Jason M. Makela, Ph.D.
Affiliations: | 2010 | Mechanical Engineering-Engineering Mechanics | Michigan Technological University, USA |
Area:
Aerospace Engineering, Materials Science EngineeringGoogle:
"Jason Makela"Parents
Sign in to add mentor| Lyon B. King | grad student | 2010 | Michigan Technological University | |
| (Re-generable field emission cathodes for electric propulsion.) | ||||
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Publications
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| Makela JM, Washeleski RL, King LB. (2011) Regenerable field emission cathodes: Surface morphology and performance Journal of Propulsion and Power. 27: 1097-1107 |
| Makela JM, Washeleski RL, Massey DR, et al. (2010) Development of a magnesium and zinc hall-effect thruster Journal of Propulsion and Power. 26: 1029-1035 |
| Makela JM, Washeleski RL, King LB. (2010) Re-generable field emission cathodes part II: Quenched emitter performance analyses 46th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit |
| Makela JM, L. Washeleski R, King LB. (2009) Regenerable field emission cathode for spacecraft neutralization Journal of Propulsion and Power. 25: 970-975 |
| Makela JM, Washeleski RL, King LB. (2009) Surface morphology and lifetime assessment of a re-generable field-emission cathode for low power electric propulsion 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit |
| Makela JM, Massey DR, King LB. (2008) Bismuth hollow cathode for hall thrusters Journal of Propulsion and Power. 24: 142-146 |
| Makela JM, King LB. (2008) Operating characteristics of a re-generable field emission cathode for low-power Electric Propulsion 44th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit |
| Massey DR, King LB, Makela JM. (2008) Development of a direct evaporation bismuth hall thruster 44th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit |
| Makela JM, King LB. (2007) Re-generable field emission cathodes for low-power electric propulsion Collection of Technical Papers - 43rd Aiaa/Asme/Sae/Asee Joint Propulsion Conference. 2: 1680-1686 |
| Makela JM, Massey DR, King LB. (2006) Performance characteristics of a LaB6 bismuth cathode for use with Hall thrusters Collection of Technical Papers - Aiaa/Asme/Sae/Asee 42nd Joint Propulsion Conference. 4: 3193-3199 |