NASA thermal control technologies for robotic spacecraft

被引:294
|
作者
Swanson, TD
Birur, GC
机构
[1] NASA, Goddard Space Flight Ctr, Greenbelt, MD 20771 USA
[2] CALTECH, Jet Prop Lab, Pasadena, CA 91109 USA
关键词
advanced thermal control; capillary pumped loops; loop heat pipes; variable emissivity surface; cryogenic; heat switches; thermal storage;
D O I
10.1016/S1359-4311(03)00036-X
中图分类号
O414.1 [热力学];
学科分类号
摘要
Technology development is inevitably a dynamic process-in search of an elusive goal. It is never truly clear whether the need for a particular technology drives its development, or the existence of a new capability initiates new applications. Technology development for the thermal control of spacecraft presents an excellent example of this situation. Nevertheless, it is imperative to have a basic plan to help guide and focus such an effort. Although this plan will be a living document that changes with time to reflect technological developments, perceived needs, perceived opportunities, and the ever-changing funding environment, it is still a very useful tool, This presentation. summarizes the current efforts at National Aeronautics, and Space Administration (NASA)/Goddard and NASA/JPL to develop new thermal control technology for future robotic-NASA missions.
引用
收藏
页码:1055 / 1065
页数:11
相关论文
共 50 条