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Kühlkreislauf
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Regulation of Thermal Sweating in Eva Space Suits
On the Nature of Io's Thermal Reservoir Unit
Effect of Exhaust Pressure on the Cooling Characteristics of an Air-cooled Engine
Program for Sea Level Test Firing of Rocket Engines Final Report, 1 Sep. 1964 - 1 Feb. 1965
An Analysis of Thermal Balance in the Cooled Cabin of a Sea King Helicopter
The a.R.L. Supersonic Propulsion Test Facility - Thermodynamic Design of Regenerative Heat Exchanger
The Influence of Spray Coolers on the Range of Operation of High-Altitude Propulsion Test Facilities
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
A radiation-cooled nuclear rocket nozzle for long firing durations.
SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINES
Overview of ESA Cryocooler Activities
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