Thermal energy storage supporting research Final technical report, Apr. 1, 1965 - Sep. 30, 1966
The requirements placed on electron tubes for space applications.
The integration of radioisotope thermoelectric systems and spacecraft.
The electrical power system for the Pegasus satellite
THE DESIGN OF THE UNITED KINGDOM SCIENTIFIC SATELLITE SOLAR POWER SYSTEM
Structural and electrical performance of a large concentrating solar cell panel.
STATIC POWER CONVERSION FOR SPACECRAFT
Solar power systems for satellites in near- earth orbits.
SOLAR-CELL POWER SYSTEMS TESTING
Silver zinc batteries power supply for the Atmosphere Explorer-B spacecraft /AE-B/
Secondary zinc-oxygen cell for spacecraft applications Quarterly report, 23 Sep. - 23 Dec. 1966
Research on spacecraft and powerplant integration problems Spacecraft analysis topical report
REQUIREMENTS FOR HIGH TEMPERATURE MATERIALS FOR SPACE VEHICLES
Rankine cycle powerplant characteristics for electric propulsion manned Mars mission.
Principles of power distribution and sequencing.
Power conditioning - inversion, conversion, and regulation
Nuclear power for space travel
Non dissipative solar array optimum charge regulator First quarterly report
Nondissipative solar array optimum charge regulator Final report
Nimbus-B solar-conversion power supply subsystem Quarterly technical report no. 3, Mar. - May 1966
Nimbus-b Solar-conversion Power Supply Subsystem Quarterly Technical Report No. 1, Sep. - Nov. 1965
Nimbus-B solar-conversion power supply subsystem Quarterly technical report, Jun. - Aug. 1966
Nickel Cadmium Spacecraft Battery Charge Control with Auxiliary Electrodes