Variable Emittance Electrochromic Devices for Satellite Thermal Control
Spacecraft Thermal Management Using Advanced Hybrid Two-Phase Loop Technology
Performance Results of the ESR from the Space Technology 5 Satellites
Second-Order Model for Transient Heat Conduction in a Sphere
Titanium Heat Pipe Thermal Plane
Test Results for a High Power Thermal Management System
Heat Transfer Through Longitudinal Fins
A Low Specific Mass Inflatable Radiator for a 100kW Solar Powered GEO Satellite
Pressure Controlled Heat Pipe for Precise Temperature Control
Spray Cooling Modeling: Droplet Sub-Cooling Effect on Heat Transfer
Demonstration of a Plug-and-Play Approach to Spacecraft Thermal Control System Design
Loop Heat Pipe Development Overview
Life Test Results for Water Heat Pipes Operating at 200^oC to 300^oC
Experimental Studies on CHF of Pool Boiling on Horizontal Conductive Micro Porous Coated Surfaces
Investigation of Pore Size Effect On Spray Cooling Heat Transfer with Porous Tunnels
Titanium Loop Heat Pipes for Space Nuclear Power Systems
Vapor Compression Hybrid Two-Phase Loop Technology for Lunar Surface Applications
Effect of Non-Uniform Inlet Temperature on Flow Stagnation in a Pumped Fluid Tube Radiator