Figure of Merit Characteristics Compared to Engineering Parameters

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Figure of Merit Characteristics Compared to Engineering Parameters

Figure of Merit Characteristics Compared to Engineering Parameters

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LIST OF ACRONYMSBrClCO 2FFe 0FoMH 2 OIISRUMSFCnFe 0OHPTMbrominechlorinecarbon dioxidefluorineiron metalfigure <strong>of</strong> meritwateriodinein situ resource utilizationMarshall Space Flight Centernanophase iron metalhydroxylphosphorousTechnical Memorandumvii

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Presentation - In Situ Resource Utilization (ISRU)

David Lynch - NASA

NU-LHT-1M PILOT - NASA

Design and Specifications for the Highland Regolith Prototype - NASA

Analysis of lunar highland regolith samples from Apollo 16 drive ...

effect of comminution method on particle damage and breakage

Lunar Airborne Dust Toxicity Assessment Group (LADTAG) - NASA

Simulant requirements - Nasa

Plasma Reduction of Lunar Regolith for In-Space ... - ISRU - Nasa

Modal Analyses of NU-LHT-1M and - NASA

Book of Abstracts- Lunar Regolith Simulant Materials Workshop

Pilot Sample NU-LHT-1M

Measurement of Particle Size and Shape Distribution For ... - Nasa

Larry Taylor (lataylor@utk.edu), David Carrier, and Jeff Taylor - Nasa

LIST OF ACRONYMSBrClCO 2FFe 0FoMH 2 OIISRUMSFCnFe 0OHPTMbrominechlorinecarbon dioxidefluorineiron metalfigure <strong>of</strong> meritwateriodinein situ resource utilizationMarshall Space Flight Centernanophase iron metalhydroxylphosphorousTechnical Memorandumvii

Page 1 and 2: NASA/TM—2010-216443Figure of Meri
Page 3 and 4: NASA/TM—2010-216443Figure of Meri
Page 7: LIST OF TABLES1. Properties from th
Page 11 and 12: TECHNICAL MEMORANDUMFIGURE OF MERIT
Page 13 and 14: 2. FIGURE OF MERIT2.1 Objective of
Page 15 and 16: 3. EVALUATION OF RECOMMENDED PROPER
Page 17 and 18: 3.1.1 Compressive Strength3.1 Geome
Page 19 and 20: 3.2.5 Surface AreaSurface area is a
Page 21 and 22: glass composition other than to res
Page 23: 4. CONCLUSIONThe FoM is considered
Page 26: REPORT DOCUMENTATION PAGEForm Appro