MIT Scientists Developing Electrically-Controlled Rocket

March 10, 2009
Earth-orbiting satellites must occasionally be nudged to stay on the correct path. MIT scientists are developing a new electrically-controlled rocket that could make this and other spacecraft maneuvers much less costly

Earth-orbiting satellites must occasionally be nudged to stay on the correct path. MIT scientists are developing a new electrically-controlled rocket that could make this and other spacecraft maneuvers much less costly. MIT's new system, called the Mini-Helicon Plasma Thruster, is much smaller than other rockets of its kind and runs on gases that are much less expensive than conventional propellants. As a result, it could slash fuel consumption by 10 times that of conventional systems used for the same applications, said Oleg Batishchev, a principal research scientist in the Department of Aeronautics and Astronautics and leader of the work.

The propulsion systems currently used for maintaining a satellite's orbit, pushing a spacecraft from one orbit to another, and otherwise maneuvering in space rely on chemical reactions that occur within the fuel, releasing energy that ultimately propels the object. However, chemical rockets are expensive largely due to the amount of fuel they use. As a result, engineers have been developing alternative, non-chemical rockets. In these, an external source of electrical energy is used to accelerate the propellant that provides the thrust for moving a craft through space. Such non-chemical rockets have been successfully used by NASA and the European Space Agency in missions including NASA's Deep Space 1, which involved the flyby of a comet and asteroid.

But the field is still relatively new, and these advanced rockets are one focus of the MIT Space Propulsion Laboratory (SPL). "The Mini-Helicon is one exciting example of the sorts of thrusters one can devise using external electrical energy instead of the locked-in chemical energy. Others we in the SPL work on include Hall thrusters and Electrospray thrusters. This area tends to attract students with a strong physics background, because it sits at the intersection of physics and engineering, with ample room for invention," said Manuel Martinez-Sanchez, director of the SPL and a professor in the Department of Aeronautics and Astronautics.

The Mini-Helicon is the first rocket to run on nitrogen, the most abundant gas in our atmosphere. It was conceived through work with former astronaut Franklin Chang-Diaz ScD '77 on a much larger, more powerful system developed by Chang-Diaz. Batishchev's team did a theoretical analysis showing that the first of three parts of the larger rocket could potentially be used alone for different applications. Since then, 12 MIT students have worked on the Mini-Helicon, resulting in one PhD and four masters' theses to date. Batishchev notes, however, that it could be years before the technology can be used commercially, in part due to certification policies through NASA and other agencies.

The Mini-Helicon has three general parts: a quartz tube wrapped by a coiled antenna, with magnets surrounding both. The gas of interest is pumped into the quartz tube, where radio frequency power transmitted to the gas from the antenna turns the gas into a plasma, or electrically charged gas. The magnets not only help produce the plasma, but also confine, guide, and accelerate it through the system. "The plasma beam exhausted from the tube is what gives us the thrust to propel the rocket," Batishchev said.

He noted that the exhaust velocity from the new rocket is some 10 times higher than the velocity from the average chemical rocket, so much less propellant is needed.

Work continues. Batishchev notes that last summer, for fun, his team built a plasma rocket based on a glass bottle (a stand-in for the quartz tube) and an aluminum can (the radio-frequency antenna), both of which previously held soft drinks. It worked. "This shows that this is a robust, simple design. So in principal, an even simpler design could be developed," he said.

This work was funded by the Air Force Research Laboratory.

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