FIELD: rocketry.
SUBSTANCE: invention relates to systems for launching rocket equipment from a transport-launching container (TLC). TLC contains a rocket, which comprises rocket engine with nozzle and retainer secured on bracket (5). This mechanism comprises double-arm lever (7) interacting with slider (6) of the rocket (movement of the slider during rocket departure is indicated by arrow (16)), stop (8), connecting rod (10) and flag (9) in the initial position (dotted line) located in the nozzle cut area. Lever axes (11), stop (12) and flag (14) are fixed on bracket (5). Stop and the flag are connected by a connecting rod by means of common axes: (13) stop and connecting rod and (15) connecting rod and flag. Axes (13) and (14) are installed in one plane, and axis (15) is installed higher. When launching the rocket, the powder gases act on the working surface of flag (9), turning it around axis (14), and by means of connecting rod (10) stop (8) is turned, which unlocks lever (7). Slider (6) together with rocket freely moves forward.
EFFECT: simplified design, decreased overall dimensions and reusability of the TLC, allowing for reliable fixation and release of the rocket when launched from the TLC.
3 cl, 4 dwg
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Authors
Dates
2024-07-17—Published
2023-06-19—Filed