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Kühlsystem
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Advanced and Additive Manufacturing Technologies for Liquid Rocket Engine Components
A large ultrahigh-vacuum environmental chamber with liquid-helium-cooled liner.
Altitude Performance Characteristics of Tail-pipe Burner with Variable-area Exhaust Nozzle
A Method for the Design of Cooling Systems for Aircraft Power-plant Installations
A Method for Welding Sheet Aluminum to SAE 4140 Steel
Analytical solution of the ''known-heat-load'' space radiator problem.
An analysis of supersonic aerodynamic heating with continuous fluid injection
AN EXPERIMENTAL INVESTIGATION OF GASEOUS-FILM COOLING OF A ROCKET MOTOR
An experimental investigation of rectangular exhaust-gas ejectors applicable for engine cooling
A Preliminary Investigation of Exhaust-gas Ejectors for Ground Cooling
A probe for total-enthalpy measurements in arcjet exhausts.
A radiation-cooled nuclear rocket nozzle for long firing durations.
A Summary of Drag Results from Recent Langley Full Scale Tunnel Tests of Army and Navy Airplanes