Feasibility Study on the Flight Demonstration for a reentry vehicle with the Magnetic Flow Control System

Feasibility Study on the Flight Demonstration for a reentry vehicle with the Magnetic Flow Control System

著者名:

H. Otsu ( Shizuoka University, Hamamatsu, Japan )
A. Matsuda ( ISAS/JAXA, Sagamihara, Japan )
T. Abe
D. Konigorski ( EADS Space Transportation, Bremen, Germany )

掲載資料名:

AIAA meeting papers on disc

シリーズ名:

AIAA Paper : AIAA Plasmadynamics and Lasers Conference

シリーズ巻号:

2006

発行年:

2006

通号:

2006-3566

ペーパー番号:

AIAA Paper 2006-3566

出版情報:

Reston, Va: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200612 [CD-ROM 2006 Disc 12]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00047236
シリーズID:	PA00000148
会議名:	AIAA Plasmadynamics and Lasers Conference
回次:	37th
会議開催地:	San Francisco, California
会議開催年:	2006.06.05-2006.06.08

類似資料:

1 テクニカルペーパー Numerical Validation of the Magnetic Flow Control for Reentry Vehicles H. Otsu, A. Matsuda, T. Abe, D. Konigorski American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Experimental Investigation of the Hall Effect for the Interaction between the Weakly-ionized Plasma Flow and Magnetic Body A. Matsuda, M. Kawamura, Y. Takizawa, H. Otsu, D. Konigorski, S. Sato, T. Abe American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Application of the Magnetic Flow Control System for Aerobraking Flight of the Reentry Vehicle H. Otsu, T. Matsumuray, A. Nakamuraz, Y. Yamagiwax, T. Abe, H. Katsurayamak, D. Konigorski American Institute of Aeronautics and Astronautics	8 テクニカルペーパー Experimental Study on Drag Enhancement in Electrodynamic Heat Shield for a Blunt Body in a Weakly Ionized Plasma Flow M. Kawamura, A. Matsuda, H. Katsurayama, H. Otsu, D. Konigorski, S. Sato, T. Abe American Institute of Aeronautics and Astronautics
3 テクニカルペーパー Rarefied gas effects on the magnetic flow control system for aerobraking flight of the reentry vehicle Otsu, Hirotaka, Katsurayama, Hiroshi, Abe, Takashi, Konigorski, Detlev American Institute of Aeronautics and Astronautics	9 テクニカルペーパー Experiment on Shock Layer Enhancement by Electro-Magnetic Effect in Reentry-Related High-Enthalpy Flow Takizawa, Y., Matsuda, A., Sato, S., Abe, T., Konigorski, D. American Institute of Aeronautics and Astronautics
4 テクニカルペーパー Influence of the Hall Effect on the Electrodynamic Heat Shield System for Reentry Vehicles Otsu, H., Abe, T., Konigorski, D. American Institute of Aeronautics and Astronautics	10 国際会議録 Trajectory Analysis of the Reentry Vehicle with the Electromagnetic Flow Control H. Otsu, H. Katsurayama, D. Konigorski, T. Abe ESA Communications
5 テクニカルペーパー Expansion Tube Experiment of Applied Magnetic Field Effect on Reentry Plasma T. Tanifuji, A. Matsuda, K. Wasai, H. Otsu, H. Yamasaki, D. Konigorski, T. Abe American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Shock Layer enhancement by electro-magnetic effect for spherical blunt body A. Matsuda, K. Wakatsuki, Y. Takizawa, M. Kawamura, H. Otsu, D. Konigorski, S. Sato, T. Abe American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Numerical Study of the Electromagnetic Control of a Weakly Ionized Flow Around a Blunt Body: Role of a Insulative Boundary in the Flow H. Katsurayama, T. Abe, H. Otsu, D. Konigorski American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Experimental Investigation of Electrodynamic Heatshield Effect in a Reentry Plasma T. Tanifuji, K. Wasai, H. Makino, H. Otsu, M. Furudate, H. Yamasaki, D. konigorski, T. Abe American Institute of Aeronautics and Astronautics

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