Three-day battery for 425 C environment.
Three-day battery capable of operation at temperature of 425 degrees C for use on lunar and planetary probes
SPACE PROBE↗
SEARCH · Engineering Papers
Results for “Spacecraft power”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Projected large-scale use of radioisotopes by NASA.
Design of isotopic heat sources for space missions, noting atmospheric contamination when source burns on reentry, source and shield weights, sealing of alpha emitters, etc
HEAT SOURCE↗
Solar-electric propulsion system performance for the 0.1-AU solar probe mission.
Suitability of Saturn IB/Centaur and Atlas/ Centaur launched solar-electric propulsion vehicles for performing 0.1-AU solar probe mission
ELECTRIC PROPULSION↗
Criteria for use of Rankine-MHD systems in space.
Criteria for use of Rankine MHD systems in space
RANKINE CYCLE↗
Conventional and thin-film solar cells
Explore the source record for details and available documents.
THIN FILM↗
Thermal energy storage supporting research Final technical report, Apr. 1, 1965 - Sep. 30, 1966
Thermophysical properties of potential thermal energy storage materials for design of TES THERMIONIC systems for long duration space flights
THERMAL ENERGY STORAGE↗
Nondissipative solar array optimum charge regulator Final report
Optimum charge regulator design evaluation for coupling spacecraft solar array to battery
VOLTAGE REGULATOR↗
Characterization of recombination and control electrodes for spacecraft nickel- cadmium cells
Characterization of recombination and control electrodes for spacecraft nickel cadmium cells
NICKEL-CADMIUM BATTERY↗
Characterization of recombination and control electrodes for spacecraft nickel-cadmium cells Quarterly report, Sep. 9 - Dec. 9, 1966
Characterization of recombination and control electrodes for spacecraft nickel-cadmium batteries
ELECTRODE↗
Characterization of recombination and control electrodes for spacecraft nickel-cadmium cells Quarterly report
Characterization of recombination and control electrodes for spacecraft nickel-cadmium batteries
NICKEL-CADMIUM BATTERY↗
Development and fabrication of advanced battery energy storage system Mid-term report, 27 Sep. 1966 - 26 Mar. 1967
Silver-cadmium secondary battery energy storage system using vented cells for manned orbital spacecraft
SPACECRAFT POWER SUPPLY↗
Life cycle tests Monthly progress report, period ending 31 Mar. 1967
Life cycle tests of nickel-cadmium space cell packs
NASA PROGRAM↗
Evaluation program for secondary spacecraft cells acceptance test of Gulton Industries, Inc. 4.0 ampere-hour flooded, sealed nickel- cadmium secondary spacecraft cells with coulmeter charge control
Acceptance testing of four ampere hour flooded sealed nickel-cadmium secondary spacecraft cells
ENVIRONMENTAL TESTING↗
Development of a 100 watt S-band traveling- wave tube Quarterly report
Development of 100 watt S-band traveling wave tube for space applications
TRAVELING WAVE TUBE↗
Secondary zinc-oxygen cell for spacecraft applications Quarterly report, 23 Sep. - 23 Dec. 1966
Secondary rechargeable zinc-oxygen battery for spacecraft
STORAGE BATTERY↗
Study to investigate and improve the zinc electrode for spacecraft electrochemical cells Quarterly report
Zinc electrode improvement work for use in spacecraft electrochemical cells
ELECTROCHEMICAL CELL↗
Voltage conversion and regulation techniques employed in the prime converter for the anchored interplanetary monitoring platform /AIMP/ spacecraft.
DC-to-DC prime converter for anchored interplanetary monitoring platform spacecraft /AIMP/ transforming power from solar array into suitable level for instrumentation electronics
DIRECT CURRENT /DC/↗
Solar-electric propulsion system performance for a close solar probe mission.
Suitability of Saturn IB/Centaur and Atlas/ Centaur launched solar-electric propulsion vehicles for performing 0.1-AU solar probe mission
ELECTRIC PROPULSION↗