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Werkstoff
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Effects of Thermal and Chemical Nonequilibrium on Response of Charring Ablative Materials
A concise review of resource requirements for future space exploration
Space Environmental Exposure of the MISSE 9-15 Polymers and Composites Experiment 1-4 (PCE 1-4)
Space Environmental Exposure of the MISSE 9-15 Polymers and Composites Experiment 1-4 (PCE 1-4)
Thermoeconomic Analysis of a Compact Active Coolant System for Lithium-Ion Battery Pack
Estimation of Thermal Properties of Solid–Liquid Phase Change Material Using Fuzzy Inference Methods
The Aerodynamic Force for the Steady Incompressible Ideal Flow
Principles of laser materials processing : developments and applications
Overview of Lunar Regolith Simulants: Figures of Merit
Melting Processes of Phase Change Material in Sidewall-Heated Cavity
Aerodynamics of Tandem Wing Aircraft : From Dinosaurs to UAVs and Supersonic Planes
Pulsating Heat Pipe Experiments for Microgravity Sounding Rocket Tests
Effect of Geometric Parameters on Aerodynamic Characteristics
Recommendations Regarding Aerodynamic Design of Tandem Wing Aircraft
Determination of Tandem Wing Aircraft Aerodynamic Characteristics
Probabilistic modeling of stress gradients, microstructural and size effects in low-cycle fatigue
Test for chip resistance of surface coatings
Planetary Protection at Marshall Space Flight Center
Approach to Online AC Impedance Measurement of the Fuel Cell
Water Content Estimation of the PEM Fuel Cell
Water Management Strategy for the PEM Fuel Cell
Modeling of Water Content in MEA for the PEM Fuel Cell
Spallation of Carbon Ablators in Arcjet Facility Experiments
Stochastic Strength of an Automotive Windscreen
Extraction of Thermal Properties of Organic Ablative Materials Using Molecular Dynamics Simulations
Nanostructured materials for sustainable energy : design, evaluation, and applications
Numerical and Experimental Studies of Transpiration Cooling Film Effectiveness over Porous Materials
Multifunctional Hybrid Fiber Composites for Energy Transfer in Future Electric Vehicles
Evaluating Variable-Emissivity Surfaces for Radiative Thermal Control
Ablative Thermal Response Numerical Modeling Under Arcjet Test Conditions