NASA Goddard Space Flight Center Cooperative Enterprise

By: Nasa, National Aeronautics and Space Adm

The viability of a Capillary Heat Pump (CHP) concept using a Loop Heat Pipe evaporator and an eductor in a closed loop to reject heat at a higher temperature than it is acquired at with the goal of reducing spacecraft radiator area is examined. Eductor inefficiency resulting from the mixing of high velocity motive flow with low velocity suction flow may preclude spacecraft radiator area savings. The utility of a CHP for thermal management may be limited...

• Format: Paperback
• Language: English
• ISBN: 1723863025
• ISBN13: 9781723863028
• Release Date: January 1
• Publisher: Independently Published
• Length: 56 Pages
• Weight: 0.34 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"