EP53C-1041
MarsCAT: Mars Array of ionospheric Research Satellites using the CubeSat Ambipolar Thruster
Friday, 18 December 2015
Poster Hall (Moscone South)
Edgar A Bering III1, Lawrence Pinsky1, Liming Li2, David R Jackson1, Ji Chen1, Helen Reed3, Mark Moldwin4, Justin Christophe Kasper4, J. P. Sheehan4, James Forbes4, Thomas Heine4, Anthony W Case5, Michael Louis Stevens5 and David G Sibeck6, (1)University of Houston, Houston, TX, United States, (2)University of Houston, Department of Physics, Houston, TX, United States, (3)Texas A & M University College Station, College Station, TX, United States, (4)University of Michigan Ann Arbor, Ann Arbor, MI, United States, (5)Smithsonian Astrophysical Observatory, Cambridge, MA, United States, (6)NASA/GSFC, Greenbelt, MD, United States
Abstract:
The MarsCAT (Mars Array of ionospheric Research Satellites using the CubeSat Ambipolar Thruster) Mission is a two 6U CubeSat mission to study the ionosphere of Mars proposed for the NASA SIMPLeX opportunity. The mission will investigate the plasma and magnetic structure of the Martian ionosphere, including transient plasma structures, magnetic field structure and dynamics, and energetic particle activity. The transit plan calls for a piggy back ride with Mars 2020 using a CAT burn for MOI, the first demonstration of CubeSat propulsion for interplanetary travel. MarsCAT will make correlated multipoint studies of the ionosphere and magnetic field of Mars. Specifically, the two spacecraft will make in situ observations of the plasma density, temperature, and convection in the ionosphere of Mars. They will also make total electron content measurements along the line of sight between the two spacecraft and simultaneous 3-axis local magnetic field measurements in two locations. Additionally, MarsCAT will demonstrate the performance of new CubeSat telemetry antennas designed at the University of Houston that are designed to be low profile, rugged, and with a higher gain than conventional monopole (whip) antennas. The two MarsCAT CubeSats will have five science instruments: a 3-axis DC magnetometer, adouble-Langmuir probe, a Faraday cup, a solid state energetic particle detector (Science Enhancement Option), and interspacecraft total electron content radio occulation experiment. The MarsCAT spacecraft will be solar powered and equipped with a CAT thruster that can provide up to 4.8 km/s of delta-V, which is sufficient to achieve Mars orbit using the Mars 2020 piggyback. They have an active attitude control system, using a sun sensor and flight-proven star tracker for determination, and momentum wheels for 3-axis attitude control.
