Electric micropropulsion systems
暂无分享,去创建一个
[1] Darren L. Hitt,et al. Mems-Based Satellite Micropropulsion Via Catalyzed Hydrogen Peroxide Decomposition , 2013 .
[2] Marc D. Rayman,et al. Dawn: A mission in development for exploration of main belt asteroids Vesta and Ceres , 2006 .
[3] Andrew D. Ketsdever,et al. Micropropulsion for small spacecraft , 2000 .
[4] A Fully Integrated Micro‐Magnetometer/Microspacecraft for Multipoint Measurements: the Free‐Flyer Magnetometer , 2013 .
[5] Georg Herdrich,et al. A Very Low Power Arcjet (VELARC) for Small Satellite Missions , 2011 .
[6] Rob Sherwood,et al. The EO-1 autonomous science agent , 2004, Proceedings of the Third International Joint Conference on Autonomous Agents and Multiagent Systems, 2004. AAMAS 2004..
[7] Simone Ciaralli,et al. PPT Development for Nanosatellite Applications: Experimental Results , 2015, IEEE Transactions on Plasma Science.
[8] Vaios Lappas,et al. Direct thrust measurement of a permanent magnet helicon double layer thruster , 2011 .
[9] C. Charles,et al. Thrust Measurements of a Small Scale Helicon Double Layer Thruster , 2011 .
[10] J. Mitterauer,et al. Micropropulsion for small spacecraft: a new challenge for field effect electric propulsion and microstructured liquid metal ion sources , 2004 .
[11] David H. Lehman,et al. Results from the Deep Space 1 technology validation mission , 2000 .
[12] Michael D. West,et al. Testing a Helicon Double Layer Thruster Immersed in a Space-Simulation Chamber , 2008 .
[13] Carole Rossi,et al. Design, fabrication and modeling of solid propellant microrocket-application to micropropulsion , 2002 .
[14] John P. W. Stark,et al. Scaling of a Colloid Thruster system for microNewton to milliNewton Thrust levels , 2007 .
[15] V. Lancellotti,et al. Design of 50 W helicon plasma thruster , 2009 .
[16] Juergen Mueller,et al. Thruster Options for Microspacecraft: A Review and Evaluation of State-of-the-Art and Emerging Technologies , 2000 .
[17] Daniel E. Hastings,et al. Three-dimensional plasma particle-in-cell calculations of ion thruster backflow contamination , 1996 .
[18] Michael Keidar,et al. Development of Micro-Vacuum Arc Thruster with Extended Lifetime , 2009 .
[19] Herbert Shea,et al. Performance of a micro-fabricated Colloid thruster system , 2009 .
[20] Robert C. Moore,et al. The MESSENGER mission to Mercury: spacecraft and mission design , 2001 .
[21] W. Steiger,et al. Indium Field Emission Electric Propulsion Microthruster Experimental Characterization , 2004 .
[22] Daniele Pavarin,et al. Thruster development set-up for the helicon plasma hydrazine combined micro research project , 2011 .
[23] J. Ziemer. Laser ablation microthruster technology , 2002 .
[24] Simon S. Ang,et al. A MEMS-based solid propellant microthruster with Au/Ti igniter , 2005 .
[25] A. Wokaun,et al. Micropropulsion Using a Laser Ablation Jet , 2004 .
[26] Sejin Kwon,et al. Design, fabrication, and testing of MEMS solid propellant thruster array chip on glass wafer , 2010 .
[27] Martin Tajmar,et al. Propulsion for Nanosatellites , 2011 .
[28] Michael J. Patterson,et al. Ion Propulsion Development Projects in US: Space Electric Rocket Test I to Deep Space 1 , 2001 .
[29] Hans Leiter,et al. Experimental Validation of RIT Micro-Propulsion Subsystem Performance at EPL , 2013 .
[30] J. Foster. Compact Plasma Accelerator for Micropropulsion Applications , 2001 .
[31] I. Katz,et al. Fundamentals of Electric Propulsion: Ion and Hall Thrusters , 2008 .
