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Combined Vibration + Thermal Aging for Airframe Elastomers & Seals

An airframe elastomer experiences 30 years of vibration, 50°C+ undercowl temperatures, and humidity cycling — simultaneously, every flight.

✈️ Models 30-year airframe service: thermal cycling + mechanical fatigue simultaneously | 🔬 Validated: carbon-black NR, SBR 1500, EPDM, neoprene (CR), VMQ silicone under combined thermal-fatigue loading | ✅ Relevant to AS9100 certification, DO-160 environmental qualification, and MIL-SPEC airframe programs

Airframe Elastomer Aging — Vibration + Thermal | K-Load

Predict airframe elastomer life under combined vibration and thermal aging. K-Load — physics-based, validated in NR, SBR, EPDM, neoprene. AS9100/DO-160 relevant. Free trial.

K-Load Trial License

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In prediction of long-term durability

Experimental tests used for training/validation

Replacing long-weathering tests with accelerated Tests

in comparison to classic FE models of Durability