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

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Date: 2016-07-28 14:45:51 Spacecraft propulsion Spaceflight Spacecraft Propulsion Busek Hall-effect thruster Ion thruster USA-221 Electrically powered spacecraft propulsion TacSat-2 Specific impulse Thruster		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 Add to Reading List Source URL: www.busek.com Download Document from Source Website File Size: 939,79 KB Share Document on Facebook

	The world’s first iodine gridded ion thruster featuring high performance and unprecedented efficiency for its size. Busek’s BIT-3 RF ion thruster is a missionenabling, iodine-fueled ion propulsion system scheduled fo DocID: 1sqrb - View Document
	Particle-in-cell investigation of the nonlinear saturation of Shear Alfv´ en Modes in hollow-q-proﬁle tokamaks Sergio Briguglio1, Gregorio Vlad1 , Fulvio Zonca1 , and Duccio Testa2 1 DocID: 1rsck - View Document
	SPACE Storable Propellant Busek test-fires tiny RF gridded-ion thruster for CubeSat apps, using ‘solid’ iodine as fuel DocID: 1rjBO - View Document
	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
	Busek’s family of barium-impregnated cathodes features extensive NASA heritage. The mechanical design builds off our BHC-1500 cathode successfully operated DocID: 1reea - View Document