Fundamental Studies of the Electrode Regions in Arcjet Thrusters
Abstract
This research focuses on the understanding of the plasma dynamics in the near node and near-cathode region of arcjets with an emphasis on the development of an extensive database for the validation of arcjet models. During the first year of this research period, the arc cathode interaction was investigated by in-situ spectroscopic imaging and by axial emission spectroscopy, providing measurements of cathode current density, cathode temperature, and near-cathode plasma properties. In addition, during this grant period, we have extended the use of Laser Induced Fluorescence (LIF) to make measurements of plasma properties within the expanding region of the nozzle and have accumulated an extended data base that includes, in addition to the use of pure hydrogen propellant, mixtures of hydrogen and nitrogen to simulate hydrazine decomposition products. In the final year, a new laser based diastic, Doppler-Free Absorption Spectroscopy (DFAS) was developed and applied to measure the exit plane electron number density in a hydrogen arcjet, one of the last properties needed to provide closure to the vast data set that we have generated for low power hydrogen arcjet. As a spin-off to this grant, the LIF diagnostics that was developed for arcjet through this program was extended to the study xenon plasmas, and implemented to measure both neutral and ionized on velocities at the exit of a Hall thruster. This contributed to a comprehensive study of the near exit region of our Hall discharge device. To compliment the LIF diagnostics on our Hall thrusters, we have made extensive measurements of the transient and time average plasma properties using conventional electrostatic probes.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1998
- Accession Number
- ADA342673
Entities
People
- Mark Cappelli
Organizations
- Stanford University