Space Propulsion Laboratory

Propelling New Ideas into Higher Orbits

Conference Proceedings

TitleYearAuthorsConference
Numerical Simulation of Ionic Liquid Ion Sources in Tip Geometries2024X. Gallud and P. C. Lozano38th International Electric Propulsion Conference, Toulouse, France (IEPC-2024-434)
Performance Characterization of High-Density Electrospray Thrusters2024M. N. Corrado, C. Wangari, M. R. Finch, L. Parameswaran, M. Cook, E. C. Holihan, R. Mathews, J. Kedzierski, L. M. Racz, M. A. Smith, and P. C. Lozano38th International Electric Propulsion Conference, Toulouse, France (IEPC-2024-811)
Temperature-Dependent Performance of Electrospray Thrusters with ASCENT Monopropellant2024A. R. Bruno, M. N. Corrado, and P. C. Lozano38th International Electric Propulsion Conference, Toulouse, France (IEPC-2024-782)
Preliminary Testing of Flat-panel Pixel Electrospray Thrusters for Increased Reliability and Efficiency2024C. J. Nachtigal and P. C. Lozano38th International Electric Propulsion Conference, Toulouse, France (IEPC-2024-752)
Investigation of Electrochemical Gas Generation in Ion Electrospray Thrusters2024S. Z. Shaik and P. C. Lozano38th International Electric Propulsion Conference, Toulouse, France (IEPC-2024-511)
Propellant Transport in Electroactive Polymer-Electrospray Thrusters2024C. Wangari and P. C. Lozano38th International Electric Propulsion Conference, Toulouse, France (IEPC-2024-356)
Direct and Indirect Thrust Measurements of Ionic-Liquid Electrospray Thrusters on a Magnetically-Levitated Testbed2024M. N. Corrado, A. R. Bruno, and P. C. LozanoAIAA SciTech Forum, Orlando, USA
“Pixels” in Electrospray Thrusters for Ultra-Reliable Flat-Panel Electric Propulsion2024C. J. Nachtigal and P. C. LozanoAIAA SciTech Forum, Orlando, USA
Characterization of Propellant-Surface Collision Byproducts using MD Simulations and RGA Measurements2024S. Z. Shaik, A. R. Bendimerad, A. T. M. Tahsin, A. Smith, P. C. Lozano, and E. PetroAIAA SciTech Forum, Orlando, USA
Angular Properties of Ionic Liquid Electrospray Emitters2023M. R. Schroeder, X. Gallud, A. R. Bruno, O. Jia-Richards, and P. C. LozanoAIAA SciTech Forum, National Harbor, USA
Thrust Inference for Ionic-Liquid Electrospray Thrusters on a Magnetically-Levitating Thrust Balance2022O. Jia-Richards, M. N. Corrado, and P. C. Lozano37th International Electric Propulsion Conference, Cambridge, Massachusetts (IEPC-2022-208)
Characterization of a Single-Polarity Electrospray Propulsion System2022S. Z. Shaik, O. Jia-Richards, and P. C. Lozano37th International Electric Propulsion Conference, Cambridge, Massachusetts (IEPC-2022-203)
Investigating Prompt Ionic Liquid Cluster Fragmentation from Electrospray Total Mass Flow Measurements2022M. R. Schroeder and P. C. Lozano37th International Electric Propulsion Conference, Cambridge, Massachusetts (IEPC-2022-210)
Performance Measurement and Propellant Testing for the STEP-1 CubeSat Electrospray Thrusters2022G. M. Pettersson, A. R. Bruno, M. N. Corrado, B. S. Medina, D. Krejci, and P. C. Lozano37th International Electric Propulsion Conference, Cambridge, Massachusetts (IEPC-2022-216)
An Electrowetting Flow Controller for Ion Electrospray Propulsion Systems2022J. V. MacArthur and P. Lozano37th International Electric Propulsion Conference, Cambridge, Massachusetts (IEPC-2022-586)
The Current Emitted by Ionic Liquid Ion Sources in the Pure-Ionic Regime2022X. Gallud Cidoncha and P. C. Lozano37th International Electric Propulsion Conference, Cambridge, Massachusetts (IEPC-2022-218)
