SBIR/STTR Research Award

Localized 3-D Fiber Reinforcement in C-C and Ceramic Composites

Award identifier a96a70e0cab80f07995714981af3f588c978e625d03ebc9567eab4ed1cd8ab12Awarding agency National Aeronautics and Space Administration

Award amount

$156,427

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
North Country Composits LLC
Proposal award date
2022-07-22
Contract end date
2023-01-25
UEI
GMZ4VR5NC6C3
Solicitation number
SBIR_22_P1
Topic code
H5

Research abstract

North Country Composites (NCC) is teaming with Lancer Systems to modify Lancerrsquo;s commercial ceramic matrix composite (CMC) manufacturing methods to produce affordable very high performance rocket engine components.nbsp; The components would operate in highly oxidative and corrosive environments to temperatures up to 3600oF for long durations (many hours) and 4600oF for shorter durations.nbsp; This will occur without the use of expensive coatings.nbsp; Through the utilization of low cost ISO 9001 controlled manufacturing methods, affordable, high performance components can rapidly be transitioned for commercial use.nbsp; In addition, NCC will utilize 3D reinforcement of the fiber preforms to significantly increase (3X) interlaminar strength properties with only a mild decrease in plane properties.The high strength, light weight and high temperature capabilities of these structures will significantly increase the performance of rocket engines by increasing the thrust to weight, operational temperatures, and pay-load capabilities.The purpose of the Phase I program is to demonstrate the feasibility producing ultra-high temperature (UHT) CMCs for use as chambers and nozzle extensions in liquid rocket engines.nbsp; During Phase I the NCC team will produce a nozzle extension for hot fire test in LOx/Methane.nbsp; In addition we will produce thermo-mechanical test specimens with optimized interlaminar strength properties. nbsp;After high temperature, oxidative exposure, they will present strength retention of greater than 85%.In the Phase II program we will work with engine suppliers to perform the technical maturation work for a specific engine system nozzle extension that will result in use of the NCC components in Phase III and other programs.nbsp; As a result of developing a significantly cost and time reduced UHT-CMC manufacturing process, NASA and other customers will garner the performance increases for rocket propulsion and other advanced vehicle applications.

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

2 SBIR/STTR records share this UEI (2022–2023). Reported award amounts total $1,056,395. Reported amounts are not federal obligations.

Phases: Phase II, Phase I

Agencies: National Aeronautics and Space Administration

Agency intelligence

National Aeronautics and Space Administration

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