Co-sponsored by: MIPSE

NASA is preparing to demonstrate high‐power electric propulsion on the Power and Propulsion Element (PPE), the first element of a human‐operated Gateway station that will orbit the Moon. The Hall thrusters (HTs) being flown on the PPE will operate at three times the power of current state‐of‐the‐art HTs and utilize magnetic shielding, which greatly increase the wear life of the thrusters. Associated with these advances in technical capability are uncertainties regarding the plasma properties of the exhaust plume, particularly the low density plume exiting sideways from the thrusters. To better predict the erosive power of the plasma plume and how the plume might interact with the PPE and future spacecraft, NASA is flying the Plasma Diagnostics Package (PDP). The PDP data will refine plasma models for predicting the behavior of high‐power HT systems on future missions. This presentation will describe a brief history of the PDP project, basic Hall thruster plume physics, the plasma physics behind the PDP sensor design, and current status of the PDP project.

Speaker(s): Dr. Wensheng Huang,

Location:
Room: 1005
Bldg: EECS
1301 Beal Ave
Ann Arbor, Michigan
48109