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Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- SOLID MATERIAL SOLUTIONS LLC
- Proposal award date
- 2024-06-24
- Contract end date
- 2026-06-23
- UEI
- D4TGS357V2K3
- Solicitation number
- SBIR_23_P2
- Topic code
- A1
Research abstract
Futurenbsp;hybrid and hydrogen-powered zero carbon-emissionnbsp;electric aircraft require high temperature superconducting (HTS) electric motors to achieve power densities above 10 kW/kg while operating at temperatures above 25 K. However, the AC modes of stator coils in these motors makes it impossible to use available HTS tapes due to their large AC losses, requiring instead fine HTS wires made with the HTS-2212 material with advanced loss reducing features. The Phase I program established the feasibility of a low loss HTS-2212 cable with commercial-level operating current densities, losses and racetrack coilability. It built on our recent breakthrough development of low-loss HTS-2212 wire and cable features. Subscale and a full build (30 turn) racetrack test coil were fabricated and tested to establish and demonstratenbsp;coil ability of this cable type. nbsp;Thisnbsp;coil was also the Phase I deliverable, with test data showingnbsp;in-coil operating currentnbsp;meeting required levels, namely, current density gt;200 A/mm2 at abovenbsp;25Knbsp;innbsp;0.5 T field.
nbsp; nbsp; nbsp; In Phase II, by building on the 16-wirenbsp;cable design, higher winding current cable with up to 96 wires will be developed and optimized for full stator coil functionality and loss. Loss and other critical properties will be validated by coil tests,nbsp;providing vitalnbsp;specifications to HTS motor developers, including guidance for cost-effective stator cooling. A 1 MW motor-scale prototype HTS-2212-based stator saddle coil with end region knuckle bends that enable required nesting will be developed, with performance, loss, and cool-ability validated by testing, and with this coil provided to NASA as a deliverable. By the end of the program all the design features for motor-useable HTS stators will be established, withnbsp;validation of low losses, performance at operating conditions and inclusion into at least one large-scale electric plane development initiative, with the groundwork for a collaboration already established in Phase I program.
Technology keywords
Not reported
Other awards by this recipient
Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.
Research funding history
19 SBIR/STTR records share this UEI (2014–2025). Reported award amounts total $9,231,848. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: National Aeronautics and Space Administration, Department of Energy, Department of Health and Human Services
Agency intelligence
National Aeronautics and Space Administration
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