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Glass Capacitor Chosen by NASA for Over 50 Years


Courtesy NASA/JPL-Caltech

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.

History

The US military began seeking a substitute for imported mica dielectric during World War II in order to make the U.S. capacitor industry independent of foreign supply. For centuries glass had been recognized as an excellent insulator, and a special composition with dielectric properties similar to those of mica was developed. The first issue was developing a process to form the glass into very thin ribbon, and then manufacturing a capacitor in large quantities using this glass dielectric technology.

 

Before glass capacitors reached significant production, Germany surrendered and the war had ended. With the threat to the mica supply removed, pressure to expand production diminished until the electrical advantages of glass dielectrics vs. mica was better documented. At the time, the majority of designs that required glass capacitors were military applications. Because mica capacitors were available in tremendous quantities at much lower prices, commercial acceptance of glass capacitors was relatively insignificant, primarily because mica capacitors were available in tremendous quantities at much lower prices.

 

Additional research and development resulted in the marketing of the CY-style capacitor in 1951. Its stability, low noise characteristics and small size led to immediate and widespread recognition by the electronics industry — military as well as commercial.

 

Further material and ‘glass fusion process’ development efforts yielded the ultra-reliable CYF series of capacitors.

 

In less than three years, the CYFR capacitor was being mass-produced with unprecedented reliability. CYFR capacitors displayed high accuracy, reliability, stability, fire control and guidance elements for the major military and commercial programs.

 

NASA’s space programs have used glass capacitors for many missions over the past 50 years.

Construction

Figure 1. Axial Glass Capacitor Construction

Glass dielectric capacitors are unique due to their novel material systems and their simple construction. There are only three materials in axial leaded capacitors: glass dielectric and case, aluminum foil electrodes, and wire leads (see figure 1). The minimized material system and its simple construction enable these hermetically sealed capacitors to perform in harsh conditions such as shock, vibration, moisture, salt spray and extreme heat and cold. With minor additional design and processing these capacitors can be configured to exhibit extremely high insulation resistance, Coulombic shielding and extreme vibration capability. Glass capacitors are also available in radial configuration, and surface mount packages are under development.

Characteristics

Figure 2. Glass Capacitor Temperature Coefficient vs Temperature
Figure 3. Capability to operate in neutron field intensity

Electrically glass capacitors are the ideal "loss-less" capacitors. All CY series glass capacitors have a temperature retraceability of capacitance of ±5ppm (see figure 2). The retraceability is independent of age of the part or voltage applied.

 

Glass capacitors also exhibit other electrical performance characteristics critical to long-term spacecraft performance. Among those characteristics are a high level of nuclear radiation resistance, zero piezoelectric noise, ultra low dielectric absorption and an ability to operate reliably from –188° to +200° Centigrade. A general illustration of glass capacitors’ radiation performance is shown in figure 3.

 

Glass Capacitors: Mission Control

Courtesy NASA/JPL-Caltech

When NASA’s Mars Exploration Rover, Spirit and its twin rover Opportunity, landed safely on the planet surface, glass capacitors in the mission critical Rover Lift Mechanism Actuator and Lander Pedal Actuator Circuits allowed the Lander to open and adjust its pedals. This action enabled the Rover lift mechanism to raise the Rover, so that its wheels could be deployed in order to drive on the Martian terrain. Glass capacitors were chosen because of their reliability in an application that was unpowered for years, then instantly required to turn on and function properly (space travel), and the reliability of operating in harsh and severe conditions (Mars). The glass capacitors used in the Mars Rover mission did not experience any aging effects over time or through a variety of environments such as temperature cycling and radiation fields. They behaved in a low noise fashion so sensor circuitry data could be accurately interpreted and acted on.

 

The Tracking and Data Relay Satellite System (TDRSS) is a communication signal relay system that provides tracking and data acquisition services between low earth orbiting spacecraft and NASA control and/or data processing facilities. The system allows nearly continuous command and telemetry communications between ground control centers and unmanned, automated research and applications spacecraft orbiting thousands of miles above the Earth. The TDRSS permits communications with spacecraft during at least 85 percent of their orbit, without the satellite system acting as a space-based relay, communications with satellites could be accomplished only when the spacecraft are in sight of a ground station, which is only 15 percent of an orbit. The TDRSS relies on glass capacitors for Doppler shift correction in the receiver circuitry. Glass capacitors allow the receiver to have better resolution and accuracy than ceramic capacitors. The stable electrical parameters with total dose radiation coupled with zero aging and lot-to-lot temperature retraceability allowed glass to be an ideal choice for the receiver front-end circuitry. Glass capacitors help enable TDRSS receiver to maintain its center frequency and correct for frequency shift effects due to spacecraft motion.

Next Generation Space Grade Components

The future of glass capacitors is as bright as the past. The European Space Agency (EAS) will be using glass capacitors in the LISA (Laser Interferometry Space Antenna) Pathfinder mission set to launch in 2006 or 2007. The LISA mission will be testing Einstein’s theory of General Relativity in order to gain more knowledge about the universe for future missions. Glass capacitors were again chosen for the LISA spacecraft because of the reliability and long-term consistent performance. Glass capacitors will also be used in several other ESA and NASA missions in the near future including advanced LISA missions.

 

Glass capacitors continue to be an anchor product that offers high reliability in spacecraft designs. Trends such as ion propulsion should help increase existing glass capacitor usage in spacecraft propulsion circuits. Zero aging effects and long term stability are critical to successful spacecraft operation – glass capacitors meet those requirements.

 

Programs have been created to offer glass chip capacitors in V case tantalum capacitor packages. These devices are expected to exhibit high stability, low noise characteristics and zero aging rates.

 

The expansion of spacecraft products includes radiation-resistant multilayer varistors (MLVs), broadband high power filters (to save weight in spacecraft designs) and low inductance decoupling capacitors. Low inductance capacitors provide significant space and weight reduction on spacecraft designs.

Glass Capacitors – Alternative Applications

Glass capacitors are also used in other applications that are not spacecraft-related. Examples of these include jet engine sensors, medical monitoring systems, audio equipment, and high temperature oil exploration equipment. As word of the glass capacitors excellent thermal performance became more widespread, development teams were modifying spacecraft-grade capacitors for use in oil well logging circuitry. The Elevated Temperature (ET) series was introduced as a cost-reduced, high-reliability harsh environment component. These devices have an extended operating range of –75°C to +200°C with short exposures up to +250°C with no degradation. Glass capacitors are used in feedback and critical control circuitry on down hole oil well logging equipment. Their ability to deliver low noise, accurate and reliable performance is unmatched in environments that have repeated temperature cycles and high mechanical shock. Specifically, their low noise performance features have made then the ideal choice for phased array receiver front ends as well as gamma ray detector circuitry.

The functionality of a glass capacitor is what makes it so attractive to design engineers. Glass capacitors are rugged and reliable, and have never failed in a space mission.

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