SBIR/STTR Research Award

Additive Manufacturing of Low CTE Open Isogrid Composite Structure

Award identifier c231b4613974fde336ca7b9c5a33e00ffe7d2b13d3e5aeab9fd2a1d16a184289Awarding agency National Aeronautics and Space Administration

Award amount

$149,854

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
Continuous Composites Inc.
Proposal award date
2022-07-20
Contract end date
2023-01-25
UEI
WS2YAMKAAWH9
Solicitation number
SBIR_22_P1
Topic code
S12

Research abstract

Continuous Composites Inc. (CCI) has developed and patented a continuous fiber 3-D printing technology known as CF3Dreg;. CF3D has unique capabilities to reduce cost, accelerate design cycles, scale throughput, and create highly tailorable structures (e.g., in terms of design and material properties). By utilizing continuous fiber reinforcement, snap curing aerospace-grade photopolymers, and robotics, CF3D can drastically reduce the time and cost of creating continuous fiber-reinforced composites.CF3D allows for fabrication of unique structures that would be impractical to produce with traditional methods requiring autoclave or vacuum bag pressure during curing. One such structure is an open iso-grid rib structure. Iso-grid composite structures are not a new technology and have been built and flown on space structures, however traditionally are very expensive to produce.CF3D is very conducive to the manufacturing of iso-grid composite structures, either with a skin or as an open lattice concept. The single carbon fiber tow can be put on a support surface of any shape (e.g., flat, cylindrical, or spherical). Each tow is then stacked on top of the previous tow and UV cured in-situ, resulting in any rib pattern desired for the target strength and stiffness of the structure.A unique property of the composite open iso-grid structural concept is its bulk thermal expansion properties. As each rib of the iso-grid structure is composed of all unidirectional fibers oriented along the length of the member, the CTE is very low. Published studies on T800 unidirectional laminates show CTE to be in the range of -.4 (10-6 X K-1) in the fiber direction. This results in a structure that is overall lightweight and isotropic given the nature of the iso-grid concept with a very low CTE. Using high strength, low-cost intermediate modulus fibers to build a lightweight, low CTE structure has the potential to greatly decrease the weight, cost, and lead time of dimensionally stable structures.nbsp;

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

8 SBIR/STTR records share this UEI (2021–2025). Reported award amounts total $6,472,937. Reported amounts are not federal obligations.

Phases: Phase I, Phase II – Direct to Phase II, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration

Agency intelligence

National Aeronautics and Space Administration

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