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  1. Hampl, Sebastian K., et al. "Comparison of computational algorithms for simulating an electrospray plume with a n-body approach." Journal of Electric Propulsion 1.1 (2022): 1-26.

  2. Bendimerad, R., & Petro, E. (2022). Molecular dynamics studies of ionic liquid-surface interactions for electrospray thrusters. Journal of Electric Propulsion, 1(1), 1-16

  3. Petro, E. M., Gallud, X., Hampl, S. K., Schroeder, M., Geiger, C., & Lozano, P. C. (2022). Multiscale modeling of electrospray ion emission. Journal of Applied Physics, 131(19), 193301.

  4. Cidoncha, X. G., Lozano, P. C., Bendimerad, R., Petro, E. M., & Hampl, S. K. (2022, March). Modeling and Characterization of Electrospray Propellant-Surface Interactions. In 2022 IEEE Aerospace Conference (AERO) (pp. 1-11). IEEE.

  5. Brophy, J., Pellegrino, S., Lubin, P., Alkalai, L., Atwater, H., Biswas, A., ... & Sellers, I. (2022). Non-Nuclear Exploration of the Solar System Study.

  6. Sheerin, T. F., Petro, E., Winters, K., Lozano, P., & Lubin, P. (2021). Fast Solar System transportation with electric propulsion powered by directed energy. Acta Astronautica, 179, 78-87.

  7. Sanghvi, R., Ni, D., Gund, V., Ji, Q., Schenkel, T., Afridi, K. K., ... & Petro, E. (2021). Application of Microelectromechanical-system based RF Linear Accelerators for Ultra-High Specific Impulse Ion Micropropulsion. In AIAA Propulsion and Energy 2021 Forum (p. 3246).

  8. van Paridon, A., & Petro, E. (2021). Survey of water powered propulsion systems. In AIAA Propulsion and Energy 2021 Forum (p. 3566).

  9. Petro, E. M., & Sedwick, R. J. (2020). Correction: Effects of Water Vapor Propellant on Electrodeless Thruster Performance. Journal of Propulsion and Power, 36(6), AU2-AU3.

  10. Petro, E., Bruno, A., Lozano, P., Perna, L. E., & Freeman, D. (2020). Characterization of the TILE electrospray emitters. In AIAA Propulsion and Energy 2020 Forum (p. 3612).

  11. Petro, E. M., Miller, C. E., Schmidt, J., & Lozano, P. C. (2019, September). Development of an electrospray fragmentation model for kinetic plume modeling. In International Electric Propulsion Conference (p. 830).

  12. Petro, E. M., Cezairli, M., Schroeder, M., & Lozano, P. C. (2019, September). Investigation of Electrospray Plume Composition during Voltage Transients. In 2019 International Electric Propulsion Conference.

  13. MacArthur, J., Kristinsson, B. O., Freeman, D., Petro, E., Li, H., & Lozano, P. C. (2019, September). Microfluidic and Extractor Electrode Update in the ion-Electrospray Propulsion System. In 36th International Electric Propulsion Conference, Vienna, Austria.

  14. Kristinsson, Ö., Freeman, D., Petro, E., Lozano, P. C., Hsu, A., Young, J. A., & Martel, F. (2019, September). Operation and Performance of a Fully-Integrated ionic-Electrospray Propulsion System. In Proceedings of the 36th International Electric Propulsion Conference, Vienna, Austria (pp. 15-20).

  15. Petro, E. M. (2019). Effects of Water Plasma Chemistry on Helicon Thruster Performance (Doctoral dissertation).

  16. Petro, E. M., Sedwick, R. J., & Brieda, L. (2019). Pic simulations of chemistry effects in an electrodeless water plasma thruster. In AIAA Propulsion and Energy 2019 Forum(p. 3998).

  17. Petro, E. M., & Sedwick, R. J. (2017). Survey of moderate-power electric propulsion systems. Journal of Spacecraft and Rockets, 54(3), 529-541.

  18. Petro, E. M., & Sedwick, R. J. (2017). Effects of water-vapor propellant on electrodeless thruster performance. Journal of Propulsion and Power.

  19. MacKenzie, S. M., Caswell, T. E., Phillips-Lander, C. M., Stavros, E. N., Hofgartner, J. D., Sun, V. Z., ... & Mitchell, K. L. (2016). THEO concept mission: testing the habitability of Enceladus’s Ocean. Advances in Space Research, 58(6), 1117-1137.
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