Heat Transfer Mitigation Along Superorbital Reentry Trajectories Using Magnetohydrodynamic Aerobraking
Author:
Affiliation:
1. The University of Queensland
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-3649
Reference28 articles.
1. DSMC Simulation of Electrodynamic Aerobraking on a Reentry Capsule in a Hypersonic Rarefied Regime
2. Magnetohydrodynamic-Hypersonic Flow Past a Blunt Body
3. Porter, R. W. “Theoretical Aspects of Blunt Body Magnetoaerodynamics,” Ph.D. thesis,Northwestern University, 1966.
4. Hypersonic magnetohydrodynamics with or without a blunt body
5. Simplified magnetoaerodynamic flow relations for axisymmetric blunt bodies.
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2. Optimised Magnetic Field Strengths for Venus Atmospheric Entry using Magnetohydrodynamic Aerobraking;AIAA SCITECH 2023 Forum;2023-01-19
3. Feasibility of MHD Aerobraking for Use in Martian Atmospheric Entry;AIAA SCITECH 2023 Forum;2023-01-19
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