missile can be installed in the installation position of the missile system launcher and ensure the normal operation of the missile system regardless of the selected loading method.

[0007] The drawbacks of this prototype invention are that: whether in the form of canister loading or single loading, it is limited to using a single type of missile and must be equipped with a special launcher dedicated to this type of missile.

[0008] The currently developed 9M96E and 9M96E2 missiles have performance parameters similar to those of the 48Н6Е (E2, E3) series of missiles. However, after using modern components, the weight and volume of this type of missile are reduced to 1 / 4 to 1 / 5 of the original model. This missile was developed specifically for the 3K96E missile system, and during its R & D process, no consideration was given to adapting to the 35Р6E and 40Р6E missile systems and their supporting launchers such as the 5П85E and 51П6E.

[0009] The common feature of the prototype (9M334E launcher) and the object of the present invention, the 9M96E2-2 launcher, is that both use a mechanical device that can assemble four surface-to-air missiles in a single installation module.

[0010] The present invention aims to achieve the adaptation and installation of the 9M96E(2) surface-to-air missile of the 3K96E missile system on the 5П85E and 51П6E launchers of the 35Р6E and 40Р6E missile systems through the 82Ц6E technical maintenance equipment and ensure its normal launch function. Summary of the Invention

[0011] The essence of the technical solution of the present invention lies in:

[0012] - Using the 9M96E2-2 launcher to assemble four 9M96E(2) surface-to-air missiles in a box, and the outer diameter of this launcher does not exceed the outer diameter of the transportation and launch canister (TLC) of the 5B55E, 48H6E (E2, E3), and 40H6E missiles;

[0013] - The design of the 9M96E2-2 launcher provides a hoop similar in design, size, and position to the hoop of the TLC of the 5B55E, 48H6E (E2, E3), and 40H6E missiles;

[0014] - The design of the 9M96E2-2 launcher has a support device for fixing the TLC containing the missile to the ground during missile launch;

[0015] - The fixed hoop band, the missile TLC fixing structure, and the 9M96E2-2 launcher support device are positioned such that the center of gravity of the 9M96E2-2 launcher loaded with missiles coincides with the TLC center of gravity of the 5B55E, 48H6E (E2, E3), and 40H6E missiles;

[0016] - The 9M96E2-2 launcher is designed to provide an external connector with a similar design, dimensions, and position to the external connectors of the 5B55E, 48H6E (E2, E3), and 40H6E missile TLCs;

[0017] - The external connector of the TLC of the 9M96E(2) missile is connected to the external connector of the 9M96E2-2 launcher through a switching device, which includes: a multiplexing channel splitter for transmitting launcher information to the 4 missiles in the 9M96E2-2 launcher, and a patch panel for conditionally setting the missile numbers in the system (35P6E or 40P6E) for the missiles in the specified 9M96E2-2 launcher through jumpers.

[0018] The positive effects produced by the technical solution of the present invention are as follows: By using the 82Ц6E technical maintenance equipment, the 9M96E(2) surface-to-air missiles of the 3K96E missile system can be adapted and installed on the 5П85E and 51П6E launchers of the 35P6E and 40P6E missile systems, thereby increasing the ammunition base of the 35P6E and 40P6E missile systems by 4 times. Specific embodiments

[0019] The embodiments of the present invention include:

[0020] - Design the 9M96E2-2 launcher, assemble four 9M96E(2) surface-to-air missiles in one box, and its outer diameter does not exceed the outer diameter of the transport and launch containers (TLCs) of the 5B55E, 48H6E (E2, E3), and 40H6E missiles;

[0021] - The hoop band of the 9M96E2-2 launcher is designed with the same design, dimensions, and position as the hoop bands of the 5B55E, 48H6E (E2, E3), and 40H6E missile TLCs;

[0022] - The 9M96E2-2 launcher design includes a support device for supporting the TLC with missiles on the ground during missile launch;

[0023] - The design of the 9M96E2-2 launcher is such that the center of gravity of the 9M96E2-2 launcher after loading missiles coincides with the center of gravity of the TLCs of the 5B55E, 48H6E (E2, E3), and 40H6E missiles;

[0024] The external connector of the 9M96E2-2 launcher tube adopts a design, dimensions and position similar to those of the TLC external connectors of the 5B55E, 48H6E (E2, E3) and 40H6E missiles;

[0025] - The TLC external connector of the 9M96E(2) missile is combined with the external connector of the 9M96E2-2 launcher tube through a switching device, which includes: a multiplex channel splitter for transmitting information from the launcher to the 4 missiles in the 9M96E2-2 launcher tube, and a wiring panel for setting jumper switches to conditionally assign missile numbers to the missile distribution systems (35P6E or 40P6E) of the missiles in the specified 9M96E2-2 launcher tube.

[0026] The present invention is illustrated by Figure 1 and Figure 2 as follows:

[0027] 1 - 9M96E(2) missile transport and launch container (TLC);

[0028] 2 - Upper partition in the 9M96E2-2 launcher tube for fixing the TLC and upper fixing strap connected to the swinging part of the launch device;

[0029] 3 - Support device in the 9M96E2-2 launcher tube for supporting the TLC with missiles on the ground and lower fixing strap connected to the swinging part of the launch device;

[0030] 4 - TLC external connector of the 9M96E(2) missile and wire harness output to the switching device and external connector of the 9M96E2-2 launcher tube;

[0031] 5 - Switching device and external connector of the 9M96E2-2 launcher tube.

Claims

1. A ground-to-air missile launcher tube, comprising a tube body and an in-built missile, capable of assembling multiple ground-to-air missiles in a single mounting module, the mounting module including a plurality of transport and launch containers, characterized in that: The design of the launcher tube allows for the assembly of up to four ground-to-air missiles in a radial compartment with a diameter not exceeding the outer diameter of a single transport and launch container in the single mounting module, with one ground-to-air missile located within the missile transport and launch container; The launcher tube is provided with an upper fixing strap and a lower fixing strap, and the design, dimensions and position of the fixing straps of the launcher tube are such that it can be fixed to the fixing straps of the transport and launch container in the single mounting module; The design of the launcher tube provides a support device for leaning the launcher tube against the ground during the launch of the ground-to-air missile from the launcher tube; The launcher tube design also provides an external connector, the design, dimensions and position of which are such that it can be connected to the external connector of the transport and launch container through a switching device, the switching device comprising: a multiplex channel splitter for transmitting information to the four ground-to-air missiles in the launcher tube, and a patch panel for assigning jumper numbers to the ground-to-air missiles in the launcher tube; The positions of the fixing points of the upper and lower fixing straps of the launcher tube on the transport and launch container and the position distribution of the external connector of the launcher tube are such that the center of mass of the launcher tube with the support device and the ground-to-air missile coincides with the center of mass of one of the transport and launch containers with one ground-to-air missile in the single mounting module.

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