TY - GEN
T1 - Multiple-kilowatt-class graphite heater for large hollow cathode ignition
AU - Wordingham, Christopher J.
AU - Taunay, Pierre Yves C.R.
AU - Choueiri, Edgar Y.
N1 - Publisher Copyright:
© 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2015
Y1 - 2015
N2 - A graphite heater design capable of operating in the multiple-kilowatt power range with an estimated life of over 40 years of continuous operation has been developed to address the power and operational life requirements of large lanthanum hexaboride hollow cathodes. Larger hollow cathodes are capable of increased discharge currents, but require higher heater powers to ignite. Legacy heater designs suffer from material interactions and increased failure rates at high temperatures and are currently not viable for high-power operation; a graphite heater can provide high power and long operational life simultaneously. Two models, a simplified circuit model and a finite-element model, have been developed to predict the operating temperature and resistance of the graphite heater design. The sublimation-limited operational life of the heater was estimated using a Hertz-Knudsen evaporation model and an alternate vacuum sublimation model proposed by Thieberger. A prototype heater has been fabricated and tested using a large-diameter lanthanum hexaboride hollow cathode to demonstrate the feasibility of the graphite heater design. The prototype has repeatedly achieved cathode ignition and has been tested at up to 4.5 kW of heater power. The temperatures of the cathode and heater element were measured during heating prior to ignition and used to calculate the heater resistance, which was found to agree fairly well with the predicted values. The exposed portion of the heater element and the cathode tube tip reached temperatures of just over 1300 and 1200°C, respectively. For a peak surface operating temperature of 1500°C, both heater sublimation life models predict a 1% loss life of approximately 400 kh.
AB - A graphite heater design capable of operating in the multiple-kilowatt power range with an estimated life of over 40 years of continuous operation has been developed to address the power and operational life requirements of large lanthanum hexaboride hollow cathodes. Larger hollow cathodes are capable of increased discharge currents, but require higher heater powers to ignite. Legacy heater designs suffer from material interactions and increased failure rates at high temperatures and are currently not viable for high-power operation; a graphite heater can provide high power and long operational life simultaneously. Two models, a simplified circuit model and a finite-element model, have been developed to predict the operating temperature and resistance of the graphite heater design. The sublimation-limited operational life of the heater was estimated using a Hertz-Knudsen evaporation model and an alternate vacuum sublimation model proposed by Thieberger. A prototype heater has been fabricated and tested using a large-diameter lanthanum hexaboride hollow cathode to demonstrate the feasibility of the graphite heater design. The prototype has repeatedly achieved cathode ignition and has been tested at up to 4.5 kW of heater power. The temperatures of the cathode and heater element were measured during heating prior to ignition and used to calculate the heater resistance, which was found to agree fairly well with the predicted values. The exposed portion of the heater element and the cathode tube tip reached temperatures of just over 1300 and 1200°C, respectively. For a peak surface operating temperature of 1500°C, both heater sublimation life models predict a 1% loss life of approximately 400 kh.
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U2 - 10.2514/6.2015-4010
DO - 10.2514/6.2015-4010
M3 - Conference contribution
AN - SCOPUS:85088196114
SN - 9781624103216
T3 - 51st AIAA/SAE/ASEE Joint Propulsion Conference
BT - 51st AIAA/SAE/ASEE Joint Propulsion Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015
Y2 - 27 July 2015 through 29 July 2015
ER -