GrabCAD 模型信息
The Dual Detonation-Driven Hypervelocity Tunnel · 模型 115230
Dual Detonation-Driven Hypervelocity Tunnel This advanced tunnel system is designed to simulate and test the behavior of spacecraft and vehicles during high-speed entry into various planetary atmospheres. It integrates cutting-edge features for flexible and efficient testing, including: Gas Section: Prepares various gas mixtures to replicate the atmospheric conditions of different planets, ensuring adaptability to a range of testing scenarios. Dual Detonation Chambers: Creates powerful shock waves, providing the high-energy environment required for hypervelocity testing. Driver Section: Guides the high-pressure gas produced by the detonation chambers toward the expansion zone, enabling smooth control over gas flow dynamics. Nozzle Section: Accelerates the gases to reach extremely high speeds, simulating the conditions spacecraft face during atmospheric re-entry. Test Section: Designed to accommodate models up to 24 inches, allowing the testing of spacecraft and vehicle prototypes in extreme environments. The section also features easy test model change capability, enabling rapid swaps of test subjects for efficient experimentation. Shock Damping Section: Reduces pressure shocks generated during testing, protecting the system from damage and ensuring stable operations. Interchangeable Diaphragm: This feature enhances the flexibility of the tunnel by allowing quick replacement of diaphragms, which regulate the flow of gases. This enables fast configuration changes for different test conditions without lengthy downtimes.
- 格式
- Rendering、STEP / IGES、Other
- 分类
- Aerospace、Industrial design、Machine design
- 标签
- nasa_hypervelocity_expansion_tunnel
- 数据更新
- 2026-10-16T19:48:48Z
