Optimization of Geometric Parameters of Cryogenic Liquid Rocket Combustion Chambers

Optimization of Geometric Parameters of Cryogenic Liquid Rocket Combustion Chambers

Author(s):

Publication title:

AIAA paper

Title of ser.:

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

Ser. no.:

2001

Pub. Year:

2001

No.:

2001-3408

Paper no.:

AIAA-2001-3408

Page(from):

1

Page(to):

11

Pages:

11

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050826
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC) & Exhibit
Conf. info. (Number):	37th
Conf. info. (Venue):	Salt Lake City, UT
Conf. info. (Date):	2001.07.08-2001.07.11
Note for article:	37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit July 8-11, 2001/Salt Lake City, Utah

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