1. References
Emsellem, 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
ml
LaPointe, 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.html
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.HTM
Oleson, 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: NASA's 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. 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 Consulted
Aerojet 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
ml
Grayson, J., & Ferguson, K. (2006). Solar system commuter trains: MagBeam plasma
propulsion. Analog Science Fiction & Fact, 126(6), 40.
3. Kuharski, R. A., & Mandell, M. J. (2005). Ion engine neutralizer erosion in lan and
space
LaPointe, 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.html
Marcuccio, 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.HTM
Oleson, 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: NASA's 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. 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 millennium's 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.