Thermal test results of the two-phase thermal bus technology demonstration loop
Entwicklung verschiedener Waermerohre zur Anwendung in Satelliten
A differential approach to heat pipe priming in microgravity
Development of the lockheed pumped two-phase thermal bus
Copper/water axially-grooved heat pipes for RTG applications
A low pressure drop heat exchanger with integral heat pipe
Totally enclosed heat pipe cooled induction motor (theoretical and experimental results)