发明名称 Inflatable spherical integrating source for spaceflight applications
摘要 A method for calibrating a sensor in a vehicle, such as a space capsule or other space borne apparatus, uses an expandable integrating sphere. A sensor in the vehicle measures the energy from an electromagnetic energy source within the integrating sphere through a calibration window. The expandable fluid impermeable integrating sphere expands when filled with a fluid, such that when filled with the fluid, its interior is viewable through the calibration window. The system includes a source of fluid to fill the integrating sphere and a fluid regulator coupled to the vehicle to determine when to supply the fluid to the integrating sphere to maintain an appropriate gas pressure level with the integrating sphere.
申请公布号 US2008013082(A1) 申请公布日期 2008.01.17
申请号 US20070825282 申请日期 2007.07.05
申请人 RAYTHEON COMPANY 发明人 CUTLIP HANSFORD H.
分类号 G01J1/04;G01J1/00 主分类号 G01J1/04
代理机构 代理人
主权项
地址