RU2288423C1 - Guided rocket missile enclosed in transportation and launching container - Google Patents

Abstract

FIELD: military engineering.

SUBSTANCE: device has missile warhead having a leading cumulative charge and onboard equipment provided with electric launching and control circuits are connected to ground control means. The electric launching circuits and controlled electric circuits are connected to the container via umbilical connector. Ring-shaped socket of the umbilical connector is arranged around the leading cumulative charge. It is connected to the electric rocket missile launching and control circuits and is snapped together with the umbilical connector plug-and-socket that is mounted on the internal side of frontal container cover and electrically connected to the launching and control plug-and-sockets sealed from container outside. The control plug is mounted on the external side of frontal container cover and sealed with plug.

EFFECT: improved rocket missile reliability.

1 dwg

Description

The present invention relates to aircraft, in particular to wire-guided missiles and shells, and can also be used in the development of automation of aircraft.

Known guided missile in a transport and launch container (RF patent No. 2233420, F 42 В 15/00) containing an additional (leading) warhead and airborne equipment, in which the electric launch and control circuits are connected through the container to ground control equipment.

In this guided missile, the connection of the launch electric circuits with the container is carried out using wires that are cut off when the rocket starts.

The disadvantage of this technical solution is the deterioration of the operational characteristics of the guided missile due to a decrease in reliability due to the possibility of shorting the wires when they are broken, and therefore, shorting the electrical circuits of the rocket and the failure of the rocket.

The objective of the invention is to increase the operational characteristics of the rocket by increasing the reliability of the rocket by eliminating the closure of electrical circuits when starting the rocket.

To achieve the task in a guided missile in a transport and launch container containing a warhead with a leading cumulative charge installed in the nose of the rocket, and an onboard control equipment in which the electric launch and control circuits are connected through the container to the ground control equipment, in it launch circuits and controlled electrical control circuits are connected to the container through a bursting connector, while in the nose of the rocket around the leading cumulative charge there is an annular socket of a bursting connector, which is connected to the launch electrical circuits and controlled electric missile control circuits and docked to the bursting plug plug, which is installed on the inside of the container front cover and electrically connected to the start and control connectors, tightly fixed outside the container, and the control connector mounted on the outside of the front cover of the container and hermetically sealed with a plug.

The proposed technical solution improves the reliability of the rocket:

- the introduction of a burst connector into the rocket eliminates the closure of electrical circuits when the rocket starts;

- introducing a control connector into the rocket and installing it outside the container allows you to control the electrical circuits of the rocket without violating the tightness of the rocket in the container;

- the introduction into the rocket of a ring outlet located around the leading cumulative charge allows it to provide free space in front of it and the free formation of its cumulative jet.

The drawing shows a guided missile in a transport and launch container, which shows the connection of the electrical launch circuits and electric control circuits of the rocket with the launch and control connectors of the container.

1 - Harness.

2 - Contacts of the ring socket of the bursting connector.

3 - Ring socket of the bursting connector.

4 - Rocket.

5 - Contacts of the ring socket of the bursting connector.

6, 7 - Plug contacts of the bursting connector.

8 - Plug burst connector.

9 - The front cover of the container

10 - Container.

11 - Contacts of the control connector.

12 - Control connector.

13 - Plug

14 - Start connector.

15 - Harness.

16 - The axis of the front cover.

17, 18 - Rubber rings.

19 - The leading cumulative charge of the warhead.

20 - Wire coil wireline.

21 - Connector.

22 - Harness.

The connection of electrical circuits is as follows. The launch electric circuits and the controlled rocket control circuits are made in the form of a harness 1. The launch electric circuits are connected to the contacts 2 of the ring socket of the explosive connector 3 of the rocket 4. The controlled electric control circuits are connected to the contacts 5 of the ring socket of the explosive connector. Contacts 2 and 5 of the annular socket of the bursting connector are docked with contacts 6 and 7, respectively, of the plug of the bursting connector 8 mounted on the inside of the front cover 9 of the container 10. Contacts 7 of the plug of the bursting connector 8 are connected to the contacts 11 of the control connector 12, closed by a plug 13. Contacts 6 the plugs of the bursting connector 8 are connected to the contacts of the starting connector 14 by means of a bundle 15 sealed through the front cover of the container.

The rocket control electric circuits contain a wireline coil located in the tail compartment of the rocket and connecting the onboard rocket control equipment with the ground control equipment using wires of the wireline coil 20 through the connector 21 located on the front cover 9 of the container 10, the bundle 22 is hermetically withdrawn through the front cover 9 of the container 10, and the start connector 14

Rubber rings 17, 18 are designed to seal the container.

Before the launch of the rocket, the front cover 9 of the container 10 automatically opens, rotates around the axis 16 and is fixed in the open position. In this case, the plug of the bursting connector 8 and the annular socket of the bursting connector 3 are disconnected, the electric launch circuits and the controlled electric control circuits of the rocket are disconnected from the container.

During the flight of the rocket, the wires of the wireline coil 20 are unwound and provide electrical communication between the rocket and the ground control equipment.

Claims (1)

Guided missile in a transport and launch container, containing a warhead with a leading cumulative charge installed in the nose of the rocket, and on-board equipment, in which the electric launch circuits and controlled electric control circuits are connected through the container to ground control equipment, characterized in that launch electric circuits and controlled electric control circuits are connected to the container through a bursting connector, while in the nose of the rocket around the leading cumulative charge an annular socket of a bursting connector is installed, which is connected to launch electric circuits and controlled electric missile control circuits and docked with a plug of a bursting connector, which is installed on the inside of the front cover of the container and is electrically connected to the starting and control connectors sealed to the outside of the container, and the control connector mounted on the outside of the front cover of the container and hermetically sealed with a plug.