Hypersonic Turbojet Engine Design of a Balloon-Based Flight Testing Vehicle

Hypersonic Turbojet Engine Design of a Balloon-Based Flight Testing Vehicle

Author(s):

H. Kobayashi ( Japan Aerospace Exploration Agency, JAXA, Chofu, Tokyo, Japan )

T. Sato ( Waseda University, Shinjuku, Chofu, Tokyo, Japan )

2 more

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : International Space Planes and Hypersonic Systems and Technologies Conference

Ser. no.:

2008

Pub. Year:

2008

No.:

2008-2620

Paper no.:

AIAA Paper 2008-2620

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200804 [CD-ROM 2008 Disc 4]

Type:

Technical Paper

Details

TDL ID:	ZA00049522
Series ID:	PA00000152
Conf. info. (Name):	AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Conf. info. (Number):	15th
Conf. info. (Venue):	Dayton, OH
Conf. info. (Date):	2008.04.28-2008.05.01
Note for article:	15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 28 April - 1 May 2008, Dayton, Ohio

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