Sensors for a system to control the liquid flow into an evaporative cold plate of a two-phase heat transport system for large spacecraft

Fluid physics instrumentation study: final report: part I: system aspects

Some considerations concerning two-phase flow thermal bus systems for spacecraft

Definition of a Variable Conductance Heat Pipe (VCHP) for the experimental verification of the VCHP mathematical model developed at NLR

A review of space-related thermophysical research at NLR

Limitations in variable conductance heat pipe performance and control predicted by the current steady-state model developed at NLR

Uniaxial model for gas-loaded variable conductance heat pipe performance : the effects of vapour flow friction and inertia

Enige beschouwingen over de eigenschappen van een MHD rookgas

Warmteoverdracht door straling in een MHD generatorkanaal

Fully controllable heat pipe containing a short electro-osmotic pumping section

Multilayer insulation blankets for spacecraft applications: thermal model accounting for outgassing and different ways of gas migration

Uniaxial model for gas-loaded variable conductance heat pipe performance in the inertial flow regime

Uniaxial model for a gas loaded variable conductance heat pipe

Quantitative considerations concerning a high performance heat pipe with a short electro-osmotic pumping section

Significance of a rotor blade failure for fleet operation, maintenance, design and certification

Some quantitative considerations on electro-osmotic flow pumping in heat pipes

Heat balance research with a thin-walled cube in a simulated space environment

The influence of outgas on the performance of multilayer insulation blankets with perforated shields

Possible benefits of electro-osmotic flow pumping in heat pipes for space applications

Heat transfer experiments with liquid helium in Spacelab