Application of the Magnetic Flow Control System for Aerobraking Flight of the Reentry Vehicle-Reference-Cited by-同舟云学术

Application of the Magnetic Flow Control System for Aerobraking Flight of the Reentry Vehicle

Published:2008-06-15 Issue: Volume: Page:
ISSN:
Container-title:39th Plasmadynamics and Lasers Conference
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Author:

Otsu Hirotaka¹,Nakamura Akiko¹,Matsumura Takeo¹,Yamagiwa Yoshiki¹,Abe Takashi²,Konigorski Detlev³

Affiliation:

1. Shizuoka University

2. Japan Aerospace Exploration Agency

3. EADS Space Transportation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-3897

Reference6 articles.

1. 1Otsu,H.,Abe,T.,andKonigorski,D."InfluenceoftheHallEffectontheElectrodynamicHeatShieldSystem forReentry Vehicles," AIAApaper2005-5049,June2005.

2. 2Hirotaka Otsu, Atsushi Matsuda, Takashi Abe, and Detlev Konigorski, "Numerical Validation of the Magnetic Flow ControlforReentryVehicles,"AIAA2006-3236,June2006.

3. 3HirotakaOtsu,AtsushiMatsuda,TakashiAbe,andDetlevKonigorski,"FeasibilityStudyontheFlightDemonstrationforareentryvehicle withtheMagneticFlowControlSystem,"AIAA2006-3566,June2006.

4. 4Takizawa, Y., Matsuda, A., Sato, S., Abe, T., and Konigorski, D. "Experiment on Shock Layer Enhancement by Electro-MagneticEffectinReentry-RelatedHigh-EnthalpyFlow,"AIAApaper2005-4786,June2005.

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1. Magnetic-Field Configuration Effect on Aerodynamic Heating of a Magnetized Body;Journal of Spacecraft and Rockets;2012-03

2. Impact of Lift Force by Electromagnetic Flow Control on the Reentry Trajectory;42nd AIAA Plasmadynamics and Lasers Conference;2011-06-14