María Scherezade Barquero Balsera

  • Nationality: Spanish

PhD Thesis

Diagnostics for time-varying exhaust reconstruction applied to a low-power Pulsed Plasma Thruster: Thruster design, development, and characterization

Date of Defense: 31 July 2025

Supervisors

Eduardo Ahedo (UC3M), Mario Merino Martínez (UC3M) and Jaume Navarro Cavallé (UC3M)

Abstract

The current numerical and experimental work spans over the study of a micro Ablative Pulsed Plasma Thruster. A MHD code and a self-contained thruster are being developed from scratch, to provide insight about the discharge process along all its stages, in both terms, physical and about performance.

PPT transient plume cross-section current density distribution at nominal conditions by means of the WAVES  (Wire Array for Variable Exhaust Scanning) experimental diagnostic technique.

MARTINLARA – Millimeter wave Array at Room Temperature for INstruments in LEO Altitude Radio Astronomy

Comunidad de Madrid and European Comission – European structural and investment funds

Research Stays

Institutions: Japan Aerospace Exploration Agency (JAXA)
Department/Group: Institute of Space and Astronautical Science: ISAS
Host: Ryudo Tsukizaki
Period: from September 2022 to November 2022

Doctoral Meetings 2023-2024

PhD Doctoral Meetings 2024 Scherezade Barquero

Doctoral Meetings 2022-2023

PhD Doctoral Meetings 2023 Scherezade Barquero

Doctoral Meetings 2021-2022

PhD Aerospace Engineering Doctoral Meetings 21-22 – M. Scherezade

Doctoral Meetings 2020-2021

PhD Aerospace – Doctoral Meetings 20-21- M. S. Barquero

Leave a comment