[32] Danick Briand,et al. Matrix of 10 × 10 addressed solid propellant microthrusters: Review of the technologies , 2006 .
[33] J. R. French. Warm Gas Propulsion for Small Satellites , 1997 .
[34] A. Wokaun,et al. Micropropulsion using laser ablation , 2004 .
[35] Masato Tanaka,et al. Research and Development of Osaka Institute of Technology PROITERES Nano-Satellite Series with Electric Rocket Engines , 2013 .
[36] P. Khiew,et al. Fabrication of a zirconia MEMS-based microthruster by gel casting on PDMS soft molds , 2012 .
[37] Denis Estublier,et al. The SMART-1 Hall Effect Thruster Around the Moon: In Flight Experience , 2005 .
[38] M. Delpech,et al. Flight demonstration of formation flying capabilities for future missions (NEAT Pathfinder) , 2014 .
[39] H. W. Loeb,et al. Design of High-Power High-Specific Impulse RF-Ion Thruster , 2011 .
[40] M. Tanaka,et al. Microstrip antenna with solar cells for microsatellites , 1995 .
[41] H. E. Barber,et al. Microthrusters Employing Catalytically Reacted N2—O2—H2 Gas Mixtures, Tridyne , 1970 .
[42] J. Khachan,et al. Downstream plasma characteristics from a single loop antenna in a helicon processing reactor , 1999 .
[43] Eric Rogers,et al. The Applicability of Pulsed Plasma Thrusters to Rendezvous and Docking of Cubesats , 2013 .
[44] Michele Coletti,et al. Low Power Ablative Pulsed Plasma Thrusters , 2013 .
[45] José A. Moríñigo,et al. Solid–gas surface effect on the performance of a MEMS-class nozzle for micropropulsion , 2010 .
[46] J. Mueller,et al. Leak-tight piezoelectric microvalve for high-pressure gas micropropulsion , 2004, Journal of Microelectromechanical Systems.
[47] H. Seifert,et al. Rocket Propulsion Elements , 1963 .
[48] Sven G. Bilen,et al. The potential of miniature electrodynamic tethers to enhance capabilities of femtosatellites , 2012, ICOPS 2012.
[49] Kar-Ming Cheung,et al. Deep Space 1 , 2016 .
[50] Peter Erichsen. Performance Evaluation of Spacecraft Propulsion Systems in Relation to Mission Impulse Requirements , 1997 .
[51] Henrik Kratz,et al. A Hybrid Cold Gas Microthruster System for Spacecraft , 2002 .
[52] Jason M. Makela,et al. Progress on Re-generable Field Emission Cathodes for Low- Power Electric Propulsion , 2007 .
[53] F. Rüdenauer. Field emission devices for space applications , 2007 .
[54] Juergen Mueller,et al. Thruster Optins for Microspacecraft: A Review and Evaluation of Existing Hardware and Emerging Technologies , 1997 .
[55] Satomi Kawamoto,et al. Precise numerical simulations of electrodynamic tethers for an active debris removal system , 2006 .
[56] Lilac Muller. Miniaturization Methods for Deep Space Microspacecraft , 1994 .
[57] Naoji Yamamoto,et al. Effects of Magnetic Field Configuration on Thrust Performance in A Miniature Microwave Discharge Ion Thruster , 2007 .
[58] Michele Coletti,et al. Design of a Two-Stage PPT for Cubesat Application , 2009 .
[59] N. Yamamoto,et al. Microwave-Plasma Interaction in a Miniature Plasma Ion Thruster , 2013 .
[60] Thales Alenia,et al. Electric Propulsion Diagnostic Package for the FEEP thruster on Lisa Path Finder: Review of status of achievements at TAS-I , 2007 .
[61] Martin Sweeting,et al. Nitrous oxide as a rocket propellant , 2001 .
[62] David Krejci,et al. Endurance testing of a pulsed plasma thruster for nanosatellites , 2013 .
[63] David H. Lehman,et al. Deep space one: NASA's first Deep-Space technology validation mission , 1997 .
