Electric micropropulsion systems

WP Wright, P Ferrer - Progress in Aerospace Sciences, 2015 - Elsevier
With the development of microspacecraft, the field of electrical micropropulsion is a rapidly
expanding discipline. New ideas are being explored constantly and a review of the current …

Mission capability assessment of cubesats using a miniature ion thruster

RW Conversano, RE Wirz - Journal of Spacecraft and Rockets, 2013 - arc.aiaa.org
The successful miniaturization of many spacecraft subsystems make CubeSats attractive
candidates for evermore-demanding scientific missions. A three-cell CubeSat employing the …

Miniature microwave discharge ion thruster driven by 1 watt microwave power

H Koizumi, H Kuninaka - Journal of Propulsion and Power, 2010 - arc.aiaa.org
THE age of space exploration using self-propelled small spacecraft is approaching. In the
past decade, research and development of small spacecraft have advanced extensively …

Plasma simulation and optimization for a miniaturized antenna ECR ion source

S Peng, A Zhang, W Wu, T Ma, Y Jiang, K Li… - Nuclear Instruments and …, 2021 - Elsevier
Abstract At Peking University (PKU), a miniaturized 2.45 GHz antenna permanent magnet
electron cyclotron resonance (PMECR) ion source, capable of generating a several-mA H+ …

Characteristics of microwave ECR ion thruster powered with plate antenna in cross-magnetic field: Standing wave, skin effect, and mode transition

SH Fu, ZF Ding - Physics of Plasmas, 2021 - pubs.aip.org
In a 2.45 GHz electron cyclotron resonance xenon ion source powered with circular plate-
antenna, a rapid evolution of radial plasma-profile with discharge power in a region below …

Theoretical and experimental study of the overdense plasma generation in a miniaturized microwave ion source

W Wu, S Peng, A Zhang, T Ma, Y Jiang, K Li… - Journal of Applied …, 2022 - pubs.aip.org
To understand the plasma evolution mechanism of microwave ion source (MIS), a hybrid
discharge heating (HDH) mode is proposed. That mode contains two parts: ignition …

Measurement of xenon plasma properties in an ion thruster using laser Thomson scattering technique

N Yamamoto, K Tomita, K Sugita, T Kurita… - Review of Scientific …, 2012 - pubs.aip.org
This paper reports on the development of a method for measuring xenon plasma properties
using the laser Thomson scattering technique, for application to ion engine system design …

Ion thruster operation with carbon nanotube field emission cathode

N Yamamoto, T Morita, Y Ohkawa, M Nakano… - Journal of Propulsion …, 2019 - arc.aiaa.org
ION engines have been used in a number of space missions, including Deep Space 1 [1],
Gravity Field and Steady-State Ocean Circulation Explorer (GOCE)[2], Hayabusa [3] and …

Effects of magnetic field configurations on the minimized ECR ion thrusters for micro-Newton and wide-range operations

SF Meng, DR Yu - Physics of Plasmas, 2023 - pubs.aip.org
Space-based gravitational wave detection missions require precise thrusts over a wide-
range of 1–100 μN. In this study, the axial ring-cusp magnetic field configuration is used to …

Numerical and experimental study of microwave-excited microplasma and micronozzle flow for a microplasma thruster

T Takahashi, Y Takao, K Eriguchi, K Ono - Physics of plasmas, 2009 - pubs.aip.org
Plasma and aerodynamic features have been investigated for a microplasma thruster of
electrothermal type using azimuthally symmetric microwave-excited microplasmas. The …