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Life and Operating Range Extension of the BPT-4000 Qualification Model Hall Thruster
Author(s) -
Ben Welander,
Christian Carpenter,
Kristi de Grys,
Richard R. Hofer,
Thomas Randolph,
David Manzella
Publication year - 2006
Publication title -
nasa technical reports server (nasa)
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2006-5263
Subject(s) - extension (predicate logic) , life extension , range (aeronautics) , aeronautics , engineering , electrical engineering , aerospace engineering , computer science , simulation , programming language , gerontology , medicine
Following completion of the 5,600 hour qualification life test of the BPT-4000 4.5 kW Hall Thruster Propulsion System, NASA and Aerojet have undertaken efforts to extend the qualified operating range and lifetime of the thruster to support a wider range of NASA missions. The system was originally designed for orbit raising and stationkeeping applications on military and commercial geostationary satellites. As such, it was designed to operate over a range of power levels from 3 to 4.5 kW. Studies of robotic exploration applications have shown that the cost savings provided by utilizing commercial technology that can operate over a wider range of power levels provides significant mission benefits. The testing reported on here shows that the 4.5 kW thruster as designed has the capability to operate efficiently down to power levels as low as 1 kW. At the time of writing, the BPT- 4000 qualification thruster and cathode have accumulated over 400 hours of operation between 1 kW-2 kW with an additional 600 hours currently planned. The thruster has demonstrated no issues with longer duration operation at low power.

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