The University of Michigan
Department of Aerospace Engineering
| Plasmadynamics & Electric Propulsion Laboratory |
PEPL Thrusters: BHT600 Cluster

Above: BHT600 cluster on display before testing and shipment to PEPL; US quarter included to indicate scale (pink caps are covering the cathodes).

Above: Nominal discharge, in PEPL's LVTF, of the full cluster: 4 thrusters each discharge settings of at 300 V, 2 A, and 2.5 mg-Xe/s.

Above: Initial discharge of the full 4x BHT-600 cluster in PEPL's LVTF (April 2005).

All rights reserved, copyright ©
Page Last Modified: Saturday, 23-Jan-2016 01:04:19 EST
PEPL is part of the University of Michigan, Department of Aerospace Engineering.
Feedback and questions about PEPL and this web site may be directed to the laboratory director, webmaster, or the laboratory land line, (734)764-4199.