Vincent F. Giangaspero
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Vincent F. Giangaspero has a total of 31 co-authors. Here are the top co-authors by number of shared publications:
- Andrea Lani
Department of Mathematics/Centre for mathematical Plasma Astrophysics, KU Leuven
3 shared publications - Alan Viladegut
Aerospace and Aeronautics Department, von Karman Institute for Fluid Dynamics, Rhode-Saint-Genèse, Belgium
2 shared publications - Olivier Chazot
Aeronautics and Aerospace Department von Karman Institute for Fluid Dynamics Chaussée de Waterloo 72 Rhode-st-Genèse 1640 Belgium
2 shared publications Stefaan Poedts
2 shared publications- Vatsalya Sharma
Centre for Mathematical Plasma-Astrophysics, KU Leuven, Celestijnenlaan 200-B, 3001 Leuven, Belgium;
2 shared publications Adam S. Pagan
1 shared publication
Latest Publications
- 19 February 2026
- Published by Elsevier in Computer Physics Communications
- Vol. 323
BORAT-EM: High frequency electromagnetic solver for atmospheric entry blackout analysis
- 19 February 2026
- Published by Elsevier in Computer Physics Communications
- Vol. 323
BORAT-EM: High frequency electromagnetic solver for atmospheric entry blackout analysis
- Open Access
- 1 March 2024
- Published by AIP Publishing in Physics of Fluids
- Vol. 36 (3)
Influence of magnetohydrodynamics configuration on aerothermodynamics during Martian reentry
This paper investigates the role of magnetohydrodynamics (MHD) on the aerothermodynamics (ATD) of a representative entry vehicle while flying into the Martian atmosphere. By strategically placing a flight-ready superconducting magnet at varied positions in the Schiaparelli reentry capsule of the ExoMars mission, we discern its impact on essential flow properties. The primary consequence of MHD during atmospheric entry is the generation of the Lorentz force, which increases the shock standoff distance resulting in a reduction of the heat flux on the spacecraft by pushing high-energy plasma particles away. Through different magnet configurations, three distinct cases are formed to comprehensively understand the effects and implications of each setup. The study is performed using the COOLFluiD MHD for EnTries, an in-house ATD solver. For case 1, the magnet's placement behind the ExoMars forebody at the stagnation point reduces the heat flux. In case 2, the magnet's relocation to the shoulder region explores its potential to mitigate communication blackouts by influencing the wake region's flow. However, this positioning also induces shock bending, leading to variations in post-shock species mass fractions and heat flux spikes in the post-shock region. Case 3, involving an additional magnet where the shock bends in case 1, showcases a consistent increase in shock standoff distance across the forebody, providing a longer relaxation zone for species equilibration. Our findings highlight that while the strength of the applied magnetic field is crucial, the magnet's size is equally pivotal in determining ATD behavior. Case 3 emerges as the most promising configuration, consistently reducing heat flux across the forebody and maintaining it in the afterbody. This study underscores the potential of multi-magnet configurations as next-generation MHD heat shields for Martian atmospheric entry, emphasizing the criticality of magnet placement and configuration in enabling future MHD-enhanced deep space exploration missions.
- 1 March 2024
- Published by AIP Publishing in Physics of Fluids
- Vol. 36 (3)
Open AccessInfluence of magnetohydrodynamics configuration on aerothermodynamics during Martian reentry
This paper investigates the role of magnetohydrodynamics (MHD) on the aerothermodynamics (ATD) of a representative entry vehicle while flying into the Martian atmosphere. By strategically placing a flight-ready superconducting magnet at varied positions in the Schiaparelli reentry capsule of the ExoMars mission, we discern its impact on essential flow properties. The primary consequence of MHD during atmospheric entry is the generation of the Lorentz force, which increases the shock standoff distance resulting in a reduction of the heat flux on the spacecraft by pushing high-energy plasma particles away. Through different magnet configurations, three distinct cases are formed to comprehensively understand the effects and implications of each setup. The study is performed using the COOLFluiD MHD for EnTries, an in-house ATD solver. For case 1, the magnet's placement behind the ExoMars forebody at the stagnation point reduces the heat flux. In case 2, the magnet's relocation to the shoulder region explores its potential to mitigate communication blackouts by influencing the wake region's flow. However, this positioning also induces shock bending, leading to variations in post-shock species mass fractions and heat flux spikes in the post-shock region. Case 3, involving an additional magnet where the shock bends in case 1, showcases a consistent increase in shock standoff distance across the forebody, providing a longer relaxation zone for species equilibration. Our findings highlight that while the strength of the applied magnetic field is crucial, the magnet's size is equally pivotal in determining ATD behavior. Case 3 emerges as the most promising configuration, consistently reducing heat flux across the forebody and maintaining it in the afterbody. This study underscores the potential of multi-magnet configurations as next-generation MHD heat shields for Martian atmospheric entry, emphasizing the criticality of magnet placement and configuration in enabling future MHD-enhanced deep space exploration missions.
- Open Access
- 31 July 2023
- Published by Elsevier in Acta Astronautica
- Vol. 212, 408-423
Effect of electron number densities on the radio signal propagation in an inductively coupled plasma facility
- 31 July 2023
- Published by Elsevier in Acta Astronautica
- Vol. 212, 408-423
Open AccessEffect of electron number densities on the radio signal propagation in an inductively coupled plasma facility
- Open Access
- 22 November 2022
- Published by Elsevier in Journal of Space Safety Engineering
- Vol. 10 (1) , 27-34
A Magnetohydrodynamic enhanced entry system for space transportation: MEESST
- 22 November 2022
- Published by Elsevier in Journal of Space Safety Engineering
- Vol. 10 (1) , 27-34
Open AccessA Magnetohydrodynamic enhanced entry system for space transportation: MEESST