Preliminary Design Optimization For A Supersonic Turbine For Rocket Propulsion

Preliminary Design Optimization For A Supersonic Turbine For Rocket Propulsion

Author(s):

Publication title:

AIAA paper

Title of ser.:

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

Ser. no.:

2000

Pub. Year:

2000

No.:

2000-3242

Paper no.:

00-3242

Page(from):

1

Page(to):

20

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050879
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	36th
Conf. info. (Venue):	Huntsville, AL
Conf. info. (Date):	2000.07.16-2000.07.19
Note for article:	36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 16-19 July 2000 / Huntsville, Alabama

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