SBIR/STTR Research Award

Superconducting stator that enables much lower weight 1 MW - 4 MW motors

Award identifier fa4de0dff111e5950a8e3c12a88268fe142a3111db4fd99e75843e2d5eb86679Awarding agency National Aeronautics and Space Administration

Award amount

$850,000

Program and phase

SBIR · Phase II

Award year

2024

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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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