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In the aerospace field, this Teflon high-temperature fabric is referred to as Beta cloth. It uses high-strength fiberglass fabric as the substrate, which is impregnated or coated on the outer layer with polytetrafluoroethylene (PTFE, i.e., Teflon). This combines the flexibility of the fabric with the extreme-environment inertness of PTFE.
According to Teflon high-temperature fabric manufacturers: In the multi-layer insulation system of extravehicular mobility units (EMUs), it serves as the outermost layer of the Thermal Micrometeoroid Garment (TMG), directly facing the vacuum, extreme temperature differentials, and micrometeoroids. It acts as the first physical and thermal barrier for the dozen or so inner layers of aluminized films.
Teflon high-temperature fabric can long-term withstand temperatures ranging from -200°C to +260°C, covering the harsh fluctuations of over 120°C on the sun-facing side of space and down to -160°C on the shadowed side. Its typically white surface effectively reflects solar radiation, significantly reducing heat absorption and maintaining internal temperature stability.
It acts like a tough, smooth skin, providing scratch resistance, tear resistance, and wear protection for the underlying extremely thin and easily damaged aluminized polyimide films. This ensures the integrity of the multi-layer vacuum insulation and prevents thermal failure caused by outer layer damage.
The extremely low coefficient of friction of the PTFE surface endows the outer fabric with non-stick, smooth characteristics. When astronauts bend their arms or torso joints, the layers do not impede movement or create tangles due to high friction, ensuring flexibility during extravehicular activities, as noted by Teflon high-temperature fabric manufacturers.
The fiberglass base fabric is inherently non-combustible, and the PTFE coating is flame-retardant and chemically extremely stable, capable of resisting erosion from strong oxidizing agents such as atomic oxygen in space. In the historically used pure-oxygen cabin environments, this flame retardancy and corrosion resistance were critical to astronaut safety.
The Apollo A7L lunar spacesuits extensively used Beta cloth for the outer layer, successfully withstanding the lunar surface's over 100°C temperatures, deadly lunar dust contamination (the smooth PTFE surface resists dust adhesion and is easy to clean), and micrometeoroid impacts. This validated its reliability across all terrains and temperature extremes.
On the spacesuits used for the Space Shuttle and the International Space Station, the outer layer has evolved into an Ortho-fabric blend. It is woven from expanded PTFE (Gore-Tex) fibers, Nomex, and Kevlar. At its core, it still relies on Teflon-based weatherability, dust resistance, and high-temperature tolerance, while incorporating other fibers to enhance strength and flame retardancy. It has become the ultimate outer armor that integrates thermal protection, mechanical protection, and motion assistance.
The above information is provided by Jiangsu OK New Material Technology Co., Ltd.
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