A solar electric propulsion Hall Effect thruster being tested under vacuum conditions at NASA. Credit: NASA
Plasma-based rocket designed for deep space exploration lasts longer and generates high power.
The increased interest in deep-space travel has necessitated the development of powerful, long-lasting rocket systems to propel spacecraft into the cosmos. Scientists at the U.S. Department of Energy’s (DOE) Princeton Plasma Physics Laboratory (PPPL) have created a small modified version of a plasma-based propulsion system known as a Hall thruster that both enhances the lifespan of the rocket and produces high power.
The plasma-powered miniature device is less than an inch in diameter and removes the walls surrounding the plasma propellant to create innovative thruster configurations. Plasma is a state of matter composed of free-floating electrons and atomic nuclei, or ions. Among these innovations are the cylindrical Hall thruster, which was initially conceived and researched at PPPL, and a completely wall-less Hall thruster. Both configurations decrease channel erosion generated by plasma-wall interactions, which limits thruster lifespan – a major issue for typical annular or ring-shaped Hall thrusters and particularly for miniaturized low-power thrusters used on small satellites.
Widely studied
Cylindrical Hall thrusters were invented by PPPL physicists Yevgeny Raitses and Nat Fisch in 1999 and have been studied with students on the Laboratory’s Hall Thruster Experiment (HTX) since then. The PPPL devices have also been studied in countries including Korea, Japan, China, Singapore, and the European Union, with Korea and Singapore considering plans to fly them.
While wall-less Hall thrusters can minimize channel erosion, they face the problem of extensive widening, or divergence, of the plasma thrust plume, which degrades the system’s performance. To reduce this problem, PPPL has installed a key innovation on its new wall-less system in the form of a segmented electrode, a concentrically joined carrier of current. This innovation not only reduces the divergence and helps to intensify the rocket thrust, Raitses said, but also, suppresses the hiccups of small-size Hall thruster plasmas that interrupt the smooth delivery of power.
Graduate student Jacob Simmonds, center, with advisors Masaaki Yamada, left, and Yevgeny Raitses with figure of wall-less Hall thruster behind them. Credit: Yamada and Raitses photos by Elle Starkman/Office of Communications; Simmonds photo by Tyler Boothe. Collage by Kiran Sudarsanan.
The new findings cap a series of papers that Jacob Simmonds, a graduate student in the Princeton University Department of Mechanical and Aerospace Engineering, has published with Raitses, his doctoral co-adviser; PPPL physicist Masaaki Yamada serves as the other co-advisor. “In the last two years we have published three papers on new physics of plasma thrusters that led to the dynamic thruster described in this one,” said Raitses, who leads PPPL research on low-temperature plasma physics and the HTX. “It describes a novel effect that promises new developments in this field.”
Application of segmented electrodes to Hall thrusters is not new. Raitses and Fisch had previously used such electrodes to control the plasma flow in conventional annular Hall thrusters. But the effect that Simmonds measured and described in the recent paper in Applied Physics Letters is much stronger and has greater impact on the overall thruster operation and performance.
Focusing the plume
The new device helps overcome the problem for wall-less Hall thrusters that allows the plasma propellant to shoot from the rocket at wide angles, contributing little to the rocket’s thrust. “In short, wall-less Hall thrusters while promising have an unfocused plume because of the lack of channel walls,” Simmonds said. “So we needed to figure out a way to focus the plume to increase the thrust and efficiency and make it a better overall thruster for spacecraft.”
The segmented electrode diverts some electric current away from the thruster’s high-voltage standard electrode to shape the plasma and narrow and improve the focus of the plume. The electrode creates this effect by changing the directions of the forces within the plasma, particularly those on the ionized xenon plasma that the system accelerates to propel the rocket. Ionization turned the xenon gas the process used into free-standing electrons and atomic nuclei, or ions.
These developments increased the density of the thrust by shaping more of it in a reduced volume, a key goal for Hall thrusters. An added benefit of the segmented electrode has been the reduction of plasma instabilities called breathing mode oscillations, “where the amount of plasma increases and decreases periodically as the ionization rate changes with time” Simmonds said. Surprisingly, he added, the segmented electrode caused these oscillations to go away. “Segmented electrodes are very useful for Hall thrusters for these reasons,” he said.
The new high-thrust-density rocket can be especially beneficial for tiny cubic satellites, or CubeSats. Masaaki Yamada, Simmonds’ co-doctoral adviser who heads the Magnetic Reconnection Experiment (MRX) that studies the process behind solar flares, Northern lights and other space phenomena, proposed the use of a wall-less segmented electrode system to power a CubeSat. Simmonds and his team of undergraduate students working under the guidance of Prof. Daniel Marlow, the Evans Crawford 1911 Professor of Physics at Princeton, took up that proposal to develop a CubeSat and such a rocket — a project that was halted near completion by the COVID-19 pandemic and that could be resumed in the future.
