dc.contributor.author | Martinez-Sanchez, Manuel | en_US |
dc.coverage.temporal | Spring 2004 | en_US |
dc.date.issued | 2004-06 | |
dc.identifier | 16.522-Spring2004 | |
dc.identifier | local: 16.522 | |
dc.identifier | local: IMSCP-MD5-208ce7c5579daeed4a1d1dbb42d77677 | |
dc.identifier.uri | http://hdl.handle.net/1721.1/100855 | |
dc.description.abstract | Space Propulsion begins with a review of rocket propulsion fundamentals. The course then proceeds into advanced propulsion concepts, ranging from chemical to electrical engines. Propulsion system selection criteria and mission analysis are introduced. The bulk of the semester is devoted to the physics and engineering of various engine classes, including electrothermal, electrostatic and electro-magnetic. Specific topics include arcjets, ion engines, Hall thrusters and colloid thrusters. | en_US |
dc.language | en-US | en_US |
dc.rights.uri | Usage Restrictions: This site (c) Massachusetts Institute of Technology 2016. Content within individual courses is (c) by the individual authors unless otherwise noted. The Massachusetts Institute of Technology is providing this Work (as defined below) under the terms of this Creative Commons public license ("CCPL" or "license") unless otherwise noted. The Work is protected by copyright and/or other applicable law. Any use of the work other than as authorized under this license is prohibited. By exercising any of the rights to the Work provided here, You (as defined below) accept and agree to be bound by the terms of this license. The Licensor, the Massachusetts Institute of Technology, grants You the rights contained here in consideration of Your acceptance of such terms and conditions. | en_US |
dc.rights.uri | Usage Restrictions: Attribution-NonCommercial-ShareAlike 3.0 Unported | en_US |
dc.rights.uri | http://creativecommons.org/licenses/by-nc-sa/3.0/ | en_US |
dc.subject | space propulsion | en_US |
dc.subject | rocket propulsion | en_US |
dc.subject | spacecraft propulsion requirements | en_US |
dc.subject | propulsion | en_US |
dc.subject | space mission analysis | en_US |
dc.subject | hydrazine | en_US |
dc.subject | monopropellant thrusters | en_US |
dc.subject | bipropellants | en_US |
dc.subject | solid propellant | en_US |
dc.subject | arcjets | en_US |
dc.subject | ion engines | en_US |
dc.subject | hall thrusters | en_US |
dc.subject | electromagnetic plasma acceleration | en_US |
dc.subject | pulsed plasma thrusters | en_US |
dc.subject | colloid thrusters | en_US |
dc.subject | FEEP thrusters | en_US |
dc.subject | Space vehicles--Electric propulsion systems | en_US |
dc.title | 16.522 Space Propulsion, Spring 2004 | en_US |
dc.title.alternative | Space Propulsion | en_US |