Densification of Ionic Liquid Electrospray Thrusters using Silicon-Based MEMS Fabrication2022M. N. Corrado, P. C. Lozano, L. Parameswaran, M. Cook, E. C. Holihan, R. Mathews, L. M. Racz, and M. A. Smith37th International Electric Propulsion Conference, Cambridge, Massachusetts (IEPC-2022-177)
Investigating Variations in Startup Emission Across a Passively Fed Porous Electrospray Thruster2022A. R. Bruno, M. R. Schroeder, S. Z. Shaik, and P. C. Lozano37th International Electric Propulsion Conference, Cambridge, Massachusetts (IEPC-2022-214)
Electroactive Polymer Emitters for Electrospray Propulsion2022C. Wangari and P. C. Lozano37th International Electric Propulsion Conference, Cambridge, Massachusetts (IEPC-2022-195)
Ensemble Kalman Update for Inference of Spatial Uniformity of Emission across an Electrospray Array
2022O. Jia-Richards and P. C. Lozano43rd IEEE Aerospace Conference, Big Sky, USA
Effect of Lithium Ionic Liquid Mixtures on Electrospray Propulsion Performance
2022M. Schroeder, A. Bruno, and P. C. Lozano43rd IEEE Aerospace Conference, Big Sky, USA
Characterization of Electrospray Thrusters with HAN-Based Monopropellans for Multimode Propulsion Applications
2022A. Bruno, M. Schroeder, and P. C. LozanoAIAA SciTech Forum, San Diego, USA
Development and Laboratory Testing of a CubeSat-Compatible Staged Ionic-Liquid Electrospray Propulsion System
2022G. M. Pettersson, O. Jia-Richards and P. C. LozanoAIAA SciTech Forum, San Diego, USA
Ionic Liquid Electrospray Transient Emission Characterization
2022M. Schroeder, A. Bruno, and P. C. LozanoAIAA SciTech Forum, San Diego, USA
Spacecraft Charging in Sunlight, Physical Mechanisms, Mitigation Techniques
2021S. T. LaiNASA Applied Space Environments Conference, Virtual
Design and Testing of a Propellant Management System for Bimodal Chemical-Electrospray Propulsion
2021A. R. Bruno and P. C. Lozano42nd IEEE Aerospace Conference, Virtual
Redundancy for Asteroid Detumbling via Staging
2021O. Jia-Richards and P. C. Lozano42nd IEEE Aerospace Conference, Virtual
Facets of Spacecraft Charging; Critical Temperature and Dependence on Ambient Electron Density
2020S. T. LaiJoint INFN-CERN-ARIES Workshop on Electron-Cloud Effects, La Biodola, Isola d’Elba, Italy
Feasibility of a Deep-Space CubeSat Mission with a Stage-Based Electrospray Propulsion System
2020O. Jia-Richards, D. C. Sternberg, D. Grebow, S. Mohan, and P. C. Lozano41st IEEE Aerospace Conference, Big Sky, MT
Real-time Motion Planning in Unknown Environments for Legged Robotic Planetary Exploration
2020K. Albee, A. Cabrales Hernandez, O. Jia-Richards, and A. Teran Espinoza41st IEEE Aerospace Conference, Big Sky, MT
Laboratory Demonstration of a Staging System for Electrospray Thrusters
2019O. Jia-Richards and P. C. Lozano36th International Electric Propulsion Conference, Vienna, Austria (IEPC-2019-173)
Informing the Design of Pure-ion Electrospray Thrusters via Simulation of the Leaky-Dielectric Model with Charge Evaporation
2019X. Gallud Cidoncha, B. O. Kristinsson, and P. C. Lozano 36th International Electric Propulsion Conference, Vienna, Austria (IEPC-2019-610)
Operation and Performance of a Fully-Integrated ionic-Electrospray Propulsion System
2019B. O. Kristinsson, D. Freeman, E. M. Petro, P. C. Lozano, A. Hsu, and J. A. Young36th International Electric Propulsion Conference, Vienna, Austria (IEPC-2019-646)
Investigation of Electrospray Plume Composition during Voltage Transients
