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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.
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.
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.
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.

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Electric Propulsion References

  • 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.