Search NASAโŒ• Search

NASA NTRS ยท 19820013378

Inert gas ion thruster

Abstract

Inert gas performance with three types of 12 cm diameter magnetoelectrostatic containment (MESC) ion thrusters was tested. The types tested included: (1) a hemispherical shaped discharge chamber with platinum cobalt magnets; (2) three different lengths of the hemispherical chambers with samarium cobalt magnets; and (3) three lengths of the conical shaped chambers with aluminum nickel cobalt magnets. The best argon performance was produced by a 8.0 cm long conical chamber with alnico magnets. The best xenon high mass utilization performance was obtained with the same 8.0 cm long conical thruster. The hemispherical thruster obtained 75 to 87% mass utilization at 185 to 205 eV/ion of singly charged ion equivalent beam.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Ramsey, W. D.. 1980-12-01. Inert gas ion thruster. https://ntrs.nasa.gov/citations/19820013378

Cite the original work for its findings. Save a collection to share your selection of sources.