Microsystems Fabrication Laboratory--New Class 100 Cleanroom Completed and Certified
Static Frequency Converter System Installed and Tested
6-ft High-Power Electric Propulsion Test Port, EPL Tank 5 Installed
Research Combustion Lab Facility Capabilities and Throughput Enhanced by New Test Stands
Short Takeoff and Vertical Landing Capability Upgraded in NASA Glenn’s 9- by 15-Foot Low-Speed Wind Tunnel
Liquid Propellant Manipulated Acoustically
Midinfrared Temperature Measurement Technique Developed
Hybrid Power Management (HPM) Program Resulted in Several New Applications
Modular Avionics Concept Developed for Microgravity Space Experiments--FEANICS
Hydrogen Fuel Capability Added to Combustor Flametube Rig
Light Microscopy Module Fan Disturbance Characterized Through Microgravity Emissions Laboratory Testing
Integrated Propulsion/Vehicle System Structurally Optimized
Facilities and Test Engineering
Last updated: June 25, 2003
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