SBIR/STTR Research Award

Lunar Oxygen and Silicon Beneficiation Using Only Solar Power

Award identifier e6d8b30e573f363f33379c94fe773a594e9cdc67ca04dc8fcf72545ea926dedbAwarding agency National Aeronautics and Space Administration

Award amount

$99,998

Program and phase

SBIR · Phase I

Award year

2007

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Packer Engineering
Proposal award date
2007-01-19
Contract end date
2007-07-23
UEI
Not reported
Solicitation number
Not reported
Topic code
X4.02

Research abstract

Element beneficiation from a moving, ionized plasma can be accomplished through the principles of mass spectroscopy. Two US patents were recently awarded to the PI on a means to separate all isotopes of regolith in a single pass using either a continuous or pulsed operation. This method of in-situ resource utilization has been studied at a system level, and results published at a national space conference. Phase I of the proposed work will extend the favorable results obtained so far towards a system-level model of the process suitable for more accurate computation of performance metrics. Mathematical models of the SiO2 molecule dissociation, ionization, transport and separation will be derived and applied to the patented apparatuses. Preliminary calculations on silicon extraction indicate the potential for solar cell production at approximately $6/Watt, a 50 times improvement over other proposed methods of space-based manufacture. We will apply this novel method of beneficiation to a simultaneous extraction of oxygen and silicon. Key questions to be answered include estimates of the physical dimensions conducive to efficient extraction (Watts/kg, kg/sec), which will drive system parameters of mirror size, solar power needs (for magnetrons and chillers), shielding, thermal management and infrastructure. Milestones within the six-month project will be: (1) vaporization, energy flow and system architecture; (2) addition of self-shielding, double-ionization, three-dimensional considerations and slag rates; (3) inlet design considerations, multiple molecule separation, and velocity profiling; and (4) composite separation rates and overall tranfer function characterization. Upon completion of Phase I we will have detailed design equations needed to construct a prototype oxygen extraction unit during Phase II.

Technology keywords

Not reported

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Agency intelligence

National Aeronautics and Space Administration

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