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Chengyu Ma, Ph.D.
Chengyu Ma, Ph.D.
Neworbit Space Ltd.
在 neworbit.space 的电子邮件经过验证 - 首页
标题
引用次数
引用次数
年份
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
242021
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
232018
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
212014
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
202021
Plume characterization of a porous electrospray thruster
C Ma, C Ryan
The 36th International Electric Propulsion Conference, 1-19, 2019
182019
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
182015
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
172014
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
112021
Design and Characterisation of Electrospray Thrusters with High Emission Density
C Ma
University of Southampton, 2020
102020
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
82017
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
62022
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
52022
Characterization of a Micro-electrospray Thruster with a Porous Glass Emitter Array
C Ma, CN Ryan
Proc. Sp. Propuls. Conf, 1-12, 2018
52018
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
42013
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
22023
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
22022
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
22021
Optical emission characterization of a single emitter electrospray thruster interacting with surfaces
N Turan, C Ma, CN Ryan
AIAA SCITECH 2023 Forum, 1409, 2023
12023
Effects of propellant temperature on fragmentation in the plume of a porous electrospray thruster
S Dworski, C Ma, C Ryan
12022
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
12022
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