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CFD Modeling of Cryogenic Chilldown in a Complex Channel under Normal and Low Gravity Conditions
CFD Modeling of Cryogenic Chilldown in a Complex Channel under Normal and Low Gravity Conditions
InSight: Single Station Broadband Seismology for Probing Mars' Interior
Shock Stand off Distance with Mass Injection
Cryogenic Propellant Tank Self-Pressurization and Active Pressure Control
Convective Heat Transfer in Rocket Engines - Part 2, Heat Transfer to the Nozzle
Analysis of Advanced Thermoelectric Materials and Their Functional Limits
Compact, Deep-Penetrating Geothermal Heat Flow Instrumentation for Lunar Landers
Flow Field Prediction and Analysis, Project Fire Final Report
An Introduction to Heat Transfer in Hydrogen/Oxygen Rocket Combustion Chambers
Methods for Decontamination of a Bipropellant Propulsion System
Flow Field Computations for Blunt Bodies in Planetary Environments (Equilibrium) Final Report
Flow Field Computations for Blunt Bodies in Planetary Environments (Equilibrium) Final Report
Solutions of Two Heat-Transfer Problems with Application to Hypersonic Cruise Aircraft
Spray Cooling And The Next Generation Of NASA Space Flight
Multidisciplinary Thermal Analysis of Hot Aerospace Structures
Analysis of Microgravity Experiments Conducted on the Apollo Spacecraft
Operational Description of the Hot Bleed Port Program, Job Ab 1108
Aerothermal Anchoring of CBAERO Using High Fidelity CFD
Heat Transfer at Reduced Gravity
Advanced Mirror Technology Development (AMTD) Thermal Trade Studies
Development of a Bearingless Ammonia Pump for Spacecraft Thermal Control
Convective Heat Transfer in Rocket Engines. Part 5 - Non-Uniform Boundary Layer Effects
Space Cold Chain: From Ground to the International Space Station and Back
Aerodynamics of Heat Exchangers for High-Altitude Aircraft
Thermal Fluid Analysis for Nuclear Thermal Propulsion Radiation Shield
Thermal Interface Comparisons Under Flight Like Conditions
Time Response Test of Thrust Chamber Thermocouples in Simulated Rocket Firing
Environmental Research Satellites for Space Propulsion Systems Experiments
Next Generation Aircraft Electrical Power Systems and Hybrid/All Electric Aircraft
Forced Air Convection Thermal Switch Concept for Responsive Space Missions
Thermal Runaway Severity Reduction Assessment For EVA Li-Ion Batteries