| Richter (1992) Experimental Determination of In Situ Utilization of Lunar Regolith for Thermal Energy Storage | 43.86 | 6.32 | 13.68 | 13.40 | 2.60 | 6.68 | 10.13 | 2.12 | 0.281 | 0.198 | - | 0.20 | - | - | - | - | - |
|---|
Details- Specific note
- Element chemistry comparison
- Method
- Not specified
- Table
- Table 1
- Page
- Page 3
|
| Tucker (1992) Glass fiber processing for the Moon/Mars program | 43.86Average45.90Maximum41.70Minimum | 6.32Average7.43Maximum4.82Minimum | 13.68Average15.60Maximum11.76Minimum | 13.40Average14.40Maximum12.00Minimum | 2.60Average4.10Maximum0.90Minimum | 6.68Average8.44Maximum5.57Minimum | 10.13Average11.48Maximum9.04Minimum | 2.12Average2.27Maximum1.97Minimum | 0.281Average0.348Maximum0.167Minimum | 0.198Average0.218Maximum0.182Minimum | - | 0.20Average0.45Maximum0.02Minimum | - | - | - | - | - |
|---|
Details- Specific note
- Major element chemistry of MLS-1
- Method
- Not specified
- Table
- Table 3
- Page
- Page 13
|
| Tucker (1991) Differential thermal analysis of lunar soil simulant | 43.86Average45.90Maximum41.70Minimum | 6.32Average7.43Maximum4.82Minimum | 13.68Average15.60Maximum11.76Minimum | 13.40Average14.40Maximum12.00Minimum | - | 6.68Average8.44Maximum5.57Minimum | 10.13Average11.48Maximum9.04Minimum | 2.12Average2.27Maximum1.97Minimum | 0.281Average0.348Maximum0.167Minimum | 0.198Average0.218Maximum0.182Minimum | - | 0.20Average0.45Maximum0.02Minimum | - | - | - | - | - |
|---|
Details- Specific note
- Average/Maximum/Minimum
- Method
- Not specified
- Table
- Table 3
- Page
- Page 9
|
| Tucker (1991) Differential thermal analysis of lunar soil simulant | - | - | - | - | 2.60Average4.10Maximum0.90Minimum | - | - | - | - | - | - | - | - | - | - | - | - |
|---|
Details- Specific note
- statistics
- Method
- Not specified
- Table
- Table 3
- Page
- Page 9
|
| Eick (1996) Dissolution of a lunar basalt simulant as affected by pH and organic anions | 45.0 | 5.2 | 15.3 | 14.2 | 1.2 | 5.6 | 9.6 | 2.0 | 0.34 | - | - | 0.45 | - | - | - | - | - |
|---|
Details- Specific note
- Compared with average Lunar Mare sample composition
- Method
- Bulk chemical composition analysis
- Table
- Table 1
- Page
- Page 3
|
| Eick (1996) Dissolution of a lunar basalt simulant as affected by pH and organic anions | 55.67Feldspar — MLS-151.88Pyroxene — MLS-135.07Olivine — MLS-10.02Ilmenite — MLS-1 | 0.09Feldspar — MLS-10.64Pyroxene — MLS-10.07Olivine — MLS-150.05Ilmenite — MLS-1 | 28.84Feldspar — MLS-11.60Pyroxene — MLS-10.01Olivine — MLS-10.04Ilmenite — MLS-1 | 0.41Feldspar — MLS-111.76Pyroxene — MLS-140.30Olivine — MLS-145.28Ilmenite — MLS-1 | - | 0.01Feldspar — MLS-113.72Pyroxene — MLS-123.88Olivine — MLS-11.31Ilmenite — MLS-1 | 10.99Feldspar — MLS-119.97Pyroxene — MLS-10.54Ilmenite — MLS-1 | 4.03Feldspar — MLS-10.24Pyroxene — MLS-10.02Ilmenite — MLS-1 | 0.03Feldspar — MLS-10.01Pyroxene — MLS-1 | 0.29Pyroxene — MLS-10.49Olivine — MLS-10.50Ilmenite — MLS-1 | 0.03Pyroxene — MLS-10.07Ilmenite — MLS-1 | - | - | - | - | - | - |
