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Investigation into High Power Converter Topologies
STATIC POWER CONVERSION FOR SPACECRAFT
Research on spacecraft and powerplant integration problems Spacecraft analysis topical report
Design of a multi-kilowatt photovoltaic power system for manned space stations.
Development of a hydrogen-oxygen space power supply system Progress report, 1-30 Sep. 1963
DEVELOPMENT OF ELECTRIC PROPULSION POWER SYSTEMS
Development of a hydrogen-oxygen space power supply system Progress report, 1-31 Dec. 1963
Development of a hydrogen-oxygen space power supply system Progress report, 1-30 Nov. 1963
THE DESIGN OF THE UNITED KINGDOM SCIENTIFIC SATELLITE SOLAR POWER SYSTEM
Structural and electrical performance of a large concentrating solar cell panel.
Power conditioning - inversion, conversion, and regulation
Solar power systems for satellites in near- earth orbits.
Development of a thermionic diode controlled power system
Cycle life test of secondary spacecraft cells first annual report
Nimbus-B solar-conversion power supply subsystem Quarterly technical report, Jun. - Aug. 1966
Characteristics of solar concentrators as applied to space power systems
Hypergolic engine space power system Volume I - Technical
Nuclear power for space travel
Nondissipative solar array optimum charge regulator Final report
Applications of snap-50 class powerplants to selected unmanned electric propulsion missions.
REQUIREMENTS FOR HIGH TEMPERATURE MATERIALS FOR SPACE VEHICLES
Design of space satellite power converter- regulators for minimum magnetic disturbance.
Design guidelines for circuitry in a nuclear reactor-propelled spacecraft Final report
Non dissipative solar array optimum charge regulator First quarterly report
SOLAR-CELL POWER SYSTEMS TESTING
Interplanetary monitoring platform IMP III - Explorer XXVIII Interim flight report no. 2
Characterization of recombination and control electrodes for spacecraft nickel- cadmium cells
Nimbus-B solar-conversion power supply subsystem Quarterly technical report no. 3, Mar. - May 1966
Secondary zinc-oxygen cell for spacecraft applications Quarterly report, 23 Sep. - 23 Dec. 1966