SBIR/STTR Research Award

High Power Density Motors/Generators for Single and Double Aisle Passenger Aircraft using Multifilamentary High Purity Aluminum Coils at 20K

Award identifier 3b924d5c0ffced9ab4beb1a7bd228f55c9aaa0cce4b35e5aad3473031de3c382Awarding agency National Aeronautics and Space Administration

Award amount

$899,999

Program and phase

SBIR · Phase II

Award year

2025

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
HYPER TECH RESEARCH INC
Proposal award date
2025-07-24
Contract end date
2027-07-28
UEI
YPG9JKMCSUA8
Solicitation number
SBIR 2024-II
Topic code
A1

Research abstract

Cutting-edge research in aeronautics is needed to overcome technology barriers and challenges in developing net-zero carbon emissions from aviation by 2050, one of the environmental goals articulated in the White House’s U.S. Aviation Climate Action Plan, and aggressive innovations will be required to reach this goal through development of hybrid-electric machines for aircraft propulsion used for direct-drive propulsion of fans or propellers or as generators, turboprops, or turbofans. High power density propulsion motors are a driving factor for aircraft electrification especially for the larger single and double aisle passenger aircraft. In order to achieve the goal of > 25 kW/kg, it is important to have both stator and rotor high performance and probably both cryogenic. NASA has been advocating the use of all-superconducting rotating machines for electric propulsion. The problem is high AC in the stator. With lower AC losses, High Purity Aluminum (HPAL) Composites configured as multifilamentary wire and cables can out-perform superconductors above 100 Hz for some rotating machine targets. We propose in this project to develop and demonstrate stator coils using multifilamentary, low AC loss, HPAL strands for 20-25 K operation. The use of HPAL low AC loss stands will facilitate aircraft applications in the 1 to 20 MW range enabling high power density motors and generators in the 35-45 kW/kg range, with efficiencies in the range of 99%. During a Phase II effort we will fabricate and characterize HPAL stator coils in an existing 100 kW motor test bed. liquid hydrogen makes an obvious candidate for a thermal sink in the aircraft; the demonstration stator coils will be cooled using liquid and gaseous helium. After the Phase II effort, the technology demonstrated will create both a technical and business pathway for introduction of motors which include our HPAL composite cryogenic conductor for single and double aisle passenger aircraft.

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

102 SBIR/STTR records share this UEI (2000–2025). Reported award amounts total $40,663,857. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Energy, National Aeronautics and Space Administration, Department of Defense, Department of Health and Human Services

Agency intelligence

National Aeronautics and Space Administration

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