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The 5-kW arcjet power electronicsThe initial design and evaluation of a 5 kW arcjet power electronics breadboard which as been integrated with a modified 1 kW design laboratory arcjet is presented. A single stage, 5 kW full bridge, pulse width modulated (PWM), power converter was developed which was phase shift regulated. The converter used metal oxide semiconductor field effect transistor (MOSFET) power switches and incorporated current mode control and an integral arcjet pulse ignition circuit. The unoptimized power efficiency was 93.5 and 93.9 percent at 5 kW and 50A output at input voltages of 130 and 150V, respectively. Line and load current regulation at 50A output was within one percent. The converter provided up to 6.6 kW to the arcjet with simulated ammonia used as a propellant.
Document ID
19890015075
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gruber, R. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Gott, R. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Haag, T. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1989
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 89-2725
NAS 1.15:102108
NASA-TM-102108
E-4876
Report Number: AIAA PAPER 89-2725
Report Number: NAS 1.15:102108
Report Number: NASA-TM-102108
Report Number: E-4876
Meeting Information
Meeting: Joint Propulsion Conference
Location: Monterey, CA
Country: United States
Start Date: July 10, 1989
End Date: July 12, 1989
Sponsors: ASEE, ASME, SAE, AIAA
Accession Number
89N24446
Funding Number(s)
PROJECT: RTOP 506-42-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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