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Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- VISTA ENGINEERING AND CONSULTING, LLC
- Proposal award date
- 2023-07-27
- Contract end date
- 2024-09-02
- UEI
- C19FRGNHX4S3
- Solicitation number
- STTR_23_P1
- Topic code
- T12
Research abstract
We propose to develop resistance welding (RW) technology for carbon fiber reinforced thermoplastic composites (CFR-TCs) based on innovative heating element technology. A proposed target for these innovations is repurposable aerospace applications. Historically, CFR-TCs were not considered as the material of choice for aerospace applications despite their excellent specific strength and modulus. Instead, CFR- epoxy composites have been extensively used primarily for their ease of manufacture and excellent specific properties. However, they pose a great challenge to be recycled, reused, and repurposed. However, CFR-TCs can be reheated and remelted which makes it possible for them to be reshaped, repaired, recycled, and repurposed.Structures must be joined together and fusion welding of CFR-TCs is a method that takes advantage of the reheatable nature of thermoplastics. Bonding is achieved by heating the CFR-TC surfaces to above the melting or glass transition temperature while applying a clamping pressure. RW involves placement of a resistive material (heating element) between two workpieces and heating it with an electric current while applying a clamping pressure to ensure good contact and efficient thermal conduction. The localized heating melts the workpiecersquo;s surfaces and mixes materials through diffusion, penetration, entanglement of thermoplastic polymer chains, and carbon fiber migration at the interface. However, poor shear strength between the bonded surfaces has been a continuing problem. The proposed project will seek to create a 3D strength pattern at the bonded surface to increase shear strength in the joint.RW, with the proposed improvements, offers unique advantages, such as 3D joint strength, less requirement of equipment, direct conversion from electricity to heat, and efficient localized heating, all of which can be significant for an application like repurposing materials for deep space exploration applications in which resources are very limited.nbsp;
Technology keywords
Not reported
Other awards by this recipient
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Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
Research funding history
3 SBIR/STTR records share this UEI (2008–2025). Reported award amounts total $1,099,948. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: National Aeronautics and Space Administration, Department of Defense
Agency intelligence
National Aeronautics and Space Administration
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