2019E. M. Petro, M. Cezairli, M. Schroeder, and P. C. Lozano36th International Electric Propulsion Conference, Vienna, Austria (IEPC-2019-794)
Microfluidic and Extractor Electrode Update in the ion-Electrospray Propulsion System
2019J. MacArthur, B. O. Kristinsson, D. Freeman, E. Petro, H. Li, and P. C. Lozano36th International Electric Propulsion Conference, Vienna, Austria (IEPC-2019-909)
Development of an Electrospray Fragmentation Model for Kinetic Plume Modeling
2019E. M. Petro, C. E. Miller, J. Schmidt, and P. C. Lozano36th International Electric Propulsion Conference, Vienna, Austria (IEPC-2019-930)
Productization of CubeSat Rendezvous and Docking Solutions
2019M. Chan, J. Bultitude, D. Faber, and D. Hawes33rd AIAA/Utah State University Small Satellite Conference, Logan, UT
Staged-based Electrospray Propulsion System for Deep-Space Exploration with CubeSats
2019O. Jia-Richards and P. Lozano40th IEEE Aerospace Conference, Big Sky, MT
Tradespace Exploration of the Next Generation Communication Satellites
2019A. Aguilar, P. Butler, J. Collins, M. Guerster, B. O. Kristinsson, P. McKeen, K. Cahoy, and E. CrawleyAIAA SciTech Forum, San Diego, CA
Characterization Of EMI-(HF)2.3F Using A Carbon Xerogel Ionic Liquid Ion Source
2017C. Miller, D. Krejci, C. Bates, D. Getty and P. LozanoIEPC-2017-210 35th International Electric Propulsion Conference, Atlanta, Georgia
Scalable tank design for the passively fed ionic liquid electrospray thruster
2017D. Krejci and P. LozanoIEPC-2017-224 35th International Electric Propulsion Conference, Atlanta, Georgia
High efficiency ionic liquid electrospray propulsion for Nanosatellites
2016D. Krejci, F. Mier-Hicks, C. Fucetola and P. LozanoIAC-16-C4.6.6×32963 67th International Astronautical Congress, Guadalajara, Mexico
Measurement of the Fragmentation Rates of Solvated Ions in Ion Electrospray Thrusters
2016C. Miller and P. LozanoAIAA-2016-4551 52ND JOINT PROPULSION CONFERENCE AND EXHIBIT, Salt Lake City, UT
Current Capabilities of Scalable Ionic Liquid Electrospray Thrusters for Nano-Satellites
2016D. Krejci and P. Lozano39th AAS Guidance & Control Conference, Breckenridge, CO
Design and characterization of a scalable ion electrospray propulsion system2015D. Krejci, F. Mier-Hicks, C. Fucetola, P. Lozano, A. Hsu Schouten and F. MartelIEPC-2015-149 34th INTERNATIONAL ELECTRIC PROPULSION CONFERENCE, Kobe, Japan
Thrust Measurements of Ion Electrospray Thrusters using a CubeSat Compatible Magnetically Levitated Thrust Balance2015F. Mier-Hicks and P. LozanoIEPC-2015-148 34th INTERNATIONAL ELECTRIC PROPULSION CONFERENCE, Kobe, Japan
The effects of metastable solvated ions on electrospray ion thruster efficiency2015C. Miller and P. LozanoIEPC-2015-179 34th INTERNATIONAL ELECTRIC PROPULSION CONFERENCE, Kobe, Japan
Electrical double layers in electrospray propulsion2015K. Masuyama and P. LozanoIEPC-2015-178 34th INTERNATIONAL ELECTRIC PROPULSION CONFERENCE, Kobe, Japan 
On the Electrospray Emission From Porous Media and Implications for Emitter Optimization2014C. Coffman and P. LozanoAIAA-2014-3695 49TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Does spacecraft potential depend on the ambient electron density?2014Lai, S. T., M. Martinez-Sanchez, K. Cahoy, M. F. Thomsen, Y. Shprits, W. Q. Lohmeyer, and F. WongAGU Fall Meeting, San Francisco, CA
Trapped Photoelectrons during Spacecraft Charging in Sunlight2014S. T. Lai and K. CahoyProc. 13th Spacecraft Charging Conf, CalTech Jet Propulsion Laboratory, Pasadena, CA, Paper 188, 5pp.
