Abstract: Some embodiments of the invention include a thruster system comprising a thruster and a pulsing power supply. The thruster may include a gas inlet port; a plasma jet outlet; and a first electrode. In some embodiments, the pulsing power supply may provide an electrical potential to the first electrode with a pulse repetition frequency greater than 10 kHz, a voltage greater than 5 kilovolts. In some embodiments, the pressure downstream from the thruster can be less than 10 Torr. In some embodiments, when a plasma is produced within the thruster by energizing a gas flowing into the thruster through the gas inlet port, the plasma is expelled from the thruster through the plasma jet outlet.

Abstract: A tool for assisting a worker in removing and reattaching brake springs includes an elongated shaft having an upper end and a lower end. Axially extending from the upper end is a tapered neck with a flattened stem extending therefrom. At a distal end of the stem is a C-shaped gripping member for grasping a brake spring. By holding the shaft, a worker can secure the C-shaped gripping member about the spring. The S-cam can be used as a fulcrum for the shaft, allowing the spring to be expanded as necessary for removal or attachment. The shaft may also include a light for illuminating dimly lit work areas.