Tab 04 4 Statement of Work
Updated
A PDF document (124 KB) attached to Testing of Lunar Regolith Stimulant Thermal Properties, from the National Aeronautics and Space Administration. Due Oct 27, 2026, 3:00 PM (UTC-5).
File name: SATPC0042989 Tab 04 4 SOW.pdf
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STATEMENT OF WORK
1. Objective/Requirements
a. Gather thermal properties of ICN-LHT-1G lunar regolith simulant at a relevant bulk sample density of 1.5 to 1.6 grams per cubic centimeter. i. ASTM E1461 Diffusivity and calculated conductivity
1. Temperatures of 1200, 1300, 1400, 1500, 1600, 1650, and 1700 Degrees Celsius
ii. ASTM E1269 DSC specific heat capacity
1. Measured from 25 to 1650 degrees Celsius
2. Characteristics, Scope, and Specs
a. Provide thermal testing of ICN-LHT-1G lunar regolith simulant. b. Testing will include
i. ASTM E1461 Diffusivity and calculated conductivity
1. Temperatures of 1200, 1300, 1400, 1500, 1600, 1650, and 1700 Degrees Celsius
ii. ASTM E1269 DSC specific heat capacity
1. Measured from 25 to 1650 degrees Celsius
iii. Simulant shall be to a density of 1.5-1.6 grams per cubic centimeter during testing. Density shall be reported.
3. Place of Performance
Frim’s Testing Facility
4. Period of Performance
Final report delivery no later than 8 weeks after procurement.
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