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AIR CONDITIONING, HELICOPTERS, GENERAL REQUIREMENTS FOR
AIR CONDITIONING, HELICOPTERS, GENERAL REQUIREMENTS FOR
REQUIREMENTS FOR HIGH TEMPERATURE MATERIALS FOR SPACE VEHICLES
The integration of radioisotope thermoelectric systems and spacecraft.
Design and reliability considerations for the mariner mars 1964 spacecraft power system.
Design of space satellite power converter- regulators for minimum magnetic disturbance.
Design and analysis of power conditioning for ion propulsion systems.
Rankine cycle powerplant characteristics for electric propulsion manned Mars mission.
Design of a multi-kilowatt photovoltaic power system for manned space stations.
Solar power systems for satellites in near- earth orbits.
The requirements placed on electron tubes for space applications.
Fabrication and testing of a 6.5 mu H, 1.5 MA, 100 kV inductor
Power conditioner for a coil-gun