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Investigation into High Power Converter Topologies
20W Multi-output Isolated Power Supply Using Secondary Regulated Flyback Topology
Testing of Airplane Installed Environmental Control Systems (ECS)
Airborne Chemicals in Aircraft Cabins
Variable Frequency and Voltage Control of Induction Motor for Electric Vehicles
From the Aviation Value Chain to the Aviation System
Environmental Control Systems for Rotorcraft
Maintenance of Ground Support Equipment
Environmental Control System Contamination
Air Conditioning Systems for Subsonic Airplanes
CH-53E Main Rotor Head Logistics Sustainment Strategy
Photovoltaic systems engineering
Photovoltaic systems engineering
Jet Blast Windshield Rain Removal Systems for Commercial Transport Aircraft
Qualification Procedure for Aerospace Standard Products
Aircraft Gas Turbine Engine Health Management System Development and Integration Guide
IVHM Concepts, Technology and Implementation Overview
Stabilization of Power Supply for the Shinkansen with Power Converters
When Trucks Stop Running, America Stops
Simulation and Optimization of Photovoltaic/Diesel Hybrid System for Off-Grid Banking Industry
Robust Optimal Operation of a Gas Turbine Cogeneration Plant Under Uncertain Energy Demands
Aircraft Tire Inflation-Deflation Equipment
NASA GRC Stirling Power Overview
Hydraulic Hybrid Parcel Delivery Truck Deployment, Testing & Demonstration
Design and Analysis of a Dual Power Supply with Super-Capacitor for EV
Environmental Control for Civil Supersonic Transport
Jet Blast Windshield Rain Removal Systems for Commercial Transport Aircraft
Aircraft Tire Inflation-Deflation Equipment
System Safety Plan for Commercial Vehicles Using Hydrogen as an Alternative Fuel
Aircraft Ground Service Connections Locations and Type
Environmental Control for Civil Supersonic Transport
Pneumatic Ground Power Supplies for Starting Aircraft
Commercial Use of Onboard Resources for Future Manned Space Stations
Evaluation of a CIDI Pre-Transmission Parallel Hybrid Drivetrain with CVT
Photovoltaic Electric Power Applied to Unmanned Aerial Vehicles (UAV)
Recycle Requirements for NASA's 30 cm Xenon Ion Thruster
Development Status of the NASA 30-cm Ion Thruster and Power Processor
QUALIFICATIONS FOR FOUR-WAY SUBBASE MOUNTED AIR VALVES FOR AUTOMOTIVE MANUFACTURING APPLICATIONS
Three-dimensional rail cooling analysis for a repetitively fired railgun
STANDARDIZATION OF LOCATIONS AND TYPE OF AIRCRAFT GROUND SERVICE CONNECTIONS
European Space Power, Volume 1