[64] Steve Oleson,et al. Chemical Microthruster Options , 1996 .
[65] C. Law,et al. Influence of Cathode Shape on Vacuum Arc Thruster Performance and Operation , 2015, IEEE Transactions on Plasma Science.
[66] John R. Brophy,et al. NASA's Deep Space 1 ion engine , 2002 .
[67] Self-consistent Simulation of the Coupling Between Plasma and Neutral Gas in N-RIT , 2011 .
[68] V. I. Petrov,et al. Diffusion of a low-soluble impurity in a solid matrix , 2004 .
[69] Klaus Schilling,et al. Design of the UWE-4 Picosatellite Orbit Control System using Vacuum-Arc-Thrusters , 2013 .
[70] Herbert Shea,et al. Design and fabrication of an integrated MEMS-based colloid micropropulsion system , 2007 .
[71] Gabriel D. Roy,et al. Advances in Chemical Propulsion : Science to Technology , 2001 .
[72] A. Anders,et al. A Theoretical Analysis of Vacuum Arc Thruster and Vacuum Arc Ion Thruster Performance , 2008, IEEE Transactions on Plasma Science.
[73] Michele Coletti,et al. Design and Testing of a Micro Pulsed Plasma Thruster for Cubesat Application , 2011 .
[74] P. J. Cilliers,et al. ZACUBE‐1 Space Weather Mission: Characterize the SuperDARN HF Radar Antenna Array at SANAE‐IV , 2013 .
[75] C. Charles,et al. Performance characterization of a helicon double layer thruster using direct thrust measurements , 2011 .
[76] Daniele Pavarin,et al. EXPERIMENTAL SET-UP TO TEST A 50 W HELICON PLASMA THRUSTER , 2009 .
[77] R. McCormick,et al. Colloid thrusters for the new millennium, ST7 DRS mission , 2004, 2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720).
[78] S. Lee,et al. The CubeSat Approach to Space Access , 2008, 2008 IEEE Aerospace Conference.
[79] Donald Platt. A Monopropellant Milli-Newton Thruster System for Attitude Control of Nanosatellites , 2002 .
[80] George A. Boyarko,et al. Catalyzed combustion of hydrogen–oxygen in platinum tubes for micro-propulsion applications , 2005 .
[81] T. Shimizu,et al. Hollow Cathode Thruster Design and Development for Small Satellites , 2011 .
[82] A. Sengupta. Magnetic confinement in a ring-cusp ion thruster discharge plasma , 2009 .
[83] Stephen Gabriel,et al. Understanding hollow cathode thrust production mechanisms , 2009 .
[84] Michael Curt Elwenspoek,et al. Nozzle fabrication for micropropulsion of a microsatellite , 2009 .
[85] Gregory G. Spanjers,et al. Micropropulsion Options for the TechSat21 Space-Based Radar Flight , 1999 .
[86] S. J. Pottinger,et al. Micro Pulsed Plasma Thruster Development , 2007 .
[87] P. Peterson,et al. A High Specific Impulse Two-Stage Hall Thruster with Plasma Lens Focusing , 2001 .
[88] Jochen Schein,et al. Microvacuum Arc Thruster Design for a Cubesat Class Satellite , 2002 .
[89] Dan M. Goebel,et al. Magnetically Shielded Miniature Hall Thruster: Development and Initial Testing , 2013 .
[90] K. Anflo,et al. Flight demonstration of new thruster and green propellant technology on the PRISMA satellite , 2009 .
[91] Robert Zee,et al. The Design and Test of a Compact Propulsion System for CanX Nanosatellite Formation Flying , 2005 .
[92] Robert M. Winglee,et al. Simulation and laboratory validation of magnetic nozzle effects for the high power helicon thruster , 2007 .
[93] Klaus Schilling,et al. Innovative Vacuum Arc Thruster for CubeSat Constellations , 2013 .
[94] Günter Dr. Kornfeld,et al. Physics and Evolution of HEMP-Thrusters , 2007 .
[95] Jose Gonzalez del Amo. European Space Agency Activities in Electric Propulsion , 2013 .
