Evaluating PA66 CF30 BLACK for UAV and drone propeller projects

PA66 CF30 BLACK is presented as a carbon-fiber reinforced nylon 66 material to evaluate for UAV propeller development. Material selection is only one part of a propeller project. This guide separates the available batch evidence from the application and processing questions that still need to be answered.

What the supplied PA66 CF30 data can tell you

The supplied COA contains tensile strength, flexural strength, flexural modulus, Charpy notched impact strength and density for two batches. These values provide a documented starting point for material evaluation. They are not measurements of a finished propeller's thrust, noise, maximum RPM, service life or flight endurance.

Processing and injection-molding questions

If you plan to mold drone propeller components, request processing guidance for the exact grade and lot. Drying temperature, drying time, permitted moisture level, melt temperature, mold temperature and other molding parameters are not supplied in the reference COA. No numerical processing settings are recommended on this website. Confirm suitable guidance before production trials.

Finished UAV propeller validation

Discuss the final geometry, process and intended operating conditions with your engineering team. Plan finished-part verification appropriate to the project, including dimensional consistency, mechanical strength, balance, fatigue and flight performance. The website does not supply a validated propeller design or a flight-qualified finished product.

Comparing carbon-fiber reinforced nylon 66 candidates

Compare materials using documented specifications and compatible test conditions rather than a single headline strength value. Ask what moisture conditioning and specimen conditions apply to each reported result. If a requirement is absent from the available report, treat it as unverified and request evidence instead of assuming a value.

Start a PA66 CF30 propeller material enquiry

Provide your application, intended process, evaluation quantity and destination. Describe any temperature, moisture, mechanical or repeatability requirements you need to investigate. Ask for current batch information, processing documentation and sample availability. The propeller hero image is AI-generated application artwork, not an image of a certified supplied component.

Technical source: supplied COA, Shanghai Yunyuan New Material Technology Co., Ltd. Test dates: 2026-09-08 and 2026-09-03. Batch results do not guarantee future shipment or finished-part performance.