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Development, integration, and testing of a 30 cm thruster/power conditioning and control system.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.
Document ID
19720043758
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Herron, B. G.
Collett, C. R.
(Hughes Research Laboratories Malibu, Calif., United States)
Garth, D. R.
(Hughes Aircraft Co. Los Angeles, Calif., United States)
Date Acquired
August 6, 2013
Publication Date
April 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 72-509
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Electric Propulsion Conference
Location: Bethesda, MD
Start Date: April 17, 1972
End Date: April 19, 1972
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
72A27424
Funding Number(s)
CONTRACT_GRANT: NAS3-14140
CONTRACT_GRANT: NAS3-15523
Distribution Limits
Public
Copyright
Other

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