GrabCAD 模型信息
Rocket Combustion Chamber(Regeneratively Cooled) · 模型 165677
Regeneratively Cooled Combustion Chamber. Designed to a small scale for 3D printing or prototyping. Main Body/Liner Consists of integrated coolant channels. Regenerative cooling is used for cooling the chamber walls, throat and the first section of the nozzle, and for the inside of the engine, some film cooling is done. Film cooling with the gas generator exhaust at the nozzle extension is utilized when the regenerative cooling channels end. Aft manifold is modelled separately with an example of a weld. Second weld not modelled.(lower aft manifold weld) More information: https://www.researchgate.net/publication/326263055_Additive_Manufacturing_of_Liquid_Rocket_Engine_Combustion_Devices_A_Summary_of_Process_Developments_and_Hot-Fire_Testing_Results
- 格式
- Rendering、STL
- 分类
- 3D printing、Aerospace、Components
- 标签
- cooled、regeneratively、chamber、combustion、engine、rocket
- 数据更新
- 2026-10-21T11:36:56Z
