VASIMR Performance Results

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Date: 2010-08-05 10:09:12 Aerospace engineering Propulsion Variable Specific Impulse Magnetoplasma Rocket Plasma Ion source Helicon Double layer Hall effect thruster Specific impulse Spacecraft propulsion Plasma physics Physics		VASIMR Performance Results Add to Reading List Source URL: www.adastrarocket.com Download Document from Source Website File Size: 2,55 MB Share Document on Facebook

	Busek’s low power Hall Effect Thrusters span between 100 and 1500 W Typical low power Isp range: 1100 to 2000 s Busek Co. has been developing next generation high performance electric propulsion systems. Our family of DocID: 1rhLc - View Document
	Improved Hall Thrusters Fed by Solid Phase Propellant Mg is more abundant than Xe and provides a much higher specific impulse. John H. Glenn Research Center, Cleveland, Ohio H DocID: 1qWbV - View Document
	Efficient and high-performance propulsion system designed for use with xenon and iodine propellants. Busek’s BHT-8000 is a 8kW (nominal) Hall Effect thruster with state-of-the-art center mounted cathode and performance DocID: 1q4E8 - View Document
	High performance and mature propulsion system with flight heritage, and the first US Hall effect thruster in space. The BHT-200 is a high performance and mature propulsion system with flight heritage aboard the Air Force DocID: 1q2O0 - View Document
	Efficient and high-performance propulsion system designed for use with xenon and iodine propellants. Busek’s BHT-1500 is a 2kW-class Hall Effect thruster with innovative center-mounted cathode. The center-mounted DocID: 1q1yV - View Document