FIELD: rocketry, applicable in the construction of two-stage bicaliber rockets provided with a device for separation of the electric lines of the rocket stages.
SUBSTANCE: the assembly of electric connection is fastened at an angle to the rocket longitudinal axis and provided with a rejecting device in the form of a hatch plate door made in the transient fairing, connected to the rejected connector block of the first stage.
EFFECT: enhanced reliability of the rocket.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TWO-STAGE MISSILE IN LAUNCHING PACK | 2005 |
|
RU2302600C1 |
| CONTROLLED BULLET IN LAUNCHING CONTAINER | 2014 |
|
RU2568823C1 |
| ROCKET IN LAUNCHING PACK | 2003 |
|
RU2247919C1 |
| ROCKET | 2003 |
|
RU2247920C1 |
| ROCKET IN A TRANSPORT AND LAUNCH CONTAINER | 2023 |
|
RU2802857C1 |
| DEVICE FOR TRANSMITTING ELECTRICAL SIGNALS FROM THE ELECTRICAL SYSTEM OF THE LAUNCHER TO THE ELECTRICAL SYSTEM OF THE SEPARATED OBJECT | 2022 |
|
RU2779975C1 |
| DEVICE FOR CONNECTION AND DISCONNECTION OF ELECTRIC COUPLINGS OF SEPARATED AIRCRAFT STAGES | 2016 |
|
RU2630858C1 |
| METHOD FOR DOCKING THE DEVICE WITH AN UNMANNED AERIAL VEHICLE | 2022 |
|
RU2784478C1 |
| ELECTRICAL CONNECTOR HATCH | 2021 |
|
RU2767220C1 |
| ROCKET-TORPEDO LAUNCHER | 1998 |
|
RU2133431C1 |
