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ADVANCES IN APPLIED PLASMA SCIENCE 2011

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Liquid Propellant, Advances in Applied Plasma Science, Vol. 4, pp. 127-132, 2003. [6] Scharlemann, C.A.; Investigation of thrust mechanisms in a water fed pulsed plasma thruster, Thesis (Ph.D.)-The Ohio State University, 2003. Publication Number: AAI3119256; ISBN: 9780496666546; Source: Dissertation Abstracts International, Volume: 65-01, Section: B, page: 0303; 187 p. [7] Koizumi, H., Kawazoe, Y., Komurasaki, K., Arakawa, Y.; Effect of solute mixing in the liquid propellant of a pulsed plasma thruster, Vacuum Journal, Vol. 80, #11-12, pp.1234- 1238. [8] Mikellides, P. G. and Turchi, P. J.; Modeling of Late-time Ablation in Teflon Pulsed Plasma Thrusters, 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 1-3, Lake Buena Vista, 1996. [9] Böhrk, H.: Zur induktiven Nachheizung einer Überschall- wasserstoffströmung, Distation, Universität Stuttgart, 2009 [10] Böhrk, H., Auweter-Kurtz, M.; Velocity and Total Pressure Measurement in the Two-stage Hybrid Thruster TIHTUS, European Conference For Aerospace Sciences (EUCASS), Brussels, Belgium, Jul. 2007. [11] Böhrk, H., Auweter-Kurtz, M.; TIHTUS Thrust Measurement with a Baffle Plate, AIAA 2007-5297, Cincinnati, OH, Jul. 2007. [12] Bauder, U., Fertig, M., Böhrk, H., Auweter-Kurtz, M.; Initiation of the Numerical Investigation of the Hybrid Thruster TIHTUS, IEPC-2007-14, Florence, Italy, September 17-20, 2007 [13] Herdrich, G., Petkow, D.; High Enthalpy, water-cooled and thin-walled ICP Sources: Characterization and MHD- Optimization, Cambridge Journal of Plasma Physics, vol. 74, part 3, pp. 1-39, Dezember 2007. [14] Grau, T.: Numerische Untersuchung von Plasmawind- kanalströmungen zur Wiedereintritts-simulation, Dissertation, Universität Stuttgart, 2000 [15] Williams C.; An Analytic Approximation to Very High Specific Impulse and Specific Power Interplanetary Space Mission Analysis, Technical Report NASA Technical Memorandum 107058,1996 [16] Reece Roth, J.; Introduction to Fusion Energy, Ibis Publishing, Charlottesville, Virginia, 1986. [17] Kammash T., Lee M., Galbraith D., Cassenti B., Borowski S., Bussard R., Miley G., Chiang P.-R., Satsangi A., Choi C., Cox L., Watanabe Y., Gerwin R., Zubrin R., et al., Fusion Energy in Space Propulsion, volume 167, AIAA - Progress in Astronautics and Aeronautics, 181 Alexander Bell Drive, Suite 500, Reston, VA 20191-4344, USA, 1995. [18] Romanelli F., Bruno C., Regnoli G., Assessment of Open Magnetic Fusion for Space Propulsion, Ariadna Final Report 04/3102 ESTEC Contract 18853/05/NL/MV , European Space Research and Technology Centre, Noordwijk, 2004. [19] Santarius J.; Fusion space propulsion - a shorter time frame than you may think, in: JANNAF, Joint Army Navy Nasa Air Force Interagency Propulsion Committee, Monterey, 2005. [20] Petkow D., Herdrich G., Laufer R., Gabrielli R.A., Zeile O., Röser H.-P.; Comparative investigation of fusion reactions for space propulsion applications, Transactions of Japan Society for Aeronautical and Space Sciences, Space Technology, Japan, Vol.7 (2009) Pb 59 – Pb 63. [21] Petkow, D., Gabrielli, R.A., Herdrich, G., Laufer, R., Röser, H.-P.; Generalized Lawson criterion for magnetic fusion applications in space, article accepted to Fusion Engineering and Design, 2011 [22] Petkow D., Herdrich G., Laufer R., Röser H.-P.; Key technologies for fusion-based space propulsion: A case study, 6 iac – 07 - c3.3.02, in: 58th Internation Astronautical Congress, International Astronautical Federation, Hyderabad, 2007. [23] Petkow D., Gabrielli R. A., Herdrich G., Laufer R., Zeile O.; A generic model for a transpiration cooled fusion propulsion system, in: 27th International Symposium on Space Technology and Science, Tsukuba, Japan, 2007. [24] Hirsch, R. L.; Journal of Applied Physics, Vol.38-11, 1967, p 4522-4534. [25] Bussard, R.W.; Journal Fusion Technology, Vol.26, 1994, p 1326-1336. [26] Miley, G.H..; IEEE Transactions on plasma science, Vol.25- 4, 1997, p733-739. [27] Dietrich, C.C., Eurice, L.J., Sedwick, R.J.; 44th AIAAASME/SAE/ASEE joint Propulsion Conference, 2008, AIAA 2008-4760. [28] Miley, G.H., Sved, J..; Journal Applied Radiation and Isotopes, Vol.53, 2000, p779-783. [29] Farnsworth, F.; US Patent 3 258 402, 1966 [30] Miley, G.H.; Journal Fusion and Science Technology, Vol.56-1, 2009, p533-539 [31] Nadler, J.; 29th AIAA Plasma Dynamics and Lasers Conference, 1998, AIAA-98-2570. [32] Bramanti, C., Walker, R., Sutherland, O., Boswell, R., Charles, C., Fearn, D., Gonzalez Del Amo, J., Orlandi, M.; International Astronautical Congress, 2006, IAC-06-C4.4.7 [33] Fertig, M., Petkow, D., Stindl, T., Auweter-Kurtz, M. Quandt, M., Munz, C.-D., Neudorfer, J., Roller S., D'Andrea, D., Schneider, R.; Transactions of the high perfomance computing center, 2008 [34] Laufer, R., Herdrich, G., Hyde, T.W., Matthews, L.S., Röser, H.-P.; Journal Planetary and Space Science [35] Zubrin R.; The magnetic sail. Technical report, NASA Institute of Advanced Concepts 2000 [36] Winglee R. M., Slought J., Ziemba T., and Goodson A.; Mini-magnetospheric plasma propulsion: Tapping the energy of the solar wind for spacecraft propulsion. Journal of Geophysical Research, 105:21067-21077, 2000. [37] Khazanov G., Delamere P., Kabin K., and Linde T. J.; Fundamentals of the plasma sail concept: Magnetohydrodynamic and kinetic studies. Journal of Propulsion and Power, 21:853-861, 2005. [38] Funaki, I., Yamakawa, H.; Research status of sail pro- pulsion using the solar wind. J. Plasma Fusion Res. 8:1580- 1584, 2009. [39] Winglee, R. M., Slough, J., Ziemba, T., Euripides, P., Adrian, M. L., Callagher, D., and Craven, P.; Large-scale mini-magnetospheric plasma propulsion (m2p2) experiments. Technical report, ESA, 2001. [40] Nanbu, K.; Probability theory of electron-molecule, ion- molecule, molecule-molecule, and coulomb collisions for particle modeling of materials processing plasmas and gases. IEEE Transaction on plasma science, 28:971-990, 2000. [41] Pfeiffer, M., Petkow, D., Herdrich, G. and Fasoulas, S.; Assessment of a Numerical Approach Suitable for the M2P2 Problem. Open Plasma Physics Journal, Volume 4:24-33, 2011. Advanced Plasma (Propulsion) Concepts at IRS

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