Herr M. Sc.

Francesco Romano

Akademischer Mitarbeiter: DISCOVERER: ABEP, IPT, birdcage, Helicon
Institut für Raumfahrtsysteme

Kontakt

+49 711 685-62399

Pfaffenwaldring 29
70569 Stuttgart
Deutschland

Sprechstunde

Einfach mir eine Email schicken!

Für Bachelor oder Masterarbeiten bitte immer Cv, Motivationschreiben, Notenspiegel zuschicken.

Fachgebiet

Elektrische Raumfahrtantriebe

Atmosphärenatmendes elektrisches Antriebsystem mit induktiven Plasmatriebwerken

DISCOVERER H2020 EU Projekt, mehr  https://discoverer.space/

  • Induktive Plasmatriebwerke;
  • Helicon Plasma;
  • RF Antenne, Birdcage;
  • Einlassentwurf, DSMC;
  • Plasmabeschleunigung;
  • Induktiv beheizter Plasmagenerator, IPG6-S.

Mehr dazu hier.

F. Romano, G. Herdrich, et al. "Inductive Plasma Thruster (IPT) design for an Atmosphere-Breathing Electric Propulsion System (ABEP) ", 70th International Astronautical Congress (IAC), Washington D.C., USA, October 2019, IAC-19,C4,6,3,x49922. 

F. Romano, G. Herdrich, et al. "Inductive Plasma Thruster (IPT) for an Atmosphere- Breathing Electric Propulsion System: Design and Set in Operation", 36th International Electric Propulsion Conference (IEPC), Vienna, Austria, September 2019, IEPC-2019-A488.

S. Masillo, F. Romano, R. Soglia, G. Herdrich, P. Roberts et al. "Analysis of electrodeless plasma source enhancement by an externally applied magnetic field for an inductive plasma thruster (IPT)", 7th Russian-German Conference on Electric Propulsion, Rauischholzhausen, Germany, October 2018, A079.

F. Romano, G. Herdrich, P. C.E. Roberts, et al. "Advances on the Inductive Plasma Thruster Design for an Atmosphere-Breathing EP System", 69th International Astronautical Congress (IAC), Bremen, Germany, October 2018,  IAC-18.C4.6.4x46387.

F. Romano, G. Herdrich, T. Binder, A. Boxberger, C. Traub, S. Fasoulas, T. Schönherr, P. Roberts,  et al.,  "Effects of applied magnetic field on IPG6-S, test-bed for an ABEP-based inductive plasma thruster (IPT)", Space Propulsion 2018, Seville, Spain, 14-18/05/2018, SP2018 00412.

F. Romano, B. Massuti-Ballester, T. Binder, G. Herdrich, S. Fasoulas, T. Schönherr, "System analysis and test-bed for an atmosphere-breathing electric propulsion system using an inductive plasma thruster", Acta Astronautica 147:114-126, June 2018, DOI: 10.1016/j.actaastro.2018.03.031

F. Romano, G. Herdrich, S. Fasoulas, T. Schönherr, et al. "Performance Evaluation of a Novel Inductive Atmosphere-Breathing EP System", 35th International Electric Propulsion Conference (IEPC), Atlanta, USA, October 2017, IEPC-2017-184.

F. Romano, T. Binder, G. Herdrich, P. C.E. Roberts, et al. "System Analysis and Test-Bed for an Atmosphere-Breathing Electric Propulsion System using an Inductive Plasma Thruster", 68th International Astronautical Congress (IAC), Adelaide, Australia, September 2017,  IAC-17-C4,6,5,x41810.

 M. Dropmann, M. Ehresmann, A. S. Pagan, Q. H. Le, F. Romano, C. Montag, and G. Herdrich, "Low Power Arcjet Application for end of Life Satellite Servicing", 7th European Conference on Space Debris, At ESA/ESOC, Darmstadt, Germany, April 2017.

T. Binder, P.C. Boldini, F. Romano, G. Herdrich,  and S. Fasoulas, "Transmission Probabilities of Rarefied Flows in the Application of Atmosphere-Breathing Electric Propulsion", AIP Conference Proceedings, 1786, 190011 (2016), DOI: http://dx.doi.org/10.1063/1.4967689

F. Romano, T. Binder, G. Herdrich, S. Fasoulas and T. Schönherr, "Intake Design for an Atmosphere-Breathing Electric Propulsion System", Space Propulsion 2016, Roma, Italy, 2-6/05/2016.

F. Romano, T. Binder, G. Herdrich, S. Fasoulas and T. Schönherr, "Air-Intake Design Investigation for an Air-Breathing Electric Propulsion System", 34th IEPC - International Electric Propulsion Conference, Kobe, Japan, 4-10/10/2015, July 2015.

T. Schönherr, K. Komurasaki, F. Romano, B. Massuti-Ballester, G. Herdrich, “Analysis of Atmosphere-Breathing Electric Propulsion”, IEEE Transactions on Plasma Science, vol.43, no.1, Jan. 2015. 

F. Romano, B. Massuti-Ballester, T. Schönherr and G. Herdrich, “System Analysis and Test Bed for an Air-Breathing Electric Propulsion System”, 5th RGCEP - Russian-German Conference on Electric Propulsion and their Applications, Dresden, Germany, 07-12/09/2014, Sep. 2014.

  • Unkonventionelle Raumfahrtantriebe: "Atmosphere-Breathing Electric Propulsion", Master Studiengang.
  • Elektrische und unkonventionelle Raumfahrtantriebe: "Induktives Triebwerk und Hybridantriebe", Master Studiengang

1988 in Sassari, Italien geboren.
2007 Abitur Luftfahrttechnik, Udine, Italien.
2011 Bachelor in Luft- und Raumfahrttechnik, Universität Padua, Italien.
2012 Auslandssemester an der TU-Dresden, Luft-und Raumfahrttechnik, ERASMUS.
2013 Diplom in Orgel und Orgel Komposition an der Konservatorium Rovigo, Italien.
2013-14 Master Arbeit an der Universität Stuttgart, System Analysis and Test-Bed for an Air-Breathing Electric Propulsion System.
2014 Master in Luft- und Raumfahrttechnik, Universität Padua, Italien.
Seit November 2014 Promotion: “RAM Augmented Inductively Heated Plasma Thruster”.
2015 Preis „Freunde der Universität Stuttgart“ für die beste Master Arbeit.
Seit März 2018 Akademischer Mitarbeiter

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