Comparison of Directly and Inductively Coupled Pulsed Electromagnetic Thrusters

Comparison of Directly and Inductively Coupled Pulsed Electromagnetic Thrusters

Author(s):

Cassibry, J. ( University of Alabama in Huntsville, Huntsville, AL )
Wu, S.

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Plasmadynamics and Lasers Conference

Ser. no.:

36th

Pub. Year:

2005

No.:

2005-4664

Paper no.:

AIAA Paper 2005-4664

Pub. info.:

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

ISSN:

10877215

Language:

English

Call no.:

A07400/200512 [CD-ROM 2005 Disc 12]

Type:

Technical Paper

Details

TDL ID:	ZA00001630
Series ID:	PA00000148
Conf. info. (Name):	AIAA Plasmadynamics and Lasers Conference
Conf. info. (Number):	36th
Conf. info. (Venue):	Toronto, Ontario, Canada
Conf. info. (Date):	2005.06.06-2005.06.09

Similar Items:

1 Technical Paper 2-D Magnetohydrodynamic modeling of a Pulsed Plasma Thruster. Thio, Y.C.F., Cassibry, J.T., Wu, S.T. American Institute of Aeronautics and Astronautics	7 Technical Paper Design of a High-energy, Two-stage Pulsed Plasma Thruster. Markusic, T.E., Thio, Y.C.F., Cassibry, J.T. American Institute of Aeronautics and Astronautics
2 Technical Paper Effects of Equation of State and Transport on the Modeling of Pulsed Plasma Accelerators Cassibry, J., Markusic, T., Wu, S. American Institute of Aeronautics and Astronautics	8 Technical Paper An Experimental Study of a Pulsed Electromagnetic Plasma Accelerator. Francis, Y.C., Eskridge, R., Lee, M., Smith, J., Cassibry, J.T. American Institute of Aeronautics and Astronautics
3 Technical Paper Effects of Propellant Injection, Material and Electrode Geometry on the Performance of a Two-Stage Pulsed Plasma Accelerator Cassibry, J., Markusic, T., Wu, S. American Institute of Aeronautics and Astronautics	9 Technical Paper Numerical Modeling of a Low Energy Pulsed Inductive Thruster P. Mikellides, J. Villarreal American Institute of Aeronautics and Astronautics
4 Technical Paper Sub-Alfvenic Inlet Boundary Conditions for Axisymmetric MHD Nozzles J. Cassibry, S. Wu American Institute of Aeronautics and Astronautics	10 Technical Paper Design of an inductively-driven pulsed plasma thruster Turchi, P.J., Leiweke, R.J., Kamhawi, H. American Institute of Aeronautics and Astronautics
5 Technical Paper Pulsed Inductive Drive for Space Applications Tracy, P., Burch, J., Zhang, T., Wu, S. American Institute of Aeronautics and Astronautics	11 Technical Paper The PIT Mark VI Pulsed Inductive Thruster Russell, D., Jackson, B., Dailey, C., Goldstein, W., Lovberg, R., Poylio, J. American Institute of Aeronautics and Astronautics
6 Technical Paper Computational Analysis of a Pulsed Inductive Thruster D. Li, J. Corpening, I. Hrbud, C. Merkle American Institute of Aeronautics and Astronautics	12 Technical Paper Numerical Modeling Studies of Plasma Driven Magnetoinertial Fusion J. Cassibry, C. Knapp, R. Kirkpatrick, S. Wu American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12