1.9 MWe Nuclear Electric Propulsion-Chemical Propulsion Piloted Mars Opposition Vehicle
6-ft High-Power Electric Propulsion Test Port, EPL Tank 5 Installed
6TH Annual Report to Congress for Fiscal Year 1982. Electric and Hybrid Vehicles Program
8- by 6-Foot Supersonic Wind Tunnel Compressor Inspected
9.5-Foot Paraboloidal Master and Concentrator Final Report
12.5kW Advanced Electric Propulsion System Thruster Development Testing
13kW Advanced Electric Propulsion Flight System Development and Qualification
30 KW Class Arcjet Advanced Technology Transition Development (ATTD)
100 Watt Thermoelectric Power System for Buoy Applications
100 Watt Thermoelectric Power System for Buoy Applications
115 Vac Single-Phase Arc-Fault Circuit Breaker Flight Test
150 kW Class Solar Electric Propulsion Spacecraft Power Architecture Model
270V Battery Using COTS NiCd Cells For Manned Spacecraft
270 Volt Direct Current Generating System: Design, Development and Test
1000 Hours of Testing Completed on 10-kW Hall Thruster