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Awards for “SOLID MATERIAL SOLUTIONS LLC”
10 awards on this page · sorted by amount · page 1
| Award ID | Recipient | Awarding agency | Amount | Start | End | NAICS | Description |
|---|---|---|---|---|---|---|---|
| 80NSSC19C0096 | SOLID MATERIAL SOLUTIONS LLC | National Aeronautics and Space Administration | $949.98K | 2019-08-07 | 2023-08-06 | 541715 | BI2212 SUPERCONDUCTORS FOR HIGH-POWER DENSITY MOTORS FOR AERO PROPULSION |
| 80NSSC24CA156 | SOLID MATERIAL SOLUTIONS LLC | National Aeronautics and Space Administration | $850K | 2024-06-24 | 2026-09-30 | 541715 | SBIR PHASE II - SUPERCONDUCTING STATOR THAT ENABLES MUCH LOWER WEIGHT 1 MW - 4 MW MOTORS |
| 80NSSC25C0073 | SOLID MATERIAL SOLUTIONS LLC | National Aeronautics and Space Administration | $850K | 2025-08-18 | 2027-08-17 | 541713 | PHASE II SBIR 80NSSC25C0073 SUPERCONDUCTING COIL OPERATING AT TEMPERATURES ABOVE 15K FOR ADR INSTRUMENTS |
| 80NSSC22CA074 | SOLID MATERIAL SOLUTIONS LLC | National Aeronautics and Space Administration | $750K | 2022-05-09 | 2024-05-08 | 541715 | EO14042 SBIR PHASE II HIGH TEMPERATURE SUPERCONDUCTING MAGNET OPERATING ABOVE 15 K FOR ADR COOLING |
| 80NSSC21C0649 | SOLID MATERIAL SOLUTIONS LLC | National Aeronautics and Space Administration | $200K | 2021-09-15 | 2022-12-06 | 541715 | BI2212 SUPERCONDUCTORS FOR HIGH-POWER DENSITY MOTORS FOR AERO PROPULSION |
| 80NSSC24PB441 | SOLID MATERIAL SOLUTIONS LLC | National Aeronautics and Space Administration | $150K | 2024-08-07 | 2025-02-06 | 541715 | SUPERCONDUCTING COIL OPERATING AT TEMPERATURES ABOVE 15K FOR ADR INSTRUMENTS |
| 80NSSC23PB574 | SOLID MATERIAL SOLUTIONS LLC | National Aeronautics and Space Administration | $150K | 2023-08-03 | 2024-02-02 | 541715 | SBIR PHASE I SUPERCONDUCTING STATOR THAT ENABLES MUCH LOWER WEIGHT 1 MW - 4 MW MOTORS |
| 80NSSC21C0249 | SOLID MATERIAL SOLUTIONS LLC | National Aeronautics and Space Administration | $125K | 2021-05-19 | 2021-11-19 | 541715 | "HIGH TEMPERATURE SUPERCONDUCTING MAGNET OPERATING ABOVE 15 K FOR ADR COOLING |
| 80NSSC18P1899 | SOLID MATERIAL SOLUTIONS LLC | National Aeronautics and Space Administration | $124.99K | 2018-07-27 | 2019-02-15 | 541715 | FUTURE HYBRID AIRCRAFT, SUCH AS NASA S N3-X PLAN, WILL REQUIRE ALL-SUPERCONDUCTING ELECTRIC MOTORS AND GENERATORS IN ORDER TO ACHIEVE POWER DENSITY IN EXCESS OF 10 KW/KG. UNLIKE THE DC ROTOR, THE STATOR MUST OPERATE IN AC MODE, FOR EXAMPLE, FROM 0-0.5 T AT 120 HZ, MAKING IT IMPOSSIBLE TO USE HIGH TEMPERATURE SUPERCONDUCTING (HTS) TAPES DUE TO THEIR HIGH LOSSES IN TRANSIENT FIELDS, REQUIRING INSTEAD HTS IN NARROW WIRE, FINE-FILAMENT FORM AND CABLED INTO A LOW-LOSS TRANSPOSED FORM. OUR INNOVATION CONSISTS OF AN ALL-HTS, LIGHTWEIGHT HIGH POWER MOTOR, IN WHICH THE STATOR COILS ARE WOUND WITH OUR UNIQUE LOW LOSS, TRANSPOSED CABLES, THAT IS IN TURN COMPRISED OF OUR NOVEL, STRONG, LOW LOSS, SMALL