|---|
Details- Specific note
- Feldspar, pyroxene, olivine, and ilmenite
- Method
- Mineral chemistry comparison
- Table
- Table 2
- Page
- Page 4
|
| Hill (2007) Apollo sample 70051 and high‐ and low‐Ti lunar soil simulants MLS‐1A and JSC‐1A: Implications for future lunar exploration | 42.8* | 6.77* | 12.1* | 16.3ᵉ* | - | 6.19* | 11.1* | 2.22* | 0.20* | 0.22* | - | 0.04* | - | - | - | - | - |
|---|
Details- Specific note
- SiO₂ bulk-chemical composition
- Method
- Not specified
- Table
- Table 1
- Page
- Page 2
|
| Hill (2007) Apollo sample 70051 and high‐ and low‐Ti lunar soil simulants MLS‐1A and JSC‐1A: Implications for future lunar exploration | 0* | - | - | - | - | - | - | - | - | - | - | - | - | - | - | - | - |
|---|
Details- Specific note
- JSC-1A and MLS-1A lunar soil simulants
- Method
- Not specified
- Table
- Table 3
- Page
- Page 4
|
| Hill (2007) Apollo sample 70051 and high‐ and low‐Ti lunar soil simulants MLS‐1A and JSC‐1A: Implications for future lunar exploration | 55.6 (5)*Plagioclase35.4 (11)*Olivine0.05 (1)*Ti-magnetite51.3 (6)*Cpxᵇ52.1 (3)*Opxᵇ39.7 (18)*Amphibole | 7.62 (38)*Ti-magnetite50.0 (11)*Ilmenite0.51 (28)*Cpxᵇ0.26 (13)*Opxᵇ1.51 (7)*Amphibole | 27.1 (4)*Plagioclase2.54 (16)*Ti-magnetite1.20 (28)*Cpxᵇ0.55 (4)*Opxᵇ11.2 (10)*Amphibole | 0.50ᶜ (19)*Plagioclase41.5ᶜ (10)*Olivine37.4 (5)*Ti-magnetite45.9ᶜ (3)*Ilmenite11.7ᶜ (11)*Cpxᵇ25.9ᶜ (6)*Opxᵇ22.5ᶜ (13)*Amphibole | 46.9 (6)* | 22.1 (17)*Olivine0.09 (1)*Ti-magnetite1.22 (23)*Ilmenite13.6 (2)*Cpxᵇ19.6 (6)*Opxᵇ6.93 (121)*Amphibole | 9.86 (49)*Plagioclase0.13 (11)*Ti-magnetite20.6 (11)*Cpxᵇ1.08 (9)*Opxᵇ11.3 (1)*Amphibole | 5.63 (23)*Plagioclase0.20 (4)*Cpxᵇ0.02 (1)*Opxᵇ2.12 (3)*Amphibole | 0.46 (7)*Plagioclase1.15 (30)*Amphibole | 0.58 (2)*Olivine0.19 (4)*Ti-magnetite0.55 (8)*Ilmenite0.32 (10)*Cpxᵇ0.55 (5)*Opxᵇ0.24 (6)*Amphibole | 0.26 (5)* | - | 0.07 (4)* | - | - | - | 99.1*Plagioclase99.7*Olivine97.4*Ti-magnetite97.7*Ilmenite99.4*Cpxᵇ100.1*Opxᵇ99.7*Amphibole |
|---|
Details- Specific note
- Major mineral phases
- Method
- Not specified
- Table
- Table 5
- Page
- Page 8
|
| Liu (2026) In Situ Synthesis of Agglutinitic Glass and Np‐Fe⁰ in a Chang'E‐5 Lunar Regolith Simulant for Multi‐Scale High Fidelity | 43.86 | 6.32 | 13.68 | 16 | - | 6.68 | 10.13 | 2.12 | 0.28 | 0.2 | - | 0.2 | - | - | - | / | - |
|---|
Details- Specific note
