A direct push head cap separation method and structure
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- XIAN MODERN CONTROL TECH RES INST
- Filing Date
- 2023-12-27
- Publication Date
- 2026-06-19
AI Technical Summary
Existing helmet separation schemes suffer from problems such as complex structure, high cost, heavy weight, large impact load, and complex timing control, making it difficult to meet the requirements of rapid and safe separation for hypersonic missiles.
A direct-push hood separation method is adopted. Through aerodynamic shape and structural optimization design, the hood is kept in a neutral and stable state during separation. The axial separation speed is provided by separation actuators of the same specifications. The minimum separation speed and the number of actuators are determined by combining unsteady separation simulation analysis to achieve safe separation of the hood.
The weight of the hood and the impact of separation were reduced, the structure of the separation system was simplified, the research and development and production costs were reduced, and the reliability and safety of the separation system were improved.
Smart Images

Figure CN117685832B_ABST