Optimal Design of Hybrid Motor for the First Stage of Air Launch Vehicle

Optimal Design of Hybrid Motor for the First Stage of Air Launch Vehicle

Author(s):

Publication title:

AIAA paper

Title of ser.:

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

Ser. no.:

2003

Pub. Year:

2003

No.:

2003-4749

Paper no.:

2003-4749

Pages:

9

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00001711
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	39th
Conf. info. (Venue):	Huntsville, AL
Conf. info. (Date):	2003.06.20-2003.06.23
Note for article:	39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, AL, 20-23 June 2003

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