May 032011
 
www.cubesat.org

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An electric propulsion technology for miniature satellites aims to give them more mobility — and may eventually allow them to take on deep-space missions.

Right now, 10 to 15 Rubik’s Cube-sized satellites are orbiting high above Earth. Known as cube satellites, or “CubeSats,” the devices help researchers conduct simple space observations and measure characteristics of Earth’s atmosphere. One advantage is that they are relatively cheap to deploy: While launching a rocket may cost between $50 million and $300 million, a CubeSat can “piggyback” onto a large rocket platform at an additional cost of as little as $40,000. But their small size also means they lack on-board propulsion systems, which is why they generally remain locked to a particular orbit.

That could soon change, however. Paulo Lozano, the H.N. Slater Assistant Professor of Aeronautics and Astronautics at MIT, is designing a tiny propulsion system that could allow the satellites, which weigh about a kilogram and are used for tasks that don’t require precise orbit control, to travel great distances and perform more serious tasks, such as searching for planets outside our solar system. The technology, which is based on the process of extracting and accelerating charged ions, or atoms that have gained or lost an electron, could make CubeSats much more useful for organizations or countries that until now have had limited access to space.

For decades, the only way to get objects into space from Earth — and then propel them through space — was to use chemical propulsion systems. But the systems require a lot of propellant, or fuel, and haven’t been miniaturized to the scale appropriate for a CubeSat. By changing the design from chemical to electric, and to one that relies on a simple power supply, Lozano has created a system that produces more efficient thrust — the force created when mass is accelerated in a certain direction — than that produced by a chemical-based system, which produces a low thrust per gram of propellant. About the size of a computer chip, the mini-thruster design also overcomes the size constraints of chemical propulsion and other forms of electric propulsion because it does not require a bulky chamber to burn (chemical) or extract ions from (electric) the propellant. Although other electric propulsion systems have been developed, Lozano’s is considered superior because it uses only one power supply.

With funding from the Air Force Office of Scientific Research, Lozano has been developing the technology to make the mini-thruster. The Air Force and other government agencies are interested in using CubeSats that can move between different orbits in space, and more specifically, that have the propulsion required to reenter Earth’s atmosphere and destroy themselves at the end of their mission (thereby keeping them from becoming “space junk”). The thruster design requires that the total volume of the propulsion system be less than 10 percent of the CubeSat.

“The goal is to have a space engine that leaves plenty of room for the payload, or cargo, of the CubeSat,” Lozano said. Certain missions require chemical propulsion, such as a trip to the moon, because in order to land on the moon’s surface, the amount of force from the engine must be at least equal to the weight of the lander, a value that Lozano said is generally “way too high” for electric propulsion engines. But chemical-based systems are severely limited by the fact that the vehicle mass must be made mostly of propellant, which leaves little room for the payload. Quite often the propellant must also be stored in a pressurized container with thick walls and pipes, further limiting the payload size. Although other electric propulsion systems exist, they require a pressurized container to store the propellant.

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