Dust Removal Technolgy for a Mars In Situ Resource Utilization SystemSeveral In Situ Resource Utilization (lSRU) systems being considered to enable future manned exploration of Mars require capture of Martian atmospheric gas to extract oxygen and other commodities. However, the Martian atmosphere contains relatively large amounts of dust which must be removed in tbe collection systems of the ISRU chambers. The amount of atmospheric dust varies largely with the presence of daily dust devils and the less frequent but much more powerful global dust storms. A common and mature dust removal technology for terrestrial systems is the electrostatic precipitator. With this technology, dust particles being captured are imparted an electrostatic charge by means of a corona discharge. Charged dust particles are then driven to a region of high electric field which forces the particles onto a collector for capture. Several difficulties appear when this technology is adapted to the Martian atmospheric environment At the low atmospheric pressure of Mars, electrical breakdown occurs at much lower voltages than on Earth and corona discharge is difficult to sustain. In this paper, we report on our efforts to obtain a steady corona/glow discharge in a simulated Martian atmosphere of carbon dioxide at 9 millibars of pressure. We also present results on the design of a dust capture system under these atmospheric conditions.
Document ID
20110016184
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Calle, C. I. (NASA Kennedy Space Center Cocoa Beach, FL, United States)
Johansen, M. R. (NASA Kennedy Space Center Cocoa Beach, FL, United States)
Williams, B. S. (University of Southern Alabama Mobile, AL, United States)
Hogue, M. D. (NASA Kennedy Space Center Cocoa Beach, FL, United States)
Mackey, P. J. (NASA Kennedy Space Center Cocoa Beach, FL, United States)
Clements, J. S. (Appalachian State Univ. Boone, NC, United States)