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NASA NTRS · 19720043758

Development, integration, and testing of a 30 cm thruster/power conditioning and control system.

Abstract

The 30 cm thruster/power conditioning and control system discussed represents a significant milestone in the evolution of prime ion propulsion systems. The effort described covers three distinct electronic hardware implementation, integration and testing phases; development of a flight-type power conditioner for laboratory testing, development of a thruster control system to control the power conditioning for demonstrating continuously variable automatic thruster throttling from a single control over a range in excess of 5:1, and finally development of an automated endurance test system incorporating many of the above designs for a 6000 hour thruster life test.

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BibTeXRIS

Herron, B. G., Collett, C. R., Garth, D. R.. 1972-04-01. Development, integration, and testing of a 30 cm thruster/power conditioning and control system.. https://ntrs.nasa.gov/citations/19720043758

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