[96] G. Zank,et al. Micro-propulsion in space via dust - plasma thruster , 2007 .
[97] Bryan Palaszewski,et al. PROPELLANT TECHNOLOGIES : FAR-REACHING BENEFITS FOR AERONAUTICAL AND SPACE-VEHICLE PROPULSION , 1998 .
[98] Claus Braxmaier,et al. Feasibility of a down-scaled HEMP-Thruster , 2011 .
[99] MorrisT.,et al. Study of an electrostatic micropropulsion system for nanosatellites , 2011 .
[100] Juergen Mueller,et al. A Review and Applicability Assessment of MEMS Based Microvalve Technologies for Microspacecraft Propulsions , 1999 .
[101] L. DeLuca,et al. Theoretical analysis of hydrides in solid and hybrid rocket propulsion , 2012 .
[102] Daniele Pavarin,et al. Development of Plasma Codes for the Design of Mini-Helicon Thrusters , 2011 .
[103] M. Martinez-Sanchez,et al. Spacecraft Electric Propulsion—An Overview , 1998 .
[104] P. Turchi,et al. Pulsed Plasma Thruster , 1998 .
[105] W. Folkner,et al. Mission analysis for the Laser Interferometer Space Antenna (LISA) mission , 2003 .
[106] Eberhard Gill,et al. PRISMA - AN AUTONOMOUS FORMATION FLYING MISSION , 2006 .
[107] L. Garrigues,et al. Two-dimensional model of a stationary plasma thruster , 2002 .
[108] C. Charles,et al. Thrust measurements in a low-magnetic field high-density mode in the helicon double layer thruster , 2010 .
[109] Andrew D. Ketsdever,et al. Systems Considerations and Design Options for' Microspacecraft Propulsion Systems , 1999 .
[110] C. Phipps,et al. Laser ablation of organic coatings as a basis for micropropulsion , 2004 .
[111] Kjell Anflo,et al. Green space propulsion: Opportunities and prospects , 2014 .
[112] Pelle Rangsten,et al. Miniaturization of components and systems for space using MEMS-technology , 2007 .
[113] C. Russell,et al. Messenger mission to Mercury , 2007 .
[114] Ulrich Johann,et al. Parametric Study of HEMP-Thruster Downscaling to $ {\mu }$ N Thrust Levels , 2015, IEEE Transactions on Plasma Science.
[115] M. Schiebl,et al. Development of a green bipropellant hydrogen peroxide thruster for attitude control on satellites , 2013 .
[116] Mathias Pietzka,et al. Development of Vacuum Arc Thrusters and Diagnostic Tools , 2011 .
[117] P. Ferrer,et al. Miniaturization of electrostatic ion engines by ionization and acceleration coupling , 2011 .
[118] Naoji Yamamoto,et al. Effect of Antenna Configuration on Thrust Performance in a Miniature Microwave Discharge Ion Engine , 2005 .
[119] P. Lozano,et al. Performance Characteristics of a Linear Ionic Liquid Electrospray Thruster , 2005 .
[120] E. Choueiri. Fundamental difference between the two variants of Hall thrusters - SPT and TAL , 2001 .
[121] Michael Keidar,et al. Analysis of Micro-Vacuum Arc Thrusters for Earth-Orbiting and Lunar Missions , 2011 .
[122] Vlad Hruby,et al. CubeSat Propulsion Using Electrospray Thrusters , 2009 .
[123] Stephen Gabriel,et al. Development of a Differential Radio Frequency Ion Thruster for Precision Spacecraft Control , 2009 .
[125] C. Charles,et al. An experimental investigation of alternative propellants for the helicon double layer thruster , 2008 .
[126] Zhaoying Zhou,et al. Development of a MEMS based colloid thruster with sandwich structure , 2005 .
[127] Robert P. Hoyt,et al. Harnessing the "Orbital Battery" for Propulsion via Energy- Harvesting Electrodynamic Tethers , 2011 .
[128] Michele Coletti,et al. Development of a Microthruster Module for Nanosatellite Applications , 2011 .