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Kühlkreislauf
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A Solar Cell and Heater System to Reduce the Temperature Variation of Units in a Spacecraft
The Rotating Combustion Engine - Compact, Lightweight Power for Aircraft
Analytical solution of the ''known-heat-load'' space radiator problem.
Investigation on the Cooling of Exhaust Gas by Direct Contact Between Exhaust Gas and Water
Thermal Insulation of Small Instrumentation Probes
The London Postal Region Dimmed Headlight Experiment
High Speed Impact Test on a 40FT. Lighting Column Fitted with a Break-Away Joint
Aircraft Instrument and Cockpit Lighting by Red or White Light
Investigations in Chemical Rocket Propulsion Final Report, 1 Jul. 1964 - 31 Dec. 1967
An Analytical Solution of the Impact Behavior of Luminaire Support Assemblies
Advanced Rocket Engine--Storable. Phase 1 Interim Final Report. Part 2. Sections 5 Through 8
Integration of Inlet and Engine — An Airplane Man’s Point of View
Transpiration Cooling System Development for Reentry Vehicles
Vuilleumier Cycle Cryogenic Refrigerator Development
Air Cooler for Hypersonic Wind Tunnels
Evaporative Cooling Garment System (Ecgs), Part 1 Final Report
Exploring in Aerospace Rocketry. 7 - Liquid Propellant Rocket Systems
Acceptance Testing of the Cold Air Supply to Third Stage and Satellite, Launcher 6 A, Woomera
Ventilation Equipment Analysis for Basement Shelters
System Validation Test. Lem Crew Compartment Cooling Unit, Launch Complex 37, Launch Area B
Thermal Process Control of Avionic Equipment and Systems
300-Ekw Thermionic Reactor Design Study. Final Report
Analysis of Three-Fluid, Crossflow Heat Exchangers
Development of a Chemical Heater for a MARS Rough-Landing Capsule
Computer Program for APOLLO Fuel Cell Radiator-Condenser Cooling System Analysis
DC Regulator for Low Pressure Mercury Lamps (Pen-Ray)
The Simulation of Cold Black Space in the Space Chamber of the Dvl in Porz- Wahn
Evaporative Cooling Garment System (Ecgs), Part 2 Final Report
Solution to the Problem of Heat Transport in a Liquid Propellant Rocket Engine
Compound a/Hydrazine Engine Design Study. Part I