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Date: 2015-06-25 02:44:56 Spacecraft propulsion Spaceflight Propulsion Electromagnetism Hall-effect thruster Ion thruster Thruster Electrically powered spacecraft propulsion Magnetoplasmadynamic thruster NEXT Plasma propulsion engine Colloid thruster		<333074685F495354535F93FA92F6955C2D7765628C668DDA977089C18D482E706466> Add to Reading List Source URL: www.ists.or.jp Download Document from Source Website File Size: 148,98 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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	NATICK, MA, JUNE 1, 2015 Today satellite propulsion firm Busek Co. Inc. confirmed the shipment of its first miniature electrospray small satellite thrusters to NASA. The modular, 100 micronewton-class thrusters enable ne DocID: 1qLgY - View Document
	MITSUBISHI ELECTRIC RESEARCH LABORATORIES http://www.merl.com MPC for Coupled Station Keeping, Attitude Control, and Momentum Management of Low-Thrust Geostationary Satellites DocID: 1qJwc - View Document
	Special Issue on IEEE Transactions on Plasma Science Plasma Propulsion (Scheduled for DecemberPlasma propulsion is a very rapidly growing area of plasma science and technology. Experiments, modeling, and computer DocID: 1qlNr - View Document