fig8

Figure 8. Soft sensors for space environment applications. (A) Ceramic nanofiber flexible pressure sensor with high-temperature resistant characteristics. The device structure, a thermal image of the sensor that is tested at 370 °C, and the capacitance to pressure sensitivities for tests at 30, 370, and 30 °C after burning are displayed^[202]; (B) Triboelectric all-textile sensor array to monitor aerial pulse waves and respiratory signals and can be worn around the neck, as a wristband, fingerstall, or integrated into a sock^[203]. [All images (A and B) are licensed under CC BY 4.0. http://creativecommons.org/licenses/by/4.0/.]