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Kühlkreislauf
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A new architecture for avionics thermal management
On the Nature of Io's Thermal Reservoir Unit
Clock Technology Development for the Laser Cooling and Atomic Physics (LCAP) Program
Effect of Exhaust Pressure on the Cooling Characteristics of an Air-cooled Engine
Liquefaction and Storage of In-Situ Oxygen on the Surface of Mars
Liquefaction and Storage of In-Situ Oxygen on the Surface of Mars
Gaseous-film cooling of a rocket motor with injection near the throat
Micro/nano spacecraft thermal control using MEMS-based pumped liquid cooling system
Design of an Electric Propulsion System for SCEPTOR
Study of Novel Refrigeration Methods Final Report
CO2 Cryofreezer Coldhead and Cycle Design Insights for Mars ISRU
Regulation of Thermal Sweating in Eva Space Suits
Program for Sea Level Test Firing of Rocket Engines Final Report, 1 Sep. 1964 - 1 Feb. 1965
Overview of ESA Cryocooler Activities
SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINES
The a.R.L. Supersonic Propulsion Test Facility - Thermodynamic Design of Regenerative Heat Exchanger
Head and/or Torso Cooling during Simulated Cockpit Heat Stress
[Research on a Self-Temperature Regulating Spacecraft Skin System]
An Analysis of Thermal Balance in the Cooled Cabin of a Sea King Helicopter
Space Shuttle Orbit Maneuvering Engine Reusable Thrust Chamber Program
Space Shuttle Orbit Maneuvering Engine Reusable Thrust Chamber Program
The Influence of Spray Coolers on the Range of Operation of High-Altitude Propulsion Test Facilities
Development of Flight Technology for Future Laser-Cooled Space Clocks
Investigation of cooling problems at high chamber pressures final report, 1 jul. 1963 - 31 mar. 1965
A radiation-cooled nuclear rocket nozzle for long firing durations.
Evaporative Cooling Garment System (Ecgs), Part 1 Final Report
Feasibility Study of a Heat-Actuated Environmental Control System for the Navy F-4 Fighter Aircraft
Feasibility Study of a Heat-Actuated Environmental Control System for the Navy F-4 Fighter Aircraft
Advanced Fuel Cell System Thermal Management for NASA Exploration Missions
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
Investigation of Methods for Transpiration Cooling Liquid Rocket Chambers Final Report
Localized Overheating in Aerobee Regeneratively Cooled Thrust Chambers
SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINES
Ground-cooling and Flight Tests of an Airplane Equipped with a Nose-blower Engine Cowling
STUDY OF CHAMBER COOLING TECHNIQUES FOR SPACECRAFT ENGINES. MONTHLY LETTER
Heating of the Solar Atmosphere: from the Bottom Up?
Program for sea level test firing of rocket engines final report, 1 sep. 1964 - 1 feb. 1965
Design and testing of an aerospace dew point hygrometer Final report
Spacecraft temperature control by thermostatic fins Progress report, 1 Jun. - 30 Nov. 1965