SBIR/STTR Research Award

Nanotailored Carbon Fibers

Award identifier bfc2bfc371d2b2599c53f365b9ad650bd6a151b0eeef674c62f1785e0951fe62Awarding agency Department of Defense · Air Force

Award amount

$750,000

Program and phase

STTR · Phase II

Award year

2010

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
NANO ENGINEERED MATERIALS CORP.
Proposal award date
2009-12-10
Contract end date
2011-12-10
UEI
Not reported
Solicitation number
2008.A
Topic code
AF08-T028

Research abstract

Polyacrylonitrile (PAN)/carbon nanotube (CNT) composite fibers will be spun using gel spinning technology in conjunction with bi-component spinning to obtain small diameter precursor fiber (2 - 6 micrometer). Single component spinning (multi-filaments) will also be conducted. The precursor fibers will have tensile strength >1 GPa and tensile modulus >25 GPa. By optimizing stabilization and carbonization conditions, high tensile strength carbon fiber will be obtained with various diameter. CNT incorporation can lead to the ordered graphitic structure around the CNT, which will improve the mechanical properties of resulting carbon fiber. These nano-tailored carbon fibers will have superior tensile and compressive properties as well as better electrical and thermal conductivity as compared to the conventional PAN-based carbon fiber. BENEFIT: We expect to process carbon fibers with a minimum tensile strength of 7 GPa and a minimum tensile modulus of 450 GPa. Compressive strength of these fibers is expected to be comparable to their tensile strength (7 GPa). These fibers are also expected to have higher electrical and thermal conductivity than commercial high strength PAN based carbon fibers. As compared to the current commercial carbon fiber, these high strength and high modulus carbon fibers should result in significant weight savings in various aerospace composite systems.

Technology keywords

Not reported

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Agency intelligence

Department of Defense

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