- a critical indicator of the volatile-poor nature of lunar regolith
- Method
- Chemical oxide composition; LOI by loss on ignition
- Table
- Table 1
- Page
- Page 2
|
| Li (2019) The Preparation and Characterization of NEU-1 Lunar Soil Simulants | 43.86 | 6.32 | 13.68 | - | 16.00 | 6.68 | 10.13 | 2.12 | 0.28 | 0.20 | - | 0.20 | - | - | - | - | - |
|---|
Details- Specific note
- %, mass fraction
- Method
- Not specified
- Table
- Table 3
- Page
- Page 4
|
| Kanamori (1998) Properties of Lunar Soil Simulant Manufactured in Japan | 43.9 | 6.3 | 13.7 | 13.4 | 2.6 | 6.7 | 10.1 | 2.1 | 0.28 | 0.20 | - | 0.20 | - | - | - | - | - |
|---|
Details- Specific note
- Concentration (Wt %)
- Method
- Not specified
- Table
- Table 2
- Page
- Page 4
|
| Jiang (2012) Properties of TJ-1 Lunar Soil Simulant | 43.86* | 6.32* | 13.68* | 13.40* | 2.6* | 6.68* | 10.13* | 2.12* | 0.28* | 0.20* | ND* | 0.20* | ND* | ND* | ND* | 0.0015* | - |
|---|
Details- Specific note
- Main element composition
- Method
- Not specified
- Table
- Table 6
- Page
- Page 5
|
| Zhou (2024) Properties and Characteristics of Regolith-Based Materials for Extraterrestrial Construction | 43.86 | 6.320 | 13.68 | 16.00 | - | 6.68 | 10.13 | 2.120 | 0.28 | 0.20 | - | 0.20 | - | - | - | - | - |
|---|
Details- Specific note
- Lunar regolith samples and regolith simulant
- Method
- Chemical composition
- Table
- Table 3
- Page
- Page 5
|
| Hou (2019) Constitutive properties of irregularly shaped lunar soil simulant particles | 47.3 | 1.6 | 17.8 | 10.5 | - | 9.6 | 11.4 | 0.7 | 0.6 | 0.1 | - | - | - | - | - | - | - |
|---|
Details- Specific note
- Average SiO₂ component
- Method
- Not specified
- Table
- Table 1
- Page
- Page 3
|
| Miller (2009) Lunar soil as shielding against space radiation | 42.8* | 6.77* | 12.1* | 16.3* | - | 6.19* | 11.1* | 2.22* | 0.20* | 0.22* | - | 0.04* | - | - | - | 0.85* | - |
|---|
Details- Specific note
- soil samples used in the radiation experiments
- Method
- Not specified
- Table
- Table 2
- Page
- Page 2
|
| Ryu (2015) Basic Study for a Korean Lunar Simulant (KLS-1) Development | 47.3* | 1.6* | 17.8* | 10.5* | - | 9.6* | 11.4* | 0.7* | 0.6* | 0.1* | - | - | - | - | - | - | - |
|---|
Details- Specific note
- Weiblen et al., 1990
- Method
- Not specified
- Table
- Table 2
- Page
- Page 5
|
| Xie (2017) Aluminothermic Reduction-Molten Salt Electrolysis Using Inert Anode for Oxygen and Al-Base Alloy Extraction from Lunar Soil Simulant | - | - | - | - | - | ~0.21 | ~0.59 | - | ~0.014 | - | - | - | - | - | - | - | - |
|---|
Details- Specific note
- 48.66 mass%NaF-46.34 mass%AlF3-5 mass%MLS-1
- Method
- Reported approximate system composition
- Page
- Page 3
|