Thruster
End-Hall Thruster
The End-Hall Thruster on display.
Developed
1994
Tested at PEPL
1994
Developer
NASA LeRC (now GRC)
The 500-W end-Hall thruster, developed at NASA Lewis Research Center (now GRC) was studied at PEPL as an alternative to the closed-drift thruster (CDT) that gained popularity due Russian research showing excellent CDT performance. This thruster does not have a center pole , thus eliminating an entire surface that can be eroded away. However, efficiency was found to be lower than similar CDT devices.
Selected Publications
Performance of the H9 Magnetically Shielded Hall Thrusters
Cusson, S. E., Hofer, R. R., Lobbia, R. B., Jorns, B. A., and Gallimore, A. D.
The H9 Magnetically Shielded Hall Thruster
Hofer, R.R., Cusson, S.E., Lobbia, R.B., and Gallimore, A.D.
Dispersion relation measurements of plasma modes in the near-field plume of a 9-kW magnetically shielded thruster
Brown, Z. A., and Jorns, B. A.
Experimental Evidence for Ion Acoustic Solitons in the Plume of a Hollow Cathode
Georgin, M.P., Jorns, B.A., and Gallimore, A.D.
Ion Acoustic Turbulence in the Hollow Cathode Plume of a Hall Effect Thruster
Cusson, S.E., Brown., Z, Dale, E.T., Jorns, B.A., and Gallimore, A.D.
Non-Invasive Characterization of the Ionization Region of a Hall Effect Thruster
Dale, E.T. and Jorns, B.A.
Spatial Evolution of Plasma Waves in the Near-field of a Magnetically Shielded Hall Thruster
Brown, Z. and Jorns, B.A.