Arcjet starting reliability - A multistart test on hydrogen/nitrogen mixturesAn arcjet starting reliability test was performed to investigate one feasibility issue in the use of arcjets on board a satellite for north-south stationkeeping. A 1 kW arcjet was run on hydrogen/nitrogen gas mixtures simulating decomposed hydrazine. A pulse width modulated power supply with an integral high voltage starting pulser was used for arc ignition and steady-state operation. The test was performed in four phases in order to determine if starting characteristics changed as a result of long term thruster operation. More than 300 successful starts were accumulated over an operating time of 18 hr. Overall results indicate that there is a link between starting characteristics and long term thruster operation; however, the large number of starts had no effect on steady-state performance.
Document ID
19870053854
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Haag, Thomas W. (NASA Lewis Research Center Cleveland, OH, United States)
Curran, Frank M. (NASA Lewis Research Center Cleveland, OH, United States)