FIELD: space technology.
SUBSTANCE: invention relates to the field of rocket technology, and more specifically to launchers. The rocket launcher contains a base with adjustable supports with a fixed gear block. A pivoting support device with the possibility of rotation in a horizontal plane is installed on the base, with a spring-lever mechanism fixed in the selected position. Platforms swinging on a fixed axis with blocks of guides for placing rockets are installed on the bed of the support-rotary device. The spring-lever mechanism is equipped with a set of wedges sliding in a vertical plane in a sealed housing and pressed by a set of springs to a profile gear block, as well as a lever swinging in a vertical plane, the short arm of which goes into the grooves of the wedges. The rocket launcher contains a digital rocket launch control system. The system includes a compact remote control unit, a launch unit, an azimuth sensor, elevation angle sensors, microswitches, and an indication unit. The pivoting device is equipped with a spring-lever mechanism. The elevation angle of each swinging platform is adjusted separately.
EFFECT: increased reliability is achieved.
5 cl, 6 dwg
Title | Year | Author | Number |
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SU1748736A1 |
Authors
Dates
2022-02-07—Published
2021-05-04—Filed