The Pulse Detonation Rocket Induced MHD Ejector (PDRIME) Concept

The Pulse Detonation Rocket Induced MHD Ejector (PDRIME) Concept

Author(s):

J. Cambier ( U.S. Air Force Research Laboratory, Edwards AFB, CA )
T. Roth ( UCLA, Los Angeles, CA )
C. Zeineh
A. Karagozian

Publication title:

AIAA meeting papers on disc

Title of ser.:

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

Ser. no.:

2008

Pub. Year:

2008

No.:

2008-4688

Paper no.:

AIAA 2008-4688

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200808 [CD-ROM 2008 Disc 8]

Type:

Technical Paper

Details

TDL ID:	ZA00050885
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Conf. info. (Number):	44th
Conf. info. (Venue):	Hartford, CT
Conf. info. (Date):	2008.07.21-2008.07.23
Note for article:	44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT, 21-23 July 2008

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