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Kühlsystem
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Advanced and Additive Manufacturing Technologies for Liquid Rocket Engine Components
Electric Aircraft Cryogenic Cooling with Thermo-Acoustic Exergy Management
Effects of Strong Wall Cooling on Supersonic and Hypersonic Shock/Boundary-Layer Interactions
CO2 Cryofreezer Coldhead and Cycle Design Insights for Mars ISRU
Cooling of Electric Motors Used for Propulsion on SCEPTOR
NASA Potential Usage of High Temperature Components and Systems
Liquefaction and Storage of In-Situ Oxygen on the Surface of Mars
Liquefaction and Storage of In-Situ Oxygen on the Surface of Mars
Design of an Electric Propulsion System for SCEPTOR
Rapid Fabrication Techniques for Liquid Rocket Channel Wall Nozzles
Rocket Propulsion (RP) 21 Steering Committee Meeting - NASA Spacecraft Propulsion Update
Analysis of a Hydrogen Containment Process for Nuclear Thermal Engine Ground Testing
Modeling of Gaseous Oxygen Liquefaction Inside Mars Ascent Vehicle Propellant Tank
High Performance Mars Liquid Cooling and Ventilation Garment Project
Advanced Propulsion with Onboard Power (APOP) Model Based Approach
Long-Term Cryogenic Propellant Storage for the Titan Orbiter Polar Surveyor (TOPS) Mission
Transformative Advances in DDDAS with Application to Space Weather Monitoring
Mini-Membrane Evaporator for Contingency Spacesuit Cooling
Spacesuit Water Membrane Evaporator Integration with the ISS Extravehicular Mobility Unit
Thermal Runaway Severity Reduction Assessment for EVA Li-ion Batteries
Heating of the Solar Atmosphere: from the Bottom Up?
Evolvable Cryogenics (eCryo) Project Technology Workshop with Industry: Thermal Venting System (TVS)
Overview of SBIR Phase 2 Airbreathing Propulsion Technologies
Einfluss der Rippenposition in einem Kühlkanal auf die Filmkühlung und den inneren Wärmeübergang