Spacecraft charging control by thermal, field emission with lanthanum-hexaboride emitters

Details Spacecraft charging control by thermal, field emission with lanthanum-hexaboride emitters Spacecraft charging control by thermal, field emission with lanthanum-hexaboride emitters

Aug 1978

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1978stin...7832014m&link_type=abstract

Unknown

Computer Science

Field Emission, Lanthanum Alloys, Spacecraft Charging, Thermionic Emitters, Electric Potential, Plasma Diagnostics, Thermal Emission, Tungsten

Scientific paper

Thermal, field emitters of lanthanum (or perhaps cerium) hexaboride (LaB6) with temperature variability up to about 1500K are suggested for spacecraft charging control. Such emitters operate at much lower voltages with considerably more control and add plasma-diagnostic versatility. These gains should outweigh the additional complexity of providing heat for the LaB6 thermal, field emitter.

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