FIELD: rocket technology.
SUBSTANCE: invention can be used in various types and classes of rockets equipped with a device for docking, undocking the electrical connectors of the rocket and the transport and launch container. The missile in the transport-launch container contains electrical connectors, placed motionless on the rocket and with the possibility of movement in the transport-launch container. The missile in the transport and launch container also includes a device for docking and undocking electrical connectors. A device for docking and undocking connectors as a part of a beam with guide grooves for moving the rocket is located in the longitudinal plane of symmetry of the rocket in the transport and launch container, on which curly guides are fixed with carriage rollers installed in them, made in the form of upper and lower plates connected by elastic elements, with electrical connectors located in the carriage. On the upper plate of the carriage there is a lever, the roller of which enters the vertical guide mounted on the base with the possibility of horizontal movement at the impact of the damper stop at a speed equal to the speed of movement of the loaded rocket. The base with the window is installed on the beam. Under the base in the grooves there is a shutter with a stop fixed on it, a fastening element of the damper return spring and a recess for accommodating electrical connectors located in the transport and launch container. Hooks are attached on the bottom of the shutter with the possibility of interacting with the rocket sliders.
EFFECT: increasing the reliability of docking and undocking of the electrical connectors of the rocket and the transport and launch container, ensuring automatic docking, as well as ensuring the safety of the contacts of the electrical connectors of the transport and launch container from burning out during rocket launch and ensuring the reusable use of the transport and launch container.
1 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
ROCKET IN LAUNCHING PACK | 2003 |
|
RU2247919C1 |
LAUNCHER | 2006 |
|
RU2309362C1 |
TWO-STAGE MISSILE IN LAUNCHING PACK | 2005 |
|
RU2302600C1 |
LAUNCHING SYSTEM | 2009 |
|
RU2406961C1 |
ELECTRICAL CONNECTOR RETRACTION MECHANISM | 2024 |
|
RU2825586C1 |
DEVICE FOR CONNECTION AND DISCONNECTION OF ELECTRIC COUPLINGS OF SEPARATED AIRCRAFT STAGES | 2016 |
|
RU2630858C1 |
AVIATION LAUNCHER | 2004 |
|
RU2259306C1 |
MULTIPIECE NAVAL LAUNCHER | 2008 |
|
RU2371654C1 |
ROCKET | 2003 |
|
RU2247920C1 |
TWO-STAGE BICALIBER ROCKET | 2003 |
|
RU2246093C1 |
Authors
Dates
2023-09-05—Published
2023-02-08—Filed