The Cassini-Huygens spacecraft was launched by NASA on October 15, 1997 from Cape Canaveral Air Force Station in Florida. It took the spacecraft about seven years to reach the rings of Saturn and the many moons Cassini-Huygens will explore. During those seven years, only the Cassini spacecraft circuitry was "awake" and operating, while the Huygens space probe was "sleeping," waiting to arrive at the destination it was designed and constructed to explore. On July 1, 2004 the spacecraft reached the sixth planet from the sun, and is currently studying Saturn and the surrounding moons.
AVX Glass capacitors played a vital role in the wake up circuitry and deployment of the Huygens space probe. Glass capacitors facilitated the separation of the probe from the Cassini spacecraft on December 25, 2004, and allowed the probe to begin a 21-day trip to the surface of Titan, Saturn’s largest moon. On Huygens’ descent to the surface of Titan, a CYR10 glass capacitor enabled Huygens’ central computer to "wake up" from its seven-year slumber to take readings and measurements of Titan’s atmosphere and images of the surface floor.
The ultra-stable glass capacitors are also currently being utilized in communication and control functions of the Cassini spacecraft. Glass capacitors have been used for many functions of the space program from the early stages of the Mercury projects to present day Space Shuttles, space probe Voyager, Magellan, Galileo, the Mars Exploration rover, the Cassini-Huygens spacecraft and many more satellite programs. The European Space Agency (ESA) also uses glass capacitors in many of their programs. Most applications are mission critical such as wake up and deployment circuits, control circuitry, receiver link circuitry and sensors. In these applications, the capacitor must be able to withstand high shock environments, large thermal cycles and a variety of radiation environments in addition to having to be dormant/unused for a variable amount of time prior to the mission (e.g. Huygens space probe).
NASA uses multilayer glass dielectric capacitors because they exhibit unique electrical properties in addition to superior reliability in harsh environments. The fused monolithic construction of the glass dielectric capacitor provides a high Q factor and a low dissipation factor that changes little with frequency and temperature excursions. This, coupled with a low, retraceable, extended range temperature coefficient ensures stable, reliable, and repeatable electrical performance, regardless of the capacitors’ environment. Glass capacitors also exhibit zero piezoelectric noise, have zero voltage coefficients regardless of age or style, and exhibit very low dielectric absorption thus allowing their use in sample and hold circuitry.
CYR10 and CYR15 devices are designed to withstand extremely high and low temperatures and exposure to radiation. The unique materials and construction techniques used in the manufacturing of glass capacitors make them highly resistant to nuclear radiation, voltage breakdown and high operating temperatures, all vital for the sever conditions of space exploration.