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Low-current, xenon orificed hollow cathode performance for in-space applications

Publication ,  Journal Article
Domonkos, MT; Patterson, MJ; Gallimore, AD
Published in: Journal of Propulsion and Power
January 1, 2003

An experimental investigation of the operating characteristics of 3.2-mm-diam orificed hollow cathodes was conducted to examine low-current and low flow-rate operation. Cathode power for self-sustaining keeper operation was minimized with an orifice aspect ratio of approximately one or through the use of an enclosed keeper. For spot-mode emission cathode flow-rate requirements were proportional to orifice diameter and the inverse of the orifice length. The minimum power consumption in diode mode was 10 W, and the minimum mass flow rate required for spot-mode emission was approximately 0.08 mg/s. Cathode temperature profiles were obtained using an imaging radiometer, and conduction was found to be the dominant heat-transfer mechanism from the cathode tube. Orifice plate temperatures were found to be weakly dependent upon the flow rate and strongly dependent upon the current.

Duke Scholars

Published In

Journal of Propulsion and Power

DOI

EISSN

1533-3876

ISSN

0748-4658

Publication Date

January 1, 2003

Volume

19

Issue

3

Start / End Page

438 / 443

Related Subject Headings

  • Aerospace & Aeronautics
  • 4001 Aerospace engineering
  • 0913 Mechanical Engineering
  • 0901 Aerospace Engineering
  • 0202 Atomic, Molecular, Nuclear, Particle and Plasma Physics
 

Citation

APA
Chicago
ICMJE
MLA
NLM
Domonkos, M. T., Patterson, M. J., & Gallimore, A. D. (2003). Low-current, xenon orificed hollow cathode performance for in-space applications. Journal of Propulsion and Power, 19(3), 438–443. https://doi.org/10.2514/2.6127
Domonkos, M. T., M. J. Patterson, and A. D. Gallimore. “Low-current, xenon orificed hollow cathode performance for in-space applications.” Journal of Propulsion and Power 19, no. 3 (January 1, 2003): 438–43. https://doi.org/10.2514/2.6127.
Domonkos MT, Patterson MJ, Gallimore AD. Low-current, xenon orificed hollow cathode performance for in-space applications. Journal of Propulsion and Power. 2003 Jan 1;19(3):438–43.
Domonkos, M. T., et al. “Low-current, xenon orificed hollow cathode performance for in-space applications.” Journal of Propulsion and Power, vol. 19, no. 3, Jan. 2003, pp. 438–43. Scopus, doi:10.2514/2.6127.
Domonkos MT, Patterson MJ, Gallimore AD. Low-current, xenon orificed hollow cathode performance for in-space applications. Journal of Propulsion and Power. 2003 Jan 1;19(3):438–443.

Published In

Journal of Propulsion and Power

DOI

EISSN

1533-3876

ISSN

0748-4658

Publication Date

January 1, 2003

Volume

19

Issue

3

Start / End Page

438 / 443

Related Subject Headings

  • Aerospace & Aeronautics
  • 4001 Aerospace engineering
  • 0913 Mechanical Engineering
  • 0901 Aerospace Engineering
  • 0202 Atomic, Molecular, Nuclear, Particle and Plasma Physics