Electric Propulsion References

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Electric Propulsion References

  1. 1. ReferencesEmsellem, G. D. (2005). Development of high power electrodeless thruster No. IEPC-2005-156). Wilmington, DE: The Elwing Company.Foster, J. E., Haag, T., & Patterson, M. (2004). The high power electric propulsion (HiPEP) ion thruster No. TM-2004-213194). Glenn Research Center, Cleveland, Ohio: NASA.Golightly, G. (2000). Advanced projects map future of spaceflight. Retrieved December 10, 2006, from http://www.space.com/businesstechnology/technology/advanced_projects_000621.ht mlLaPointe, M. R., & Mikellides, P. G. (2001). High power MPD thruster development at the NASA glenn research center No. CR-2001-211114). Ohio Aerospace Institute, Brook Park, Ohio: NASA.Marcuccio, S. (1998). The FEEP principle. Retrieved November 28, 2006, from http://www.centrospazio.cpr.it/FEEPPrinciple.htmlMarcuccio, S., Gianelli, S., & Andrenucci, M. (1997). Attitude and orbit control of small satellites and constellations with FEEP thrusters No. IEPC-97-188). Cleveland, OH: Proceedings of the 25th Electric Propulsion Conference.Marrese-Reading, C., Polk, J., Mueller, J., & Owens, A. (2001). In-FEEP thruster ion beam neutralization with thermionic and field emission cathodes No. IEPC-01-290). Pasadena, CA: 27th International Electric Propulsion Conference.Mikellides, P. G. (2003). Pulsed inductive thruster (PIT): Modeling and validation using the MACH2 code No. CR-2003-212714). Arizona State University, Tempe, Arizona: NASA.Nowicki, A. (1999). Earth-to-orbit transportation. Retrieved December 10, 2006, from http://www.nas.nasa.gov/About/Education/SpaceSettlement/Nowicki/SPBI101.HTMOleson, S. R., & Sankovic, J. M. (2001). Advanced hall electric propulsion for future in- space transportation No. NASA/TM-2001-210676). Cleveland, Ohio: Glenn Research Center.Oleson, S., & Gefert, L. (2002). Mission advantages of NEXT: NASAs evolutionary xenon thruster No. TM-2002-211892)NASA.Sankaran, K., Cassady, L., Kodys, A. D., & Choueiri, E. Y. (2003). A survey of propulsion options for cargo and piloted missions to mars. Princeton, NJ: Princeton University.
  2. 2. Sengupta, A. (2005). Destructive physical analysis of hollow cathodes from the deep space 1 flight spare ion engines 30,000 hr life test No. IEPC-2005-026)NASA.Snyder, J. S., & Goebel, D. M. (2005). Results of a 2000-hour wear test of the NEXIS ion engine No. IEPC-2005-281) Works ConsultedAerojet delivers breakthrough engine for planetary exploration.(2006). PR Newswire, , n/ a.Beal, B. E. (2004). Clustering of hall effect thrusters for high-power electric propulsion applications. (Aerospace Engineering, University of Michgan).BREEZE, M. E. D. (2006, Sep 1). Lockheed to lead next era in space. Daily Breeze, pp. A.1.Emsellem, G. D. (2005). Development of high power electrodeless thruster No. IEPC-2005-156). Wilmington, DE: The Elwing Company.Emsellem, G. D. (2004). Electrodeless plasma thruster design characteristics and performances No. ESA SP-555). Wilmington, DE: Elwing Company.Fed: Aust scientist build new space engine to rival the best.(2006). AAP General News Wire, , 1.Foster, J. E., Haag, T., & Patterson, M. (2004). The high power electric propulsion (HiPEP) ion thruster No. TM-2004-213194). Glenn Research Center, Cleveland, Ohio: NASA.Foster, J. E., Haag, T., & Patterson, M. (2004). The high power electric propulsion (HiPEP) ion thruster No. TM-2004-213194). Glenn Research Center, Cleveland, Ohio: NASA.Golightly, G. (2000). Advanced projects map future of spaceflight. Retrieved December 10, 2006, from http://www.space.com/businesstechnology/technology/advanced_projects_000621.ht mlGrayson, J., & Ferguson, K. (2006). Solar system commuter trains: MagBeam plasma propulsion. Analog Science Fiction & Fact, 126(6), 40.
  3. 3. Kuharski, R. A., & Mandell, M. J. (2005). Ion engine neutralizer erosion in lan and spaceLaPointe, M. R., & Mikellides, P. G. (2001). High power MPD thruster development at the NASA glenn research center No. CR-2001-211114). Ohio Aerospace Institute, Brook Park, Ohio: NASA.Marcuccio, S. (1998). The FEEP principle. Retrieved November 28, 2006, from http://www.centrospazio.cpr.it/FEEPPrinciple.htmlMarcuccio, S., Genovese, A., & Andrenucci, M. (1997). FEEP microthruster technology status and potential applications. Turin, Italy: 48th International Astronautical Federation Congress.Marcuccio, S., Gianelli, S., & Andrenucci, M. (1997). Attitude and orbit control of small satellites and constellations with FEEP thrusters No. IEPC-97-188). Cleveland, OH: Proceedings of the 25th Electric Propulsion Conference.Marrese-Reading, C., Polk, J., Mueller, J., & Owens, A. (2001). In-FEEP thruster ion beam neutralization with thermionic and field emission cathodes No. IEPC-01-290). Pasadena, CA: 27th International Electric Propulsion Conference.Mikellides, P. G. (2003). Pulsed inductive thruster (PIT): Modeling and validation using the MACH2 code No. CR-2003-212714). Arizona State University, Tempe, Arizona: NASA.Nowicki, A. (1999). Earth-to-orbit transportation. Retrieved December 10, 2006, from http://www.nas.nasa.gov/About/Education/SpaceSettlement/Nowicki/SPBI101.HTMOleson, S. R., & Sankovic, J. M. (2001). Advanced hall electric propulsion for future in- space transportation No. NASA/TM-2001-210676). Cleveland, Ohio: Glenn Research Center.Oleson, S., & Gefert, L. (2002). Mission advantages of NEXT: NASAs evolutionary xenon thruster No. TM-2002-211892)NASA.Plihon, N., Chabert, P., & Raimbault, J. (2005). Helicon double layer thruster concept for high power NEP missions No. 18852/05/NL/MV)ESA.Sankaran, K., Cassady, L., Kodys, A. D., & Choueiri, E. Y. (2003). A survey of propulsion options for cargo and piloted missions to mars. Princeton, NJ: Princeton University.Science and technology: Sail of the century; space propulsion.(2005). The Economist, 375(8431), 85.
  4. 4. Sengupta, A. (2005). Destructive physical analysis of hollow cathodes from the deep space 1 flight spare ion engines 30,000 hr life test No. IEPC-2005-026)NASA.Snyder, J. S., & Goebel, D. M. (2005). Results of a 2000-hour wear test of the NEXIS ion engine No. IEPC-2005-281)Sovey, J. S., & Anderson, J. R. (1997). Development of an ion thruster and power processor for new millenniums deep space 1 mission No. TM-1997-113129)NASA.Webber, T. R. (2005, Nov 21). Ion propulsion ; how it works and where it will enable us to go on future space mssions. News Sentinel, pp. B.8.

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