On the Manufacturing and Emission Characteristics of Dielectric Electrospray Sources2013C. Coffman and P. LozanoAIAA-2013-4035 49TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Investigating Efficiency Losses from Solvated Ion Fragmentation in Electrospray Thruster Beams2013T. Coles and P. LozanoAIAA-2013-4033 49TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Bimodal Propulsion System Using Ionic Liquid Propellant for Pico- and Nano-satellite Applications2013K. Masuyama, M. and P. LozanoAIAA-2013-3962 49TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Physical Limitations on the Lifetime of Ionic Liquid Ion Sources2013N. Brikner and P. LozanoAIAA-2013-3881 49TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Characterization of a CubeSat compatible magnetically levitated thrust balance for electrospray propulsion systems2013F. Mier-Hicks, L. Perna, C. Coffman and P. LozanoAIAA-2013-3879 49TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Ion Electrospray Propulsion System Feasibility Study for various Satellite Missions and Architectures2013S. Arestie, C. Whitlock and P. LozanoAIAA-2013-3877 49TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Fabrication of Electrospray Thrusters by Sintering Glass Microspheres2013J. Xie, M. Canonica and P. LozanoAIAA-2013-3824 49TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Progress toward demonstration of remote, autonomous attitude control of a CubeSat using ion electrospray propulsion systems2012L. Perna, F. Mier-Hicks and P. LozanoAIAA-2012-4289 48TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Progress toward demonstration of remote, autonomous attitude control of a CubeSat using ion electrospray propulsion systems2012L. Perna, F. Mier-Hicks and P. LozanoAIAA-2012-4289 48TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Molecular dynamics simulations and experimental results of fragmentation characteristics of EMI-BF4 ion beams2012T. Coles, T. Fedkiw and P. LozanoAIAA-2012-3793 48TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Structural design for a small satellite platform2012R.A. Vazquez-Robledo, S.D. Santillan-Gutierrez, C. Romo-Fuentes, A. Ramirez-Aguilar, A. Farah-Simon, A. Saenz-Otero and P. LozanoSan Luis Potosi, Mexico 2nd National and 1st Latin-American Conference in Aerospace Science and Engineering
UNAM-MIT Quetzal satellite project2012S.D. Santillan-Gutierrez, C. Romo-Fuentes, J.A. Ramirez-Aguilara, S. de la Rosa-Nieves, E. Sanchez-Medina, P. Lozano, A. Saenz-Otero, M. Grutter de la Mora and J. Prado-MolinaSan Luis Potosi, Mexico 2nd National and 1st Latin-American Conference in Aerospace Science and Engineering
Design and construction of a power subsystem prototype for electric propulsion in the Quetzal microsatellite2012M. Mendez-Astudillo, P. Lozano, A. Saenz-Otero, S.D. Santillan-Gutierrez, C. Romo-Fuentes and J.A. Ramirez-AguilarSan Luis Potosi, Mexico 2nd National and 1st Latin-American Conference in Aerospace Science and Engineering
Miniature ion electrospray thrusters and performance tests on CubeSats2012F. Martel, L. Perna and P. LozanoLogan, UT 26th Annual AIAA/USU Conference on Small Satellites, August 13-16, 2012, Logan, UT
A porous metal electrospray array for space propulsion applications2012C. Coffman and P. LozanoBordeaux, France Space Propulsion 2012, May 7-10, 2012, Bordeaux, France
The role of surface condition in the yields of secondary electrons, backscattered electrons, and photoelectrons from spacecraft2012Shu T. Lai12th Spacecraft Chraging Technology Conference, Kitakyushu, Japan
Spacecraft charging: incoming and outgoing electrons2012Shu T. LaiECLOUD’12 WORKSHOP, Elba, Italy
Progress toward a variable specific impulse electrospray propulsion system2011C. Coffman, D. Courtney, F.M. Hicks, S. Jamil, H. Li and P. LozanoAIAA-2011-5591 47TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Characterization and optimization of a diverging cusped field thruster with a calibrated horizontal accelerometer2011R. Daspit, C. Han, P. Lozano and M. Martinez-SanchezAIAA-2011-6069 47TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Fabrication and testing of an ionic electrospray propulsion system device with a porous Ni tip array2011H. Li, D. Courtney, P. Diaz-Gomez and P. LozanoBeijing, China 16th International Conference on Solid-State Sensors, Actuators and Microsystems, June 5-9, 2011, Beijing, China
