FIELD: rocketry.
SUBSTANCE: invention relates to rocket engineering, namely to devices for undocking missile with container. Device for disconnection of connector between missile and transport-launching container comprises quick-disconnect electrical connection of plug with wire and socket. In the missile body there is a recess in which a metal plate is placed perpendicular to the missile axis. One side of the plate is elongated and forms a triangle with a rounded corner. Rectangular part is completely in the recess, and the triangle protrudes outside the missile body. Dielectric plate of the same shape is superimposed on the plate. Length of the second plate is greater than that of the metal plate. Triangular part of the dielectric plate protrudes beyond the metal plate. Recess is made in dielectric plate in rectangular part. On top of this plate there is a dielectric plate in which a projection is made along its entire width. This ledge is located in the recess of the previous plate. Electric connection plug wire is placed between plates. All three plates are attached by screws to the missile body. Internal angles of the recess and external corners of the projection of the dielectric plates can be made rounded.
EFFECT: higher reliability.
2 cl, 5 dwg
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Authors
Dates
2024-06-25—Published
2023-10-12—Filed