Homogeneous Equilibrium Modeling for Subcritical Flows in Liquid Rocket Engine Cooling Systems
Progress of CFM Model Development and Validation at NASA Glenn Research Center
Testing of TVS Augmented Injectors for Tank-to-Tank Transfer of Cryogens
Thermal Analysis of Cooling Channels on Electromechanical Actuator During Actual Flight
Space Technology Mission Directorate Game Changing Development Program
Unsteady Heat Transfer for Pressure Vessels in Atmospheric Flight at Orbital Velocities
Structural Heat Intercept, Insulation and Vibration Evaluation Rig (SHIIVER)
NASA's Cryogenic Fluid Management Technology Development Roadmaps
Stress to Failure Testing of Pressure Vessels with SHM Sensors at Liquid Nitrogen (LN2) Temperature
Comparison of Oxygen Liquefaction Methods for Use on the Martian Surface
In-Space Chemical Propulsion Systems Roadmap
NASA's Space Launch System Gains Momentum Toward Integration and Testing
Tank System Integrated Model: A Cryogenic Tank Performance Prediction Program
Cold Helium Gas Pressurization For Spacecraft Cryogenic Propulsion Systems
Coil-On-Plug Ignition for LOX/Methane Liquid Rocket Engines in Thermal Vacuum Environments
Integrated Insulation System for Automotive Cryogenic Storage Tanks
Liquefaction and Storage of In-Situ Oxygen on the Surface of Mars
Liquefaction and Storage of In-Situ Oxygen on the Surface of Mars
Cryogenic Propulsion for the Titan Orbiter Polar Surveyor