On the validation of porous nickel as substrate material for electrospray ion propulsion2010D.G. Courtney, H. Li, P. Diaz-Gomez, T.P. Fedkiw and P.C. LozanoAIAA-2010-7020 46TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Low frequency oscillations in the diverging cusped-field thruster2010S.R. Gildea, T.S. Matlock, P. Lozano and M. Martinez-SanchezAIAA-2010-7014 46TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Magnetic field effects on the plume of a diverging cusped-field thruster2010T.S. Matlock, S.R. Gildea, P. Lozano and M. Martinez-SanchezAIAA-2010-7104 46TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Discharge chamber wall flux measurements in a diverging cusped-field thruster2010T. Matlock, P. Lozano and M. Martinez-SanchezSan Sebastian, Spain Space Propulsion 2010, May 2-6, 2010, San Sebastian, Spain
Efficiency measurement of an ionic liquid electrospray thruster2010T. Fedkiw and P. LozanoSan Sebastian, Spain Space Propulsion 2010, May 2-6, 2010, San Sebastian, Spain
On the development of high specific impulse electric propulsion thrusters for small satellites2010P. Lozano and D. Courtney1915685 The Small Satellites Systems and Services – The 4S Symposium
Porous ionic liquid ion source thrusters for small satellite Propulsion2010D. Courtney and P. LozanoToronto, Ontario, Canada Canadian Aeronautics and Space Institute 15th Astronautics Conference, ASTRO 2010
Electrostatic thrusters for microgravity propulsion in a pressurized environment2010A. Saenz-Otero, A. Pina, G. Wellman, R. Garriott and P. LozanoBig Sky, MT IEEE 2010 Aerospace Conference
High Delta-V nanosatellite missions using a diverging cusped field thruster2009R. Daspit, C. Han, P. Lozano and D. MillerIEPC-2009-047 31st International Electric Propulsion Conference
Atomistic simulations of electrospray ion emission from a tungsten plate2009N. Takahashi and P. LozanoAIAA-2009-5089 45TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Porous ionic liquid ion source fabrication refinements and variable beam energy experiments2009D. Courtney and P. LozanoAIAA-2009-5087 45TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Spectroscopic and electrostatic investigation of the diverging cusped-field thruster2009T. Matlock, B. Tartler, R. Daspit, O. Batishchev, P. Lozano and M. Martinez-SanchezAIAA-2009-4812 45TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Experimental analysis of low Reynolds number supersonic flow efficiency2009A.R. Bruccoleri and P. LozanoAIAA-2009-5243 45TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Atomistic numerical approach to electrospray thrusters2009N. Takahashi, M. Lieu and P.C. LozanoTsukuba, Japan 27th International Symposium on Space Technology and Science, July 5-12, 2009
Development of ionic liquid electrospray thrusters using porous emitter substrates2009D. Courtney and P. LozanoTsukuba, Japan 27th International Symposium on Space Technology and Science, July 5-12, 2009
Two Dimensional Simulation of a Radio-Frequency Ion Thruster Discharge2008Tsay, M. and Martinez-Sanchez, M.AIAA-2008-5196 44TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Continued Investigation of a Diverging Cusped Field Thruster2008Courtney, D., Lozano, P. and Martinez-Sanchez, M.AIAA-2008-4631 44TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Performance of Heavy Ionic Liquids with Porous Metal Electrospray Emitters2008R. Legge and P. LozanoAIAA-2008-5002 44TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Computational Investigation of Molecular Ion Evaporation in Electrospray Thruster2008N. Takahashi and P. LozanoAIAA-2008-4533 44TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Continued investigation of diverging cusped field thruster2008D.G. Courtney, P. Lozano and M. Martinez-SanchezAIAA-2008-4631 44TH JOINT PROPULSION CONFERENCE AND EXHIBIT
Maximizing one-dimensional porous emitter packing density for electrospray applications2008R. Legge and P. LozanoHeraklion, Crete, Greece 5th International Spacecraft Propulsion Conference, May 5-8, 2008
Emission of ions from electrically stressed ionic liquid menisci in vacuum2008N. Takahashi, A. Zorzos and P. LozanoKobe, Japan Symposium on Molten Salts, October 19-23, 2008
Simple Performance Modeling of a Radio-Frequency Ion Thruster2008Tsay, M. and Martinez-Sanchez, M.IEPC-2007-072 30TH INTERNATIONAL ELECTRIC PROPULSION CONFERENCE, FLORENCE, ITALY
Diverging Cusped-field Hall Thruster (DCHT)2007Courtney, D. and Martinez-Sanchez, M.IEPC-2007-039 30TH INTERNATIONAL ELECTRIC PROPULSION CONFERENCE, FLORENCE, ITALY
Fabrication and characterization of porous metal emitters for electrospray thrusters2007R. Legge, P. Lozano and M. Martinez-SanchezIEPC-2007-145 30TH INTERNATIONAL ELECTRIC PROPULSION CONFERENCE, FLORENCE, ITALY
Design and Preliminary Testing of a Miniaturized TAL Hall Thruster 2006Warner, Noah., Martinez-Sanchez, M. AIAA-2006-4994  42ND JOINT PROPULSION CONFERENCE, SACRAMENTO, CA, JULY 9-12, 2006. 
