Mass flux and current density distributions of electrospray plumes
Abstract
Performance and lifetime analysis of electrospray thrusters requires accurate knowledge of the mass and charge distributions of the plume. Mass flux and current density distributions were measured for a single capillary electrospray emitter using EMI-Im and found to be substantially different across a wide range of flow rates and emission voltages. Mass flux measurements yield an n∼3 super-Gaussian profile across all flow rates and voltages, while current density measurements change shape from n∼1.5–2.5 super-Gaussian profiles monotonically with decreasing flow rate, where n=1 is Gaussian and higher n values correspond to increasingly more flat-top “super-Gaussian” profiles with steeper drop-off toward higher angles. For increasing flow rate, the mass flux profile grows while maintaining its shape, whereas the current density profile exhibits higher kurtosis, i.e., plumes that distribute proportionately more charge to higher angles. Additionally, higher extraction voltages exhibited tilted emission that led to highly off-axis plumes, ∼10°, for both mass flux and current density. Lifetime and performance assessments of electrospray thrusters must consider that mass flux and current density in the plume display different distribution shapes and trends in shape across changes in extraction voltage and flow rate.
Document Details
- Document Type
- Pub Defense Publication
- Publication Date
- Sep 08, 2021
- Source ID
- 10.1063/5.0056761
Entities
People
- Adam L Collins
- Anirudh Thuppul
- Nolan Uchizono
- Peter L. Wright
- Richard E. Wirz
Organizations
- Air Force Office of Scientific Research
- Air Force Research Laboratory
- Jet Propulsion Laboratory
- National Aeronautics and Space Administration
- University of California, Los Angeles