Development of a high temperature combustor for HYPR Mach 3 turbojet engines

Development of a high temperature combustor for HYPR Mach 3 turbojet engines

Author(s):

Kawano, M. ( Jet Engine Division, Kawasaki Heavy Industries, Ltd., Japan )
Kuyama, T. ( Jet Engine Division, Kawasaki Heavy Industries, Ltd., Japan )
Kobayashi, M. ( Jet Engine Division, Kawasaki Heavy Industries, Ltd., Japan )
Ogata, H. ( Jet Engine Division, Kawasaki Heavy Industries, Ltd., Japan )

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Ser. no.:

1998

Pub. Year:

1998

No.:

98-3281

Paper no.:

98-3281

Page(from):

1

Page(to):

10

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050858
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	34th
Conf. info. (Venue):	Cleveland, OH
Conf. info. (Date):	1998.07.13-1998.07.15
Note for article:	34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July 13-15, 1998/Cleveland, OH

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