Multi-Grid IEC Fusion for Space Power and Propulsion 2006Sedwick, R.., McGuire, T., Dietrich, C., Warner, N. and Zayas, D.  AIAA-2006-4390  42ND JOINT PROPULSION CONFERENCE, SACRAMENTO, CA, JULY 9-12, 2006. 
A microfabricated electrospray thruster using ridge emitters and ceramic-ball extractor location2006B. Gassend, L.F. Velasquez-Garcia, P. Lozano, A.I. Akinwande and M. Martinez-Sanchez AIAA-2006-5009  42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 9-12, 2006, Sacramento, CA
Propellant spread over Silicon Electrospray surfaces2006T.C. Garza, P. Lozano, L.F. Velasquez-Garcia and M. Martinez-Sanchez AIAA-2006-4640  42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 9-12, 2006, Sacramento, CA
Capillary vs. externally wetted ionic liquid ion sources2006S. Castro, C. Larriba, J. Fernandez de la Mora, P. Lozano and S. Sümer AIAA-2006-4645  42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 9-12, 2006, Sacramento, CA
Characterization of a variable specific impulse ionic liquid electrospray thruster beam2006S. Sümer, P. Lozano and M. Martinez-Sanchez AIAA-2006-4641  42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, July 9-12, 2006, Sacramento, CA
Efficiency estimation of EMI-BF4 Ionic Liquid Electrospray Thrusters 2005Lozano, P., Martinez-Sanchez M.AIAA-2005-4388  41ST AIAA/ASME/SAE/ASEE JOINT PROPULSION CONFERENCE
Performance Characteristics of a Linear Ionic Liquid Electrospray Thruster 2005Lozano, P., Glass B., Martinez-Sanchez M. IEPC-2005-192  29TH INTERNATIONAL ELECTRIC PROPULSION CONFERENCE, PRINCETON UNIVERSITY (USA) 
Mechanical Assembly of Electrospray Thruster Grid 2005Gassend, B., Velasquez-Garcia, L.F., Akinwande, A.I. and Martinez-Sanchez, M. IEPC-2005  29TH INTERNATIONAL ELECTRIC PROPULSION CONFERENCE 
The characterization of Si wettability and properties of externally wetted microfabricated electrospray thruster arrays 2005Garza, T.C., Lozano, P., Velasquez-Garcia, L.F. and Martinez-Sanchez, M. IEPC-2005-195  29TH INTERNATIONAL ELECTRIC PROPULSION CONFERENCE, PRINCETON UNIVERSITY (USA), OCT 21-NOV 
Externally wetted ionic liquid thruster 2004Lozano, P., Martinez-Sanchez, M. and Lopez-Urdiales, J.M. Cagliari, Italy.  4TH INTERNATIONAL CONFERENCE ON SPACECRAFT PROPULSION 
Numerical simulation of Taylor cone-jets and colloid thruster plumes 2004Carretero, J., Lozano, P. and Martinez-Sanchez, M. Cagliari, Italy.  4TH INTERNATIONAL CONFERENCE ON SPACECRAFT PROPULSION 
High Voltage Plume Measurements and Internal Probing of the BHT-1000 Hall Thruster 2004Azziz, Y., Warner, N., Martinez-Sanchez, M. and Szabo, J. AIAA 2004-4097  40TH JOINT PROPULSION CONFERENCE, FORT LAUDERDALE, FL 
Two-dimensional microfabricated colloid thruster array 2004L. F. Velasquez-Garcia, M. Martinez-Sanchez and A.I. Akinwande AIAA-2004-3595  40th Joint Propulsion Conference, Fort Lauderdale, FL 
Characterization of a High Specific Impulse Hall Thruster Using Electrostatic Probes 2003Warner, N., Szabo, J. and Martinez-Sanchez, M. IEPC-2003-082  28TH INTERNATIONAL ELECTRIC PROPULSION CONFERENCE, TOULOUSE, FRANCE 
