Liquid metal micro heat pipes for space radiator applications
- Author(s):
- Gerner, F. M. ( Cincinnati Univ. )
- Henderson, H. T. ( Cincinnati Univ. )
- Publication title:
- NASA Technical Reports
- Pub. Year:
- 1995
- Issue:
- NASA-CR-199122
- Pt.:
- NAS 1.26:199122
- Paper no.:
- N96-11650
- Page(from):
- 1
- Page(to):
- 15
- Pages:
- 15
- Pub. info.:
- National Aeronautics and Space Adminstration
- Language:
- English
- Type:
- Technical Paper
Similar Items:
American Society of Mechanical Engineers |
7
Technical Paper
Space-proven indium liquid metal field ion emitters for ion microthruster applications
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
THE LIQUID DROPLET RADIATOR-AN ULTRALIGHTWEIGHT HEAT REJECTION SYSTEM OR EFFICIENT ENERGY CONVERSION IN SPACE
National Aeronautics and Space Administration |
3
Technical Paper
Investigation of the Temperature Distribution in Radiator Fins with Micro Heat Pipes
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
Commercial Micro Heat-Pipes Installation Into High Dissipation Space Equipments: On Ground Testing Preliminary Results
Society of Automotive Engineers |
American Institute of Aeronautics and Astronautics |
Society of Automotive Engineers |
6
Technical Paper
New applications of liquid-crystal thermography in rotating turbomachinery heat transfer research
The American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |