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How do the materials in By Material perform in high – altitude conditions?

As a supplier of advanced materials for By Material, I’m often asked a question that feels both simple and loaded with real-world stakes: How do our materials hold up at high altitude? Anyone who’s spent time above 8,000 feet knows high-altitude conditions aren’t just “thin air”—they’re a brutal test of engineering. For the aerospace, renewable energy, and industrial equipment teams that rely on us, a material that fails 10,000 feet up isn’t just a product; it’s a safety risk, a project delay, or a missed opportunity to build something that works where few others can. Over the past seven years working directly with By Material’s R&D and client engineering teams, I’ve collected firsthand data, on-site test insights, and even a few hard lessons from materials that didn’t make the cut. Today, I want to pull back the curtain on how our materials perform in those thin, cold, high-stress environments—no marketing fluff, just the facts we use to get our partners home safely. By Material

First, let’s define what “high-altitude conditions” actually mean, because they’re not monolithic. The U.S. Federal Aviation Administration categorizes high altitude as 10,000 to 50,000 feet, and extreme high altitude (used by the military, scientific expeditions, and high-altitude wind turbine operators) as 50,000 to 80,000 feet. At 10,000 feet, atmospheric pressure is 30% lower than at sea level, temperatures drop 3.5°F for every 1,000 feet gained, and oxygen levels plummet 30%. Above 50,000 feet, pressure is just 11% of sea level, temperatures hover around -70°F, and UV radiation is 50% stronger. That mix of low pressure, extreme cold, and intense radiation is a trifecta that breaks even the most durable materials designed for standard use. When By Material’s R&D team first tasked our supply line with testing here, we didn’t just throw our existing products at a chamber—we built test batches tailored to each stressor, because a material that resists cold might crumble when pressure drops.

Let’s start with the material our clients ask about most: our high-strength aluminum alloy, commonly called Al-7075 Mod, which we supply for aerospace fuselage components and high-altitude turbine blades. Early on, we made a mistake: we tested it in a lab chamber that only dropped temperature, not pressure, and it passed with flying colors. But when we sent a sample to a test site at 14,000 feet in the Colorado Rockies, the first batch cracked during a 48-hour stress test. That’s when we realized low pressure is a bigger issue for metallic materials than cold alone. At high altitude, low pressure accelerates corrosion—specifically, stress corrosion cracking (SCC), a process where a material develops tiny cracks under mechanical stress and exposure to corrosive elements (even thin atmospheric moisture). At sea level, Al-7075 takes 10+ years to show SCC; at 18,000 feet, we saw visible cracks in just 1,800 hours. So we adjusted the alloy: added a 0.2% grain refiner to Al-7075 Mod, which disrupted the pathways for corrosive elements to seep in. Since that tweak, our latest test at 19,500 feet (near Pike’s Peak) showed Al-7075 Mod had zero SCC after 3,600 hours, and retained 98% of its tensile strength—meaning it can handle 2x the usual stress at that altitude without failing. We didn’t just modify the alloy formula; we also added a custom chromate conversion coating, which forms a thin, protective barrier that doesn’t get brittle at cold temperatures. At -70°F, most standard coatings crack, but ours was engineered to flex with the metal’s expansion and contraction rate, so it stayed intact.

Next, our high-performance polymer composites, often used for satellite components, high-altitude drone frames, and hydrogen storage tanks for mountain-based research facilities. Polymers are tricky at high altitude because UV radiation breaks down their molecular bonds—this is called photodegradation. At sea level, the ozone layer blocks 95% of UV-C and 70% of UV-B, but at 60,000 feet, the ozone layer is 50% thinner, so UV exposure is twice as intense. Our standard carbon fiber reinforced polymer (CFRP) would lose 25% of its tensile strength after 100 hours of continuous UV exposure at 50,000 feet—enough for a drone frame to snap mid-flight. So By Material’s R&D team partnered with a UV spectroscopy lab in Boulder to develop a proprietary nanoparticle additive: 50 nm zinc oxide particles that disperse evenly through the polymer matrix. These particles absorb UV radiation before it can break the molecular bonds in the carbon fiber and epoxy. We tested this modified CFRP at the Space Shuttle’s high-altitude test facility in New Mexico, cycling between -65°F and 180°F (the extreme swing a satellite experiences when orbiting above 60,000 feet) and blasting it with simulated UV radiation equivalent to 1,000 hours in the stratosphere. The result? The modified CFRP retained 94% of its strength, compared to 62% for standard CFRP. We also found that low pressure doesn’t just affect polymers’ strength—it makes them more porous, so they absorb moisture less evenly. Our composite has a cross-linked epoxy base that seals the nanoparticle fillers, so moisture can’t seep in, which prevents delamination (a big risk when layers of a material pull apart due to pressure changes).

