Effects of Propellant Injection, Material and Electrode Geometry on the Performance of a Two-Stage Pulsed Plasma Accelerator

Effects of Propellant Injection, Material and Electrode Geometry on the Performance of a Two-Stage Pulsed Plasma Accelerator

Author(s):

Cassibry, J. ( University of Alabama in Huntsville, Huntsville, AL )
Markusic, T. ( NASA Marshall Space Flight Center, Huntsville, AL )
Wu, S. ( University of Alabama-Huntsville, Huntsville, AL )

Publication title:

AIAA meeting papers on disc

Title of ser.:

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

Ser. no.:

40th

Pub. Year:

2004

No.:

2004-3641

Paper no.:

AIAA Paper 2004-3641

Pub. info.:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200412 [CD-ROM 2004 Disc 12]

Type:

Technical Paper

Details

TDL ID:	ZA00001611
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	40th
Conf. info. (Venue):	Fort Lauderdale, Florida
Conf. info. (Date):	2004.07.11-2004.07.14

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