GrabCAD 模型信息
Design and Analysis of Morphing Rocket Nozzle for Thrust Vector Control · 模型 266217
This project focuses on the design and analysis of a morphing rocket nozzle intended for thrust vector control (TVC) in aerospace propulsion systems. The aim is to enhance maneuverability and efficiency by developing a bio-inspired, flexible nozzle structure capable of controlled deformation under high thermal and mechanical loads. The proposed design incorporates a honeycomb morphing structure actuated using smart materials and external mechanisms. Simulations using CFD and FEA tools are conducted to analyze the aerodynamic and structural performance of the nozzle under RS-25 engine boundary conditions. This work offers a novel approach to modern TVC systems by combining material science, morphing mechanics, and aerospace engineering.
- 格式
- STEP / IGES、Rendering
- 分类
- Aerospace
- 标签
- rocket nozz、cfd analysis、fea analysis、rs-25 rocket engine、morphing nozzle、thrust vector control、rocket propulsion
- 数据更新
- 2026-10-30T10:29:56Z