Plume composition measurements of a high-emission-density electrospray thruster C Ma, T Bull, CN Ryan Journal of Propulsion and Power 37 (6), 816-831, 2021 | 24 | 2021 |
The Design and Characterization of a Porous-emitter Electrospray Thruster (PET-100) for Interplanetary CubeSats C Ma, CN Ryan Proceedings of the 7th Interplanetary Cubesat Workshop, Paris, France, 29-30, 2018 | 23 | 2018 |
Study of the electric field formation in a multi-cusped magnetic field H Liu, H Wu, Y Zhao, D Yu, C Ma, D Wang, H Wei Physics of plasmas 21 (9), 2014 | 21 | 2014 |
Plume particle energy analysis of an ionic liquid electrospray ion source with high emission density C Ma, C Ryan Journal of Applied Physics 129 (8), 2021 | 20 | 2021 |
Plume characterization of a porous electrospray thruster C Ma, C Ryan The 36th International Electric Propulsion Conference, 1-19, 2019 | 18 | 2019 |
Experimental study on a variable magnet length cusped field thruster C Ma, H Liu, Y Hu, D Yu, P Chen, G Sun, Y Zhao Vacuum 115, 101-107, 2015 | 18 | 2015 |
Plume control of a cusped field thruster H Liu, G Sun, Y Zhao, P Chen, C Ma, H Wu, D Yu IEEE Transactions on Plasma Science 43 (1), 127-129, 2014 | 17 | 2014 |
Investigation of a plasma delivery system for optical figuring process YU Nan, R Jourdain, M Castelli, A Bennett, GUO Jiang, MA Chengyu, ... Chinese Journal of Aeronautics 34 (4), 518-525, 2021 | 11 | 2021 |
Design and Characterisation of Electrospray Thrusters with High Emission Density C Ma University of Southampton, 2020 | 10 | 2020 |
Feasibility study of a micro-electrospray thruster based on a porous glass emitter substrate C Ma, T Bull, C Ryan Proceedings of the 35th International Electric Propulsion Conference, 2017 | 8 | 2017 |
Green ionic liquid multimode monopropellant based chemical micro-thruster A Sharma, AC Adducci, J Rovey, C Ma, CN Ryan, S Berg, M Lembeck, ... AIAA SCITECH 2022 Forum, 1733, 2022 | 6 | 2022 |
Plume study of an electrospray thruster using a HAN-based dual-mode ionic liquid propellant C Ma, V Messina, CN Ryan, JL Rovey, Z Putnam, M Lembeck, S Berg Proceedings of the 37th International Electric Propulsion Conference, 2022 | 5 | 2022 |
Characterization of a Micro-electrospray Thruster with a Porous Glass Emitter Array C Ma, CN Ryan Proc. Sp. Propuls. Conf, 1-12, 2018 | 5 | 2018 |
Particle-in-Cell Simulations for a variable magnet length Cusped-Field thruster Y Zhao, H Liu, D Yu, C Ma Paper presented Proceedings of the 33rd International Electric Propulsion …, 2013 | 4 | 2013 |
Designing and commercialization of porous emitter electrospray thruster for space applications A Quraishi, S Dworski, C Ma, CN Ryan, A Ferreri, G Vincent, H Larsen, ... AIAA SCITECH 2023 Forum, 0262, 2023 | 2 | 2023 |
Emission characterization of porous electrospray thrusters with actively controlled flow rate C Ma, V Messina, C Ryan, JL Rovey, ZR Putnam, MF Lembeck, SP Berg | 2 | 2022 |
Time-of-flight characterization of electrospray thrusters using porous emitters with high emission currents C Ma, TG Bull, C Ryan Journal of Propulsion and Power, 2021 | 2 | 2021 |
Optical emission characterization of a single emitter electrospray thruster interacting with surfaces N Turan, C Ma, CN Ryan AIAA SCITECH 2023 Forum, 1409, 2023 | 1 | 2023 |
Effects of propellant temperature on fragmentation in the plume of a porous electrospray thruster S Dworski, C Ma, C Ryan | 1 | 2022 |
Characterization of Ionic Liquid Multimode Propellant Operating in a Porous Glass Electrospray Thruster AC Adduci, JL Rovey, CT Lyne, ZR Putnam, MF Lembeck, C Ma, ... IEPC-2022-500, 2022 | 1 | 2022 |