DIAMETER 2212 WIRES NOT WIDE TAPES, WHERE THE WIRES ARE SUFFICIENTLY NARROW, HAVE SUFFICIENTLY FINE FILAMENTS WITH ENHANCED MATRIX RESISTANCES BETWEEN THEM, AND AXIAL TWIST FOR THE REQUIRED LOW LOSSES IN TRANSIENT FIELD CONDITIONS WHILE PROVIDING THE OPERATING CURRENT DENSITY AND FIELD DISTRIBUTIONS AT 20 K FOR ACHIEVING>10 KW/KG SPECIFIC POWER THAT HAS BEEN SPECIFIED IN NASA SUBTOPIC A1.07. AS THE FIRST STEP, AN OPTIMIZED, PRACTICAL DESIGN WILL BE DEVELOPED FOR AN ALL-SUPERCONDUCTING, STRONG BI-2212 WIREBASED MACHINE USING A STATE OF THE ART DESIGN APPROACH. AS THE SECOND STEP, 2212-BASED WIRE AND CABLED CONDUCTOR SAMPLES FOR CHARACTERIZATION OF CRITICAL PROPERTIES WILL BE FABRICATED IN PART BY BUILDING ON THE RESULTS FROM STEP ONE, AND ALSO FROM PRIOR WORK COMPLETED BY SOLID MATERIAL SOLUTIONS ON REDUCING RAMPED FIELD LOSSES IN 2212 WIRES AND CABLES. AS THE THIRD STEP, PROPERTIES OF THE CABLES AND CONSTITUENT WIRES WILL BE TESTED , INCLUDING CRITICAL CURRENT AT 20 K AND IN FIELDS FROM 0 T TO 5 T. AS THE FINAL STEP, THE RESULTS WILL BE UTILIZED TO DEVELOP A 2212-BASED CONDUCTOR, STATOR AND MOTOR DESIGN THAT INCORPORATES FEATURES FOR ATTAINING THE TARGET AC LOSS LEVELS, WHILE ALSO MEETING ALL THE OTHER REQUIREMENTS, LIKE STRENGTH, JE AND MANUFACTURABILITY. |
| 80NSSC18P2047 | SOLID MATERIAL SOLUTIONS LLC | National Aeronautics and Space Administration | $122.42K | 2018-07-27 | 2019-02-25 | 541715 | ADIABATIC MAGNETIC REFRIGERATION (ADR) CAN ACHIEVE MUCH BETTER EFFICIENCY, AND WITH FEWER MOVING PARTS THAN COMPRESSOR-REFRIGERATORS, MAKING IT THE CHOICE FOR SPACE-BASED INSTRUMENTS THAT REQUIRE COOLING TO THE SUB-KELVIN RANGE. THE LOW OPERATING CURRENTS REQUIRED FOR SPACE-BASED USAGE, THE HIGH OPERATING CURRENT DENSITIES TO KEEP WEIGHT AND SIZE DOWN, AS WELL AS THE BENEFITS OF HIGHER OPERATING TEMPERATURE PROVIDED BY OUR 2212 SUPERCONDUCTOR ARE UNMATCHED BY ANY OTHER SUPERCONDUCTING WIRE OPTION FOR POWERING THE ADR S MAGNET. THE INNOVATION IN THIS PROGRAM CONSISTS OF A COMPACT, LOW CURRENT COIL WOUND WITH A NOVEL, VERY FINE 2212 WIRE, THAT OPERATES AT ABOUT 6 A OR LOWER, THAT GENERATES IN EXCESS OF 4 T AND THAT OPERATES AT UP TO 25K (NOT 10K) WITH LOW HYSTERESIS LOSSES IN RAMPED FIELDS, VERY CONSIDERABLY EXCEEDING THE SPECIFICATIONS IN THE GUIDELINE PUT FORWARD BY NASA, AND EXCEEDING EVEN MORE SO, PRESENT STATEOF- THE-ART ADR COIL CAPABILITIES. AS A FIRST STEP, THE PROTOTYPE 2212-BASED FINE WIRE WILL BE DESIGNED AND FABRICATED, WITH PROCESS DEVELOPMENT TO ACHIEVE THE ABOVE DESCRIBED PROPERTIES. BASED ON THESE RESULTS, LONGER LENGTH PROTOTYPE SECTIONS WILL BE PRODUCED AT BEST DESIGN AND MODE CONDITIONS, FOLLOWED BY TESTING TO VALIDATE SCALABILITY. AS A FINAL STEP, A SUBSCALE TEST COIL WILL BE WOUND AND TESTED WITH SAME BORE SIZE AS THE CURRENT, LOW TEMPERATURE SUPERCONDUCTOR-BASED COILS, IN ORDER TO DEMONSTRATE THE FEASIBILITY OF FABRICATING AN ADR- TYPE OF COIL WITH THIS WIRE. |