Temperature control of the orbital otolith experiment
Thermal design of «AIST» small spacecraft
MULTIMEDIA FLEXIBLE COMPUTERIZED LINE SYSTEM OF VEHICLE TECHNICAL CONDITION MONITORING.
Predictor–Corrector Method for Scramjet Inlet Air Mass Flow Rate Measurement
Stabilization and Attitude Determination Methods for FalconSAT-3
Cryogenic Heat Pipe for Cooling High-Temperature Superconducting Coils
Temperature Synchronization of Natural Convection in Adjacent Thermostatically Controlled Cavities
Autoignitable and Restartable Hybrid Rockets Using Catalytic Decomposition of an Oxidizer
Thermal Design and Analysis of a Hard X-Ray Modulation Telescope
Novel Thermally Stable Segmented Solid Paraboloid Antenna for High Surface Accuracy
Electric Aircraft Cryogenic Cooling with Thermo-Acoustic Exergy Management
Energy Storage System Modeling and Control
Transient Method for Estimating the Effective Emittance of Multilayer Insulation Blankets
NASA Acoustic Stirling IRAD Energy Conversion in Aircraft