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Design of a multi-kilowatt photovoltaic power system for manned space stations.
Solar power systems for satellites in near- earth orbits.
Aircraft Tire Inflation-Deflation Equipment
Jet Blast Windshield Rain Removal Systems for Commercial Transport Aircraft
Environmental Control Systems for Rotorcraft
REQUIREMENTS FOR HIGH TEMPERATURE MATERIALS FOR SPACE VEHICLES
Qualification Procedure for Aerospace Standard Products
Design of space satellite power converter- regulators for minimum magnetic disturbance.
Air Conditioning Systems for Subsonic Airplanes
Jet Blast Windshield Rain Removal Systems for Commercial Transport Aircraft
Design and reliability considerations for the mariner mars 1964 spacecraft power system.
Airborne Chemicals in Aircraft Cabins
Environmental Control for Civil Supersonic Transport
Testing of Airplane Installed Environmental Control Systems (ECS)
Maintenance of Ground Support Equipment
Aircraft Ground Service Connections Locations and Type
The requirements placed on electron tubes for space applications.
Design and analysis of power conditioning for ion propulsion systems.
Environmental Control System Contamination
Pneumatic Ground Power Supplies for Starting Aircraft
Aircraft Tire Inflation-Deflation Equipment
The integration of radioisotope thermoelectric systems and spacecraft.
Environmental Control for Civil Supersonic Transport
Aircraft Gas Turbine Engine Health Management System Development and Integration Guide
Rankine cycle powerplant characteristics for electric propulsion manned Mars mission.
AIR CONDITIONING, HELICOPTERS, GENERAL REQUIREMENTS FOR
STANDARDIZATION OF LOCATIONS AND TYPE OF AIRCRAFT GROUND SERVICE CONNECTIONS
IVHM Concepts, Technology and Implementation Overview
QUALIFICATIONS FOR FOUR-WAY SUBBASE MOUNTED AIR VALVES FOR AUTOMOTIVE MANUFACTURING APPLICATIONS
AIR CONDITIONING, HELICOPTERS, GENERAL REQUIREMENTS FOR
Space mirrors, sails and screens for better environments and more useful energy