Optimization of CubeSat System-Level Design and Propulsion Systems for Earth-Escape Missions

Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140416/1/1.A33136.pd

Computational Studies of Magnetic Nozzle Performance

An extensive literature review of magnetic nozzle research has been performed, examining previous work, as well as a review of fundamental principles. This has allow us to catalog all basic physical mechanisms which we believe underlie the thrust generation process. Energy conversion mechanisms include the approximate conservation of the magnetic moment adiabatic invariant, generalized hall and thermoelectric acceleration, swirl acceleration, thermal energy transformation into directed kinetic energy, and Joule heating. Momentum transfer results from the interaction of the applied magnetic field with currents induced in the plasma plume., while plasma detachment mechanisms include resistive diffusion, recombination and charge exchange collisions, magnetic reconnection, loss of adiabaticity, inertial forces, current closure, and self-field detachment. We have performed a preliminary study of Hall effects on magnetic nozzle jets with weak guiding magnetic fields and weak expansions (p(sub jet) approx. = P(sub background)). The conclusion from this study is that the Hall effect creates an azimuthal rotation of the plasma jet and, more generally, creates helical structures in the induced current, velocity field, and magnetic fields. We have studied plasma jet expansion to near vacuum without a guiding magnetic field, and are presently including a guiding magnetic field using a resistive MHD solver. This research is progressing toward the implementation of a full generalized Ohm's law solver. In our paper, we will summarize the basic principle, as well as the literature survey and briefly review our previous results. Our most recent results at the time of submittal will also be included. Efforts are currently underway to construct an experiment at the University of Michigan Plasmadynamics and Electric Propulsion Laboratory (PEPL) to study magnetic nozzle physics for a RF-thruster. Our computational study will work directly with this experiment to validate the numerical model, in order to study magnetic nozzle physics and optimize magnetic nozzle design. Preliminary results from the PEPL experiment will also be presented

Mode Transitions in Hall Effect Thrusters

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/106480/1/AIAA2013-4116.pd

Hall Thruster and VASIMR VX-100 Force measurements using a Plasma Momentum Flux Sensor

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76509/1/AIAA-2009-246-125.pd

Validating A Plasma Momentum Flux Sensor Against an Inverted Pendulum Thrust Stand

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76115/1/AIAA-2008-4739-514.pd

ISS Space Plasma Laboratory: An ISS instrument package for investigating the opening/closing of solar and heliospheric magnetic fields

Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140428/1/6.2014-1422.pd

Improved Efficiency and Throttling Range of the VX-200 Magnetoplasma Thruster

Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140438/1/1.b34801.pd

Validating a Plasma Momentum Flux Sensor to an Inverted Pendulum Thrust Stand

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76451/1/AIAA-35706-298.pd