25-04-2023 дата публикации
Номер: CN116006353A
Принадлежит:
The invention relates to a split type sliding block of a solid rocket engine, which comprises a sliding block base arranged along the radial direction of a combustion chamber shell, a sliding block base body is sleeved on the outer side of the sliding block base, an assembly hole matched with the sliding block base in appearance is formed in the center of the sliding block base body, and a tile-shaped groove tightly matched with the combustion chamber shell is formed in the bottom of the sliding block base body. A missile launcher sliding rail is arranged at the top of the sliding block base body, a plurality of base connecting holes are formed in the periphery of the sliding block base, a plurality of base body connecting holes are formed in the periphery of the sliding block base body, and the base body connecting holes are connected with the base connecting holes through fasteners. A split structure is adopted, the sliding block base body can freely select a high-strength alloy material ...
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