One and Two Dimensional Modeling of the BHT-1000 2003Szabo, J., Rostler, P., McElhinney, S. and Warner, N. IEPC-2003-231  28TH INTERNATIONAL ELECTRIC PROPULSION CONFERENCE, TOULOUSE, FRANCE 
Mass spectrometric analysis of ion-emission from selected colloid thruster fuels 2003Chiu, Y., Levandier, B., Austin, R., Dressler, R., Murray, P.T., Lozano, P. and Martinez-Sanchez, M. AIAA-2003-4848  39TH JOINT PROPULSION CONFERENCE, 20-23 JULY 2003, HUNTSVILLE, ALABAMA 
The concept and development of a micro-fabricated colloid thruster array 2003L. F. Velasquez-Garcia, J. A. Carretero, A.I. Akinwande and M. Martinez-Sanchez Huntsville, AL  39th Joint Propulsion Conference 
Development of a micro-fabricated colloid thruster array 2003L. F. Velasquez-Garcia, M. Martinez-Sanchez and A.I. Akinwande IEPC 0138  28th International Electric Propulsion Conference, Toulouse, France 
Modeling developments on colloid thrusters2003Carretero, J., Higuera, F., Martinez-Sanchez, M. and Lozano, P. Toulouse, France  28TH INTERNATIONAL ELECTRIC PROPULSION CONFERENCE 
Instrumentation and Modeling of a High Isp Hall Thruster 2002Szabo, J., Warner, N. and Martinez-Sanchez, M. AIAA 2002-4248  38TH JOINT PROPULSION CONFERENCE, INDIANAPOLOIS, IN 
Experimental measurements of colloid thruster plumes in the ion-droplet mixed regime2002Lozano, P., Martinez-Sanchez, M. AIAA-3814  38TH JOINT PROPULSION CONFERENCE, 7-10 JULY 2002, INDIANAPOLIS, INDIANA. 
Microfabrication of a Colloid Thruster Array 2002L. F. Velasquez-GarciaVersailles, France  6th Intnl. Symposium on Propulsion for Space Transportation of the XXI Century, 14-17 May 2002 
A MICRO-FABRICATED COLLOID THRUSTER ARRAY 2002Luis Fernando Velasquez Garcia, Manuel Martinez-Sanchez AIAA-2002-3810  38th Joint Propulsion Conference, Indianapolis, IN 
The Effect of Using Finite-Width Electrostatic Gates in Time-of-Flight Measurements for Colloid Thrusters 2001Lozano, P., Martinez-Sanchez, M. Pasadena, CA  27TH INTERNATIONAL ELECTRIC PROPULSION CONFERENCE 
Experimental Study of Colloid Plumes 2001Lozano, P., Martinez-Sanchez, M.AIAA-2001-3334  37TH JOINT PROPULSION CONFERENCE, 8-11 JULY 2001, SALT LAKE CITY, UTAH. 
Jets and Sprays Emitted from Colloid Thrusters: Experiments and Modeling 2000Lozano, P., Martinez-Sanchez, M.ESA SP-465   3RD INTERNATIONAL CONFERENCE ON SPACECRAFT PROPULSION, CANNES (FRANCE) 10-13 OCTOBER 2000 
The Use of Vibration Data for Liquid Rocket Health Monitoring 1998Lozano, P., Ho, N., Mangoubi, R. and Martinez-Sanchez, M. AIAA-98-3615  34TH AIAA/ASME/SAE/ASEE JPC & EXHIBIT, JULY 12-15, 1998, CLEVELAND, OH. 
A Model-Based Vehicle Health Monitoring System for the Space Shuttle Main Engine 1998Ho, N., Lozano, P., Mangoubi, R. and Martinez-Sanchez, M. AIAA-98-3609  34TH AIAA/ASME/SAE/ASEE JPC & EXHIBIT, JULY 12-15, 1998, CLEVELAND, OH.
Failure Detection and Isolation for the Space Shuttle Main Engine 1997Ho, N., Lozano, P., Mangoubi, R. and Martinez-Sanchez, M. Seattle, WA  33RD JOINT PROPULSION CONFERENCE & EXHIBIT, JULY 6-9