FIELD: rocketry, in particular, devices for separation of electrical communications of the rocket with the transport launching pack or launcher.
SUBSTANCE: a hatch with exposed supporting edges is made on the rocket body in the point of the outlet of the electrical connector receptacle. The rocket is provided with a rotary panel made in the shape of hatch plate cover reduction and a lever rigidly connected to it with one end, hinge-fastened with the other end on the outer surface of the rocket body in front of the hatch. The inner surface of the cover is made for engagement by its edges with the reduced supporting edges of the hatch, and the cover outer surface is made tapered with expansion towards the rocket aft.
EFFECT: enhanced reliability of the rocket due to provision of protection of the contacts of the separated electrical receptacle against the effect of kinetic heating.
2 cl, 5 dwg
| Title | Year | Author | Number |
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|
RU2302600C1 |
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|
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| ROCKET-TORPEDO LAUNCHER | 1998 |
|
RU2133431C1 |
| DOCKING UNIT OF THE DEVICE WITH AN UNMANNED AERIAL VEHICLE | 2022 |
|
RU2775187C1 |
