Space Thruster Based on Inertial Electrostatic Confinement Benjamin A. Ulmen, Guilherme Amadio, Hugo Leon, George Chen, William W. Matisiak, Paul Keutelian, George H. Miley Introduction Theory of Operation

First Page		Document Content
Date: 2010-01-20 18:11:48 Physics Ion thruster Hall effect thruster Inertial electrostatic confinement Plasma Ion source Electrostatic ion thruster Electrically powered spacecraft propulsion Spacecraft propulsion Aerospace engineering Propulsion		Space Thruster Based on Inertial Electrostatic Confinement Benjamin A. Ulmen, Guilherme Amadio, Hugo Leon, George Chen, William W. Matisiak, Paul Keutelian, George H. Miley Introduction Theory of Operation Add to Reading List Source URL: fti.neep.wisc.edu Download Document from Source Website File Size: 1,38 MB Share Document on Facebook

	O K L A H O M A S T A T E U N I V E R S I T Y SCHOOL OF ELECTRICAL AND COMPUTER ENGINEERING SCHOOL OF MECHANICAL AND AEROSPACE ENGINEERING ECEN/MAE 5713 Linear Systems Spring 2011 DocID: 1vrGX - View Document
	The motion formalism for flexible multibody dynamics: A practical introduction Olivier A. Bauchau, Alfonso Callejo and Valentin Sonneville Department of Aerospace Engineering University of Maryland College Park, MD, USA DocID: 1vql6 - View Document
	LIST OF MINORS 1. AEROSPACE ENGINEERING MINOR DocID: 1vodZ - View Document
	We have comprehensive expertise in the following areas: For more than 15 years we, Astround Feinwerktechnik Adlershof GmbH, are developing, engineering and testing in the fields of aerospace, basic research and optics. DocID: 1vfzn - View Document
	Autonomous Quadrotor for the 2011 International Aerial Robotics Competition Daniel Ellis M.S.E. Aerospace Engineering 2012 Thomas Brady M.S.E. Aerospace Engineering 2012 DocID: 1vaZZ - View Document