Cite
RF Helicon-based Inductive Plasma Thruster (IPT) Design for an Atmosphere-Breathing Electric Propulsion system (ABEP)
MLA
Romano, Francesco, et al. RF Helicon-Based Inductive Plasma Thruster (IPT) Design for an Atmosphere-Breathing Electric Propulsion System (ABEP). 2020. EBSCOhost, https://doi.org/10.1016/j.actaastro.2020.07.008.
APA
Romano, F., Chan, Y.-A., Herdrich, G., Roberts, P. C. E., Fasoulas, C. T. S., Smith, K., Edmondson, S., Haigh, S., Crisp, N. H., Oiko, V. T. A., Worrall, S. D., Livadiotti, S., Huyton, C., Sinpetru, L. A., Straker, A., Becedas, J., Domínguez, R. M., González, D., Cañas, V., … Heißerer, B. (2020). RF Helicon-based Inductive Plasma Thruster (IPT) Design for an Atmosphere-Breathing Electric Propulsion system (ABEP). https://doi.org/10.1016/j.actaastro.2020.07.008
Chicago
Romano, Francesco, Yung-An Chan, Georg Herdrich, Peter C. E. Roberts, C. Traub S. Fasoulas, K. Smith, S. Edmondson, et al. 2020. “RF Helicon-Based Inductive Plasma Thruster (IPT) Design for an Atmosphere-Breathing Electric Propulsion System (ABEP).” doi:10.1016/j.actaastro.2020.07.008.