High Temperature, Optical Sapphire Pressure Sensors for Hypersonic Vehicles-UF
| 项目名称： | High Temperature, Optical Sapphire Pressure Sensors for Hypersonic Vehicles-UF |
| 摘要： | Orbital commercial space vehicles require high-temperature sensors (~1000°C/1600°F) or various phases of flight (e.g, hypersonic flight, high speed reentry) or to monitor system and subsystem performance (e.g., for gas turbines or scramjets). Current commercial sensors are only capable of up to ~300°C/600°F. |
| 状态： | Active |
| 资金： | 272000 |
| 资助组织： | Federal Aviation Administration Center of Excellence for Commercial Space Transportation |
| 项目负责人： | Davidian, Ken |
| 执行机构： | University of Florida |
| 开始时间： | 20110103 |
| 预计完成日期： | 20150830 |
| 主题领域： | Aviation；Vehicles and Equipment |
相关文献
- High Temperature, Optical Sapphire Pressure Sensors for Hypersonic Vehicles
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