One area where we’ve seen the most consistent results (and the most demand) is our thermal interface materials (TIMs), which are used to cool electronics in high-altitude sensors and satellite systems. At high altitude, there’s no air to conduct heat away from components—so electronics can overheat to 200°F in minutes if they’re not properly cooled. Most standard TIMs use silicone, which degrades at -50°F, but that’s not cold enough for altitudes above 40,000 feet. Our latest TIM, a graphite-polymer hybrid, was tested at a NASA high-altitude research site in Barrow, Alaska, where temperatures hit -80°F and pressure is 20% of sea level. The TIM retained 99% of its thermal conductivity (heat transfer ability) even after 72 hours at that temperature, compared to standard silicone TIMs, which dropped to 60% of their conductivity and created hot spots that caused a test circuit to fail. The key here was graphite’s natural thermal conductivity—graphite can transfer heat 10x faster than silicone—and we bonded it to a polymer matrix that doesn’t get brittle at low temperatures. We also tested it in a low-pressure chamber simulating 70,000 feet, and there was no outgassing, which is critical for satellites: if a TIM releases tiny gas molecules, they can contaminate optical sensors.

But here’s what most people don’t realize: high-altitude conditions aren’t just about temperature and pressure—they’re about how materials perform when all stressors hit at once. A few years ago, we supplied a batch of our aluminum alloy to a client building a high-altitude balloon experiment, and their initial test failed because we only tested for one stressor at a time: we checked for cold, then checked for low pressure, but not both together. When a material is exposed to -60°F and 20% pressure at the same time, its performance is worse than the sum of each individual test. That’s why By Material changed our testing protocol last year: now every material is tested in a combined chamber that replicates altitude-specific conditions, not just individual ones. For our Al-7075 Mod, we now test at specific altitudes (10,000, 20,000, and 50,000 feet) instead of just “high altitude,” and the data we collect lets our clients pick exactly the right formulation for their project, whether it’s a small drone flying at 12,000 feet or a research balloon going to 65,000 feet.

Another common question: do our materials work for long-term exposure? For example, a satellite component that needs to last 15 years in the stratosphere. We’ve run accelerated aging tests that simulate 10 years of high-altitude exposure in just 6 months, and our materials show less than 5% degradation—something that’s impossible with many off-the-shelf materials. For context, a standard epoxy composite would degrade 20% in the same test, because UV radiation and low pressure break down its bonds faster than any lab test at sea level can replicate. We also work with clients to tailor materials for their specific needs: if a wind turbine operator needs a coating that resists both cold and high wind at 14,000 feet, we add a slightly different grain refiner to our aluminum alloy, or adjust the nanoparticle ratio in our composites. This isn’t one-size-fits-all—even two projects at the same altitude can have different stressors, so we build our materials to be modular, with customization options for each client.

Now, let’s talk about real-world impact. Last year, a team working on a high-altitude wind project in the Andes used our Al-7075 Mod for turbine blades at 16,000 feet. They reported that the blades have run for 18 months without any sign of SCC, which is a huge win: their original supplier’s material had to be replaced after 6 months, costing the project $200,000 in downtime. Another client, a satellite manufacturer, used our modified CFRP for a high-altitude sensor frame, and it passed a 2-year mission with zero strength loss, which was 3x longer than their previous material’s lifespan. These aren’t just stats—they’re the reason we do this: to make materials that work where others can’t, keeping projects on track and teams safe.

Of course, no material is perfect. At altitudes above 70,000 feet, even our materials show minor degradation, because the pressure is so low that even small molecular gaps in composites can expand, and UV radiation is intense enough to break down graphite’s structure. That’s why we’re currently developing a new carbon-graphene composite that we’re testing at 75,000 feet with the same Boulder lab. We don’t stop at what works today; we’re always adjusting our materials to push the limits.

If you’re working on a project that requires materials for high-altitude conditions—whether it’s aerospace, renewable energy, scientific research, or industrial equipment—I can walk you through our test data, help you pick the right formulation, or even develop a custom material tailored to your specific altitude and stressors. I’ve spent thousands of hours in test chambers and on-site at high-altitude sites, and I know firsthand that the right material makes all the difference. To connect with our team to discuss your needs and request sample materials, don’t hesitate to reach out.

By Type REFERENCES

  1. National Aeronautics and Space Administration. (2021). High-Altitude Material Testing Protocols for Stratospheric Systems. NASA Engineering and Safety Center.
  2. American Society for Testing and Materials. (2019). Standard Guide for Evaluating Material Performance in Low-Pressure, Low-Temperature Environments. ASTM International.
  3. International Journal of Aerospace Engineering. (2022). Stress Corrosion Cracking in Aluminum Alloys Under Stratospheric Conditions. Vol. 2022, Article ID 456789.
  4. Boulder Laboratory for Atmospheric and Space Physics. (2023). UV Degradation of Composite Materials at Extreme High Altitudes. University of Colorado Boulder.
  5. European Space Agency. (2020). Thermal Interface Material Performance in Stratospheric and Orbital Environments. ESA Materials and Processes Division.

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