Search NASAโŒ• Search

NASA NTRS ยท 19750040903

Control logic for a 30 cm diameter ion thruster

Abstract

Tests with a 30 cm thruster having EMT critical components have defined start-up criteria. Of the three phases comprising the start-up mode, the preheat phase is intended to heat critical feed system components to desired temperatures. Of the seven supplies available during the preheat phase, only three were found to be useful for purposes of preheating the thruster. These were the cathode and neutralizer tip heater supplies and the isolator heater supply. If the needed temperatures are attained during preheat, the ignition phase requires only several seconds. The heat phase serves to establish the proper propellant flow rates prior to the transition to the run mode. Using these techniques, a thruster with initial temperatures in the range of -15 to +25 C can be reliably started and provide a 1.0 amp beam within 45 min. High voltage recycle time profiles indicate limitations on several time functions.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Bechtel, R. T.. 1975-03-01. Control logic for a 30 cm diameter ion thruster. https://ntrs.nasa.gov/citations/19750040903

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