Impact of Lift Force by Electromagnetic Flow Control on the Reentry Trajectory-Reference-Cited by-同舟云学术

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Impact of Lift Force by Electromagnetic Flow Control on the Reentry Trajectory

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Plasmadynamics and Lasers Conference
language:
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Author:

Otsu Hirotaka¹,Katsurayama Hiroshi²,Konigorski Detlev³,Abe Takashi⁴

Affiliation:

1. Ryukoku University

2. Yamaguchi University

3. EADS

4. Japan Aerospace Exploration Agency (JAXA)

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3466

Reference16 articles.

1. Influence of Hall Effect on Electrodynamic Heat Shield System for Reentry Vehicles

2. Numerical Validation of the Magnetic Flow Control for Reentry Vehicles

3. Experiment on Shock Layer Enhancement by Electro-Magnetic Effect in Reentry-Related High-Enthalpy Flow

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. New Magnetic Field Setup for Electromagnetic Flow Control of Lifting Reentry Vehicle;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2018

2. Numerical Simulation of Mars Entry Flight using Magnetohydrodynamic Parachute Effect;47th AIAA Plasmadynamics and Lasers Conference;2016-06-10

3. Numerical Study of Magnetohydrodynamic Flow Control Along Superorbital Reentry Trajectories;Journal of Spacecraft and Rockets;2016-05

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