星箭分离面结构板
By combining the honeycomb core structure panel with I-shaped reinforcing ribs, the problems of lightweighting and high strength of the satellite-rocket separation surface structure panel were solved, improving the safety and payload capacity of the launch mission and reducing launch costs.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- 北京钧天航宇技术有限公司
- Filing Date
- 2025-10-13
- Publication Date
- 2026-07-17
AI Technical Summary
The existing satellite-rocket separation surface structure plate is difficult to achieve lightweight while meeting the requirements of high strength and rigidity, which affects the safety and payload capacity of the launch mission.
The honeycomb core structure panel, combined with I-shaped reinforcing ribs and star-and-arrow docking surface embedded parts, forms a radial structure through mechanical connection and adhesive bonding, which increases the overall strength and reduces the weight. Weight reduction grooves and aluminum skin protection are set in key parts.
This achievement enabled high strength and lightweight design of the spacecraft separation surface structure plate, improving the safety and payload capacity of the launch mission while reducing launch costs.
Smart Images
Figure CN120986706B_ABST