Electrodeless Magnetohydrodynamic Local Force Generator for Aerocapture

Research output: Contribution to journalArticlepeer-review

1 Scopus citations

Abstract

This paper presents a novel magnetohydrodynamics (MHD) system for planetary entry aerocapture. The following two features provide the system an advantage over earlier methods: i) it can be deployed locally to one or various flow regions, and ii) it does not make use of electrodes. Previous MHD systems for planetary entry were either electrodeless global systems or two-electrode local systems. The proposed novel MHD system employs two magnets to establish a current loop, resulting in a Faraday electromotive force. The first magnet is positioned to ensure that the magnetic field faces outward from the shell, while the second magnet is oriented to ensure that the magnetic field faces inward toward the shell. Preliminary findings demonstrate that when located on the surface of an Earth-entry capsule at a flight Mach number of 35, the novel electrodeless MHD system can generate forces several times greater than a two-electrode system while utilizing the same magnetic field strength. The study is conducted entirely through numerical simulation using Computational Fluid Dynamics, Waves, Reactions, Plasmas (CFDWARP), a computational fluid dynamics code that employs advanced numerical methods allowing for the full coupling between aerodynamics, magnetohydrodynamics, and non-neutral plasma sheaths. The physical model includes an 11-species finite-rate chemical solver, including real gas effects, and the drift-diffusion model for all charged species, along with an electric field potential equation that satisfies Gauss’s law.

Original languageEnglish (US)
Pages (from-to)3035-3047
Number of pages13
JournalAIAA journal
Volume63
Issue number8
DOIs
StatePublished - Aug 1 2025

Keywords

  • Aerobraking and Aerocapture
  • Aerodynamics
  • Computational Fluid Dynamics
  • Descent and Landing
  • Entry
  • Magnetic Field Strength
  • Magnetohydrodynamics
  • Non Neutral Plasmas

ASJC Scopus subject areas

  • Aerospace Engineering

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