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

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

著者名:

H. Otsu ( Shizuoka University, Hamamatsu, Shizuoka, Japan )

T. Matsumuray

A. Nakamuraz

Y. Yamagiwax

T. Abe ( Institute of Space and Astronautical Science, Sagamihara, Kanagawa, Japan )

H. Katsurayamak

D. Konigorski ( EADS Space Transportation, Bremen, Germany )

さらに 2 件

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:

2008

発行年:

2008

通号:

2008-3897

ペーパー番号:

AIAA Paper 2008-3897

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200807 [CD-ROM 2008 Disc 7]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00050894
シリーズID:	PA00000148
会議名:	Plasmadynamics and Lasers Conference
回次:	39th
会議開催地:	Seattle, WA
会議開催年:	2008.06.23-2008.06.26
論文注記:	39th Plasmadynamics and Lasers Conference, 23-26 June 2008, Seattle, Washington

類似資料:

1 テクニカルペーパー Feasibility Study on the Flight Demonstration for a reentry vehicle with the Magnetic Flow Control System H. Otsu, A. Matsuda, T. Abe, D. Konigorski American Institute of Aeronautics and Astronautics	7 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
2 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	8 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
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 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
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 テクニカルペーパー Electro-Magnetic Effect on Shock Layer Structure in Reentry-Related High-Enthalpy Flow Takizawa, Y., Sato, S., Abe, T., Konigorski, D. American Institute of Aeronautics and Astronautics
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 Reentry Environment Advanced Diagnostics (READ) Flight Experiment on USERS Reentry Vehicle Abe,T., Fujita,K., Otsu,H., Hama,K., Shingu,S., Ichizono,K. American Institute of Aeronautics and Astronautics
6 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	12 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

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