Microsoft Word - TimSTAIF2005.doc - Ion cyclotron resonance - Document - PDFSEARCH.IO

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Date: 2009-07-29 16:12:14 Aerospace engineering Propulsion Variable Specific Impulse Magnetoplasma Rocket Ion thruster Plasma propulsion engine Plasma Helicon Electron cyclotron resonance Specific impulse Spacecraft propulsion Physics Plasma physics		Microsoft Word - TimSTAIF2005.doc Add to Reading List Source URL: vasimr.net Download Document from Source Website File Size: 421,56 KB 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
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	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