SBIR/STTR Research Award

Boron Nitride Nanotube-Enhanced Hot Structure Technology for Aerospace Vehicles

Award identifier ad5c84094e3cdbf613f848d384e499a094e6378ae73a3b1d2dc3aca19481dff0Awarding agency National Aeronautics and Space Administration

Award amount

$149,994

Program and phase

SBIR · Phase I

Award year

2022

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
BNNT LLC
Proposal award date
2022-07-20
Contract end date
2023-01-25
UEI
YG25NMGFRND9
Solicitation number
SBIR_22_P1
Topic code
H5

Research abstract

Boron nitride nanotubes (BNNTs) are a breakout reinforcement, structurally and thermally, needed for hot structures from 1650-2000 deg;C. BNNTs advance the state-of-the-artnbsp;being as strong as carbon nanotubes plus superior oxidation and chemical resistance. The highest-quality BNNTs, which we recently started producing at industrial scale by methods improved from what earned our founders NASA Invention of the Year, now embody key performance parameters of being ultra-strong (63 GPa or above), highly flexible, lightweight, pure, highly crystalline (low-defect), molecular ceramic fibers.nbsp;BNNT offers the strongest and lightest high-temperature reinforcement for ceramic matrix composite (CMC) hot structures, where, protected from oxidation, service temperature of BNNTs is at least 2000 deg;C. State-of-the-art BNNT reinforcement has significantly improved ceramic, e.g., SiCN, to 3.5x toughness, 2x hardness, 1.3x flexural strength (also SiON and ZrO2). This project adds hafnium oxide (HfO2) to SiCN/BNNT, so HfSiO4 forms a protective coating and protects within the volume to raise temperature thresholds.nbsp;Project objective is to use BNNTs as sturdy, self-supporting, 3-D shapes infused with the pre-ceramic polymer precursor, SiCN doped with hafnium oxide (HfO2), and pyrolyzed to form a new polymer-derived ceramic (PDC) composite, BNNT/SiCN/HfSiO4. Phase I will develop techniques to fabricate reinforced ceramics for hot structures based on prior proofs-of-concept in other ceramic matrices. Coupons will be delivered for thermal and mechanical tests, arc-jet tests, hot-fire/combustion flame tests, plus complex shapes for additional tests.nbsp;NASA applications start with uncooled propulsion components, combustion chambers, nozzles, and load-carrying aeroshell structures, leading edges, and heatshields subject to oxidizing environments and/or temperatures of 1650-2000 deg;C. Defense applications follow, starting with RF-transparent matrices for radar domes on aircraft traveling above Mach 5.

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

9 SBIR/STTR records share this UEI (2018–2025). Reported award amounts total $8,244,634. Reported amounts are not federal obligations.

Phases: Phase II, Phase I

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

Agency intelligence

National Aeronautics and Space Administration

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