SBIR/STTR Research Award

Boron Nitride Nanotube-Enhanced-Performance Radome Materials for High-Speed Missiles

Award identifier 24ae244f5984e5695223f766eb794c746c0754d21a465ae5f0e5cc67c9e49bd1Awarding agency Department of Defense · Navy

Award amount

$246,954

Program and phase

SBIR · Phase I

Award year

2022

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Award details

Awarding agency
Department of Defense
Branch
Navy
Recipient company
BNNT LLC
Proposal award date
2022-08-01
Contract end date
2023-02-03
UEI
YG25NMGFRND9
Solicitation number
22.1
Topic code
N221-043

Research abstract

PDC/BNNT composites are the solution to otherwise intractable challenges to hypersonic flight.  Hypersonic flight requires significant innovation to radar domes (radomes) of vehicle nosecones to maintain essential RF communications and sensing amid the compressed engagement timelines and severe aerodynamic heating with thermal shocks that such speed brings.  Known ceramics and fiber reinforcement techniques do not allow the required combination of RF transparency, strength, or high-temperature endurance, nor allow tailoring compatible layers.  Boron nitride is a known high-temperature dielectric, but not previously in a structurally useful form.  Previously-known nanotubes and fiber reinforcements, while having high strength, do not meet the combined requirements of high-temperature strength, controllable thermal conductivity, low dielectric constant, and low loss tangent for reliably-performing RF transparent radome structures. ?  PDC/BNNT (boron nitride nanotube-enhanced polymer-derived ceramic matrix composites) facilitate insertion of these high-temperature nano-reinforcements first into a polymer, then pyrolyzing it into the desired ceramic with controlled, tailorable characteristics.  Not only do they improve thermo-structural capability and not compromise electrical performance, they improve both.  Earliest PDC/BNNT composites already demonstrate over ten times the flexural strength of legacy materials (such as Pyroceram 9606), and excellent RF transparency with dielectric constant (relative permittivity) as low as 1.5 and dielectric loss tangent smaller than 0.025.    These PDC/BNNT composites will be used to develop architecture concepts, then prototypes, for a new common radome architecture to enable multiple future advanced missiles to fly longer and faster (supersonic and hypersonic) through all weather.  Optimization of ceramics explored so far is expected to improve strength above 1,500 ºC, and potentially to 2,100 ºC for newer matrix systems.

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

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

Department of Defense

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