Engineers on a constant quest to reduce the weight of space vehicles will look to next-generation materials, replacing metals with fabrics that provide the same thermal and radiation protection while giving the spacecraft a fighting chance of survival outside the Earth’s atmosphere. This article will address current materials used, as well as a new generation of high-performing materials.
Most satellites and space vehicles such as the International Space Station (ISS) and the Space Shuttle travel in what is known as Low Earth Orbit (LEO), which is considered to be an orbital band between 100 – 1240 miles above sea level. The most common orbits, however, are between 200 – 250 miles because less energy is required to launch and communications distances are more favorable.
The LEO area is filled with elements we don’t find on earth such as atomic oxygen. Atomic oxygen is highly unstable, particularly in this environment, and is a chief source of the degradation of exposed surfaces in space vehicles. At this altitude there is also a high concentration of debris and particles traveling at extremely high speeds relative to that of the vehicle. Even a particle the size of a marble can cause significant damage to a space vehicle.
In addition to the above affects, a spacecraft is also subject to extreme temperature fluctuations as it orbits the Earth. Different parts of the spacecraft may see very hot or cold temperatures during some or all of its “day,” which can list minutes or hours depending on its orbit. The sun’s radiation combined with the Earth’s magnetic fields create a hostile environment for spacecraft systems and instruments, which must still perform flawlessly for the spacecraft’s working life.
Thermal and radiant energy and TPS The sun emits energy in the form of radiation that we on Earth feel as warmth or thermal energy. Our atmosphere protects us from receiving the sun’s radiation while retaining enough of it to keep us warm. Spacecrafts operating outside of the atmosphere don’t have that protection. They rely on specialized materials referred to as its Thermal Protection System (TPS) to perform this function.
In addition, thermal energy is generated by internal components of a satellite such as batteries, transmitters, computers and other devices. This thermal energy must be emitted so it does not damage the components. Thermal management control systems are an integral part of the design of a satellite. Techniques include passive and active systems. Some active techniques include the use of heaters or refrigerators. Multi-Layer Insulation (MLI) and radiators are other passive techniques.
MLI is a type of thermal protection system (TPS) used on spacecraft, launch vehicles, The Space Shuttle and the International Space Station. MLI insulation is typically found in blanket form and consists of films and fabric constructions ranging from five to forty layers as well as highly specialized tapes used in edge binding and cable wrapping.
The goal of the TPS is to maintain equipment temperatures in very specific ranges during the mission life. Keeping this temperature range allows all electronic equipment, instruments and systems to function in their optimal operating conditions. The most notable example may be the ISS, which has been continuously inhabited since November 2, 2000.
David Patterson, known for his pioneering research that led to RAID, clusters and more, is part of a team at UC Berkeley that recently made its RISC-V processor architecture an open source hardware offering. We talk with Patterson and one of his colleagues behind the effort about the opportunities they see, what new kinds of designs they hope to enable and what it means for today’s commercial processor giants such as Intel, ARM and Imagination Technologies.