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Kühlkreislauf
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Sub-Kelvin Coolers for Space Missions: ADR Development at NASA/GSFC
A Laboratory Comparison of Three Methods of Personal Conditioning
A Laboratory Comparison of Three Methods of Personal Conditioning
Investigation of External Refrigeration Systems for Long Term Cryogenic Storage
NASA Space Cryocooler Programs: A 2003 Overview
Clock Technology Development for the Laser Cooling and Atomic Physics (LCAP) Program
Investigation of Cooling Problems at High Chamber Pressures Final Report, 1 Jul. 1963 - 31 Mar. 1965
Investigation of Cooling Problems at High Chamber Pressures Final Report, 1 Jul. 1963 - 31 Mar. 1965
Heating of the Solar Atmosphere: from the Bottom Up?
Analytical Study of Moderator Wall Cooling of Gaseous Nuclear Rocket Engines
Experimental Snow Plenum Air Cooling System for Byrd Station, Antarctica
Investigation of Aircraft Heaters. 25 - Use of the Thermopile Radiometer
Final Qualification and Early On-Orbit Performance of the HESSI Cryocooler
Analysis of a Hydrogen Containment Process for Nuclear Thermal Engine Ground Testing
Evaluation of an Infrared Heating Simulation of a Mach 4.63 Flight on an X 15 Horizontal Stabilizer
OPTIMISM Experiment and Development of Space-Qualified Seismometers in France
Study of Transformations in T-A6V Titanium Alloy under Continuous Cooling
Design of a Convective Cooling System for a Mach 6 Hypersonic Transport Airframe
Electric Aircraft Cryogenic Cooling with Thermo-Acoustic Exergy Management
The Influence of Gravity on Heat Transfer in Heat Pipes
Effects of Strong Wall Cooling on Supersonic and Hypersonic Shock/Boundary-Layer Interactions
Silent, 3.75 KW Liquid Hydrocarbon-Air Fuel Cell Powerplant. Volume II. Figures and Tables
Structural Design for Aerodynamic Heating. Part II. Analytical Studies
Influence of a Retarding Rocket on Parameter Limits for Reentry Trajectories
Study of Premixed, Shock-Induced Combustion With Application to Hypervelocity Flight
Heatpipes and Vapor Chambers for Satellite Thermal Balance
Propulsion Apparatus and Method Using Boil-off Gas from a Cryogenic Liquid
Air Heating by a Rotating Arc with Cold Gas Flow Transverse to the Axis of the Arc
Aerocooling of a 12-Inch Diameter Missile During Air Carry