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Date: 2011-04-18 19:40:42 Spacecraft propulsion Ion thruster Hall effect thruster Mars sample return mission Mars Direct Dawn Sample return mission Exploration of Mars Electrically powered spacecraft propulsion Spaceflight Space technology Spacecraft		Add to Reading List Source URL: ia600605.us.archive.org Download Document from Source Website File Size: 5,31 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
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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