Rocket propellant - Document - PDFSEARCH.IO

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Date: 2012-04-19 10:27:18 Aerospace engineering Rocket propulsion Rocket engines Rocket-powered aircraft Rocketry Specific impulse Rocket Propellant Engine Space technology Spacecraft propulsion Transport		Add to Reading List Source URL: cs.astrium.eads.net Download Document from Source Website File Size: 1,73 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