FIELD: armament.
SUBSTANCE: the two-stage missile in a launching pack has an intermediate fairing, an electric connector located on the missile and coupled to the pack, and a spring device for disconnection of the electric connector blocks. The electric connector is located under the intermediate fairing behind one of the wings in the plane of its symmetry. A through radius slot for the withdrawable part of the blocks with the rear wall of the slot is made of the intermediate fairing above the point of out-let of the electric connector. The missile is provided with a rotary panel consisting of a laminated cover and one end of the lever rigidly coupled to it, whose other end is hinge-fastened on the rear edge of the wing. The cover inner surface is made as the mating outer surface of the intermediate fairing in the point of outlet of the radial slot from it and the equitant outer surface of the missile body in the point of outlet of the electric connector from it.
EFFECT: enhanced reliability of the missile.
5 dwg
Title | Year | Author | Number |
---|---|---|---|
TWO-STAGE BICALIBER ROCKET | 2003 |
|
RU2246093C1 |
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 CONNECTION AND DISCONNECTION OF ELECTRIC COUPLINGS OF SEPARATED AIRCRAFT STAGES | 2016 |
|
RU2630858C1 |
TRANSPORTER-LAUNCHER CONTAINER | 2007 |
|
RU2350885C1 |
ROCKET IN LAUNCHING PACK | 2003 |
|
RU2242697C1 |
LAUNCHER | 2006 |
|
RU2309362C1 |
MULTIFUNCTIONAL SMALL-SCALE TRANSFORMABLE REUSABLE UNMANNED AERIAL VEHICLE IN TRANSPORT-LAUNCH CONTAINER AND STARTING METHODS | 2022 |
|
RU2778177C1 |
Authors
Dates
2007-07-10—Published
2005-12-27—Filed