Composites

Thermal Protection

Textum fabricates composite thermal protection systems that operate in both ablative and non-ablative regimes, addressing a wide variety of application needs including aeroshells and shrouds, heatshields, and flow paths. Textum is focused mainly on carbon-based composite solutions but has some flexibility to support non-carbon composite solutions as well. Textum does not provide final machining or coating services but can help you address those additional details with partner businesses if needed.

Composites

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Wall thickness up to 4” in general

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Axi-symmetric or variable cross-section

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Open or closed geometries

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Variable density/porosity

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With or without shingle angle

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Can be made thermally insulative

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Multiple matrix options (including carbon) and grades of C fiber available

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Demonstrated parts nearly 4’ long (no fundamental constraints on size)

Benefits:

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Fast production times (6-8 weeks on average)

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Highly scalable production paradigm

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Affordable manufacturing costs

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Excellent thermo mechanical performance

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Performance tunability based on material choices and processing

Composites

Hot Structures

Thermal protection systems sometimes have to do double duty and satisfy primary structural requirements as well. When that happens, the choices for how to approach the dual challenge shrink to a narrow subset of materials. C/C and CMC materials are required.

Technical Detail:

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Wall thickness up to 2” in general

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Complicated shapes and cross-sections

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New, proprietary fiber architectures

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Blended reinforcement strategies with co-molding

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Very low defect count (including porosity)

Benefits:

Fast production times
Dimensional stability in extreme environments
Multifunctional system capability
Low material variability
Excellent interlaminar properties

Composites

Solid Rocket Motors

Composites are used throughout solid rocket motor nozzle assemblies for weight optimization, but they introduce concerns about erosion resistance and thermal conductivity at the throat, in the insulation and support of throat materials, and protection of bond lines to metallic components. They may be designed to erode or retain shape stability, and Textum can address a wide range of need in terms of geometry, part size, environmental exposures, and mission durations.

Technical Detail:

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C/C throat components up to 24” in diameter

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Composite throat support/insulation

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Composite exit cone liners and conic sections

Benefits:

Domestic material choices
Fast production and short lead times
Affordable and scalable manufacturing
Stable supply chain (with redundancy)
Variable
performance

Composites

Hypersonics

Flying fast is hard to endure. Our job isn’t to plan the mission or build the system, but we are ready to help your vehicle survive whatever path it takes, be it a reusable system or a one-time use. Everything we do in composite TPS, Hot Structures, and Solid Rocket Motors as well as High Temperature Seals, gets pushed to the edge of its performance envelope in the hypersonic mission
set. Our job is to keep producing high quality components at high rate as the requirements hit their upper limits.

Technical Detail:

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Nosetips, leading edges, acreage, and flight control surfaces

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Axi-symmetric or variable cross-sections

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Bespoke textile preform designs for specific part geometries

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Manufacturing paradigm designed for high-volume, low-cost production

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Boost-glide and airbreathing

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Propulsion and glide body components

Benefits:

Stable, domestic supply chains
Near net shape manufacturing
Fast production and lead times
Improved thermo mechanical performance
Manufacturing reliability
(low scrap)
Reduced part counts through co-molding

Contact Us

Textum welcomes the opportunity to become your solutions manufacturer for scrims and composite fabrics. Our expertise includes standard fabrics, narrow fabrics, tubular fabrics, helical/circular fabrics, 3D fabrics, 3-D preforms, plus hybrid combinations.

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