A Comprehensive Review of Atmosphere‐Breathing Electric Propulsion Systems
P Zheng, J Wu, Y Zhang, B Wu - International Journal of …, 2020 - Wiley Online Library
To develop the satellites for a low‐Earth‐orbit environment, atmosphere‐breathing electric
propulsion (ABEP) systems have become more attractive to researchers in the past decade …
propulsion (ABEP) systems have become more attractive to researchers in the past decade …
Review of High-Power Electrostatic and Electrothermal Electric Propulsion
DR Jovel, MLR Walker, D Herman - Journal of Propulsion and Power, 2022 - arc.aiaa.org
HIGH-POWER electric propulsion (EP) systems with input power levels greater than 10 kW
are now being considered and implemented on various space missions. This is primarily …
are now being considered and implemented on various space missions. This is primarily …
[图书][B] The influence of neutral flow rate in the operation of Hall thrusters
BM Reid - 2009 - search.proquest.com
Neutral flow dynamics in Hall thrusters are not often regarded as a critical aspect that
controls thruster operation and discharge channel physics. This dissertation, combined with …
controls thruster operation and discharge channel physics. This dissertation, combined with …
High-specific impulse Hall thrusters, part 1: Influence of current density and magnetic field
RR Hofer, RS Jankovsky, AD Gallimore - Journal of Propulsion and …, 2006 - arc.aiaa.org
MOST often regarded as a 1600-s specific impulse technology, the Hall effect thruster has
benefited from considerable theoretical and experimental research since the 1960s. 1− 3 …
benefited from considerable theoretical and experimental research since the 1960s. 1− 3 …
Mass and cost model for selecting thruster size in electric propulsion systems
RR Hofer, TM Randolph - Journal of Propulsion and Power, 2013 - arc.aiaa.org
A model of system mass and life-cycle costs is used to determine the optimal number of
thrusters for electric propulsion systems. The model is generalized for application with most …
thrusters for electric propulsion systems. The model is generalized for application with most …
A theoretical thrust density limit for Hall thrusters
Hall Thrusters typically operate at thrust densities on the order of 10 N/m 2, which appear to
be orders of magnitude below the thrust density limits suggested in previous literature …
be orders of magnitude below the thrust density limits suggested in previous literature …
High-specific impulse operation of the BPT-4000 Hall thruster for NASA science missions
R Hofer - 46th AIAA/ASME/SAE/ASEE Joint Propulsion …, 2010 - arc.aiaa.org
To meet the propulsive requirements, cost constraints, and scientific objectives of NASA
deep-space missions, high-performance, low-cost electric propulsion (EP) options are …
deep-space missions, high-performance, low-cost electric propulsion (EP) options are …
大功率霍尔电推进研究现状与关键技术
康小录， 张岩， 刘佳， 丁永杰， 于达仁 - 推进技术, 2019 - jpt.tjjsjpt.com
综述了大功率霍尔电推进技术的国内外研究现状, 并结合未来空间任务需求,
指出了大功率霍尔电推进技术的发展趋势. 根据大功率霍尔电推进的技术特点 …
指出了大功率霍尔电推进技术的发展趋势. 根据大功率霍尔电推进的技术特点 …
Overview of the development of the solar electric propulsion technology demonstration mission 12.5-kW Hall thruster
H Kamhawi, W Huang, T Haag, J Yim… - 50th AIAA/ASME/SAE …, 2014 - arc.aiaa.org
Abstract− NASA is developing mission concepts for a solar electric propulsion technology
demonstration mission. A number of mission concepts are being evaluated including …
demonstration mission. A number of mission concepts are being evaluated including …
Performance test results of the NASA-457M v2 Hall thruster
G Soulas, T Haag, D Herman, W Huang… - 48th AIAA/ASME/SAE …, 2012 - arc.aiaa.org
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit : Performance Test Results
of the NASA-457M v2 Hall Thruster Page 1 American Institute of Aeronautics and Astronautics …
of the NASA-457M v2 Hall Thruster Page 1 American Institute of Aeronautics and Astronautics …