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

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

Author(s):

Otsu, H. ( Shizuoka University, Hamamatsu, Japan )
Abe, T. ( Japan Aerospace Exploration Agency, Sagamihara, Japan )
Konigorski, D. ( EADS Space Transportation, Bremen, Germany )

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Plasmadynamics and Lasers Conference

Ser. no.:

36th

Pub. Year:

2005

No.:

2005-5049

Paper no.:

AIAA Paper 2005-5049

Pub. info.:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200512 [CD-ROM 2005 Disc 12]

Type:

Technical Paper

Details

TDL ID:	ZA00001630
Series ID:	PA00000148
Conf. info. (Name):	AIAA Plasmadynamics and Lasers Conference
Conf. info. (Number):	36th
Conf. info. (Venue):	Toronto, Ontario, Canada
Conf. info. (Date):	2005.06.06-2005.06.09

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