GrabCAD 模型信息
Bio-Inspired Morphing Rocket Nozzle · 模型 266262
The Morphing Rocket Nozzle for Thrust Vector Control project focuses on improving propulsion systems by using advanced morphing techniques for precise thrust vectoring. It begins with designing a liquid rocket nozzle and conducting CFD simulations to evaluate its aerodynamic and thermal performance. A bio-inspired honeycomb structure, actuated by Shape Memory Alloy (SMA) springs, provides adaptive morphing capabilities for improved flexibility and control. Comprehensive FEA in ANSYS ensures the structural and thermal integrity of the nozzle under operational conditions. This project lays the foundation for future advancements in adaptive aerospace propulsion, enhancing maneuverability and mission efficiency
- 格式
- Rendering、STEP / IGES
- 分类
- Aerospace、Machine design、Tech
- 标签
- bio-inspired、thrust vector control、morphing rocket nozzle
- 数据更新
- 2026-10-19T10:32:02Z