Chemical processing of the dusty, low-pressure Martian atmosphere typically requires conditioning and compression of the gases as first steps. A temperature-swing adsorption process can perform these tasks using nearly solid-state hardware and with relatively low power consumption compared to alternative processes. In addition, the process can separate the atmospheric constituents, producing both pressurized CO2 and a buffer gas mixture of nitrogen and argon. To date we have developed and tested adsorption compressors at scales appropriate for the near-term robotic missions that will lead the way to ISRU-based human exploration missions. In this talk we describe the characteristics, testing, and performance of these devices. We also discuss scale-up issues associated with meeting the processing demands of sample return and human missions.
[1]
Christopher P. McKay,et al.
Martian Atmospheric Utilization by Temperature-Swing Adsorption
,
1996
.
[2]
Lila M. Mulloth,et al.
A Solid-State Compressor for Integration of CO 2 Removal and Reduction Assemblies
,
2000
.
[3]
T. R. Meyer,et al.
The atmosphere of Mars - Resources for the exploration and settlement of Mars
,
1984
.
[4]
D. R. Rushneck,et al.
The composition of the atmosphere at the surface of Mars
,
1977
.
[5]
Robert L. Ash,et al.
Feasibility of rocket propellant production on Mars
,
1978
.
[6]
Christopher P. McKay,et al.
Utilizing Martian Resources for Life Support
,
1993
.