丁

丁永杰 (Yongjie Ding)

Harbin Institute of Technology邮箱:dingyongjie@hit.edu.cn

H指数:20

被引数:1,988

个人简介

现任哈尔滨工业大学能源学院副教授。2001年获哈尔滨工业大学（威海）汽车学院学士学位，2003年获哈尔滨工业大学能源学院硕士学位，2008年获哈尔滨工业大学能源学院博士学位。2009年至2014年任讲师，2015年起任副教授。研究方向为霍尔推力器设计及放电物理。主持国家自然科学基金等多项科研项目。

教育背景

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工作经历

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荣誉奖项

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Optimization of Hall Thruster With Large Height-Radius Ratio via Internally Loaded Magnetic Field and Short Channel

通过内部加载磁场和短通道对高长径比霍尔推进器进行优化

IEEE Transactions on Aerospace and Electronic Systems

IF5.7

2026-09-290

PRE

Study on the discharge characteristics of a Hall thruster operating on N₂ propellant

霍尔推进器使用N₂推进剂时的放电特性研究

Vacuum

IF3.9

2026-09-030

PRE

Effect of first-stage anode axial position on discharge characteristics of a double-stage anode layer thruster

第一级阳极轴向位置对双级阳极层推进器放电特性的影响

Advances in Space Research

IF2.8

2026-08-070

PRE

Effect of split anode–gas distributor configuration on hall-effect thruster operation with low-molecular-weight propellants

低分子量推进剂下分隔式阳极-气体分布器构型对霍尔效应推力器工作的影响

Advances in Space Research

IF2.8

2026-07-140

PRE

Design and Performance of a Lightweight, High Power Density Permanent Magnet Hall Thruster

Vacuum

IF3.9

2026-01-150

PRE

A postpartum-adapted algorithm for safe management of suspected pulmonary embolism: a retrospective cohort study

一种用于疑似肺栓塞安全管理的产后适应型算法：一项回顾性队列研究

American Journal of Obstetrics and Gynecology

IF8.4

2025-11-010

PRE

Electron Conduction and Ionization-Acceleration Decoupling in a 3kW-Class Double-Stage Anode Layer Hall Thruster: Voltage Effects Analysis

3kW级双级阳极层霍尔推进器中的电子传导与电离-加速解耦：电压效应分析

Vacuum

IF3.9

2025-10-100

PRE

Investigation of the impact of BN/graphite composite nozzles on arcjet thruster performance

BN/graphite复合喷嘴对电弧喷射推力器性能影响的研究

Vacuum

IF3.9

2025-09-150

PRE

Corrigendum to “Experimental study on abnormal spark discharge characteristics of a Hall thruster” [Acta Astronaut. 235 (2025) 653–659]

勘误表：“Hall thruster异常电火花放电特性的实验研究”[Acta Astronaut. 235 (2025) 653–659]

Acta Astronautica

IF3.4

2025-07-170

PRE

Plume focusing characteristics and optimal design of Hall thruster with large height-radius ratio

大高径比霍尔推进器的羽流聚焦特性与最优设计

Chinese Journal of Aeronautics

IF5.7

2025-07-140

OAAI

Study on the generation and acceleration characteristics of multivalent ions in Hall thruster with large height-radius ratio

大长径比霍尔推进器中多价离子产生与加速特性的研究

Vacuum

IF3.9

2025-07-050

PRE

Experimental study on abnormal spark discharge characteristics of a Hall thruster

霍尔推进器异常电火花放电特性的实验研究

Acta Astronautica

IF3.4

2025-06-160

PRE

Investigation of the effect of induced magnetic fields on Hall thruster discharge

研究感应磁场对霍尔推进器放电的影响

PLASMA SOURCES SCIENCE & TECHNOLOGY

IF3.3

2025-05-140

PRE

Application of Kriging interpolation in Hall drift current reconstruction

Kriging插值在Hall漂移电流重建中的应用

PHYSICA SCRIPTA

IF2.6

2025-04-040

PRE

Comparison of the effect of internal magnetically shielded and normal cathode on the performance of permanent magnet Hall thrusters with Krypton propellant

VACUUM

IF3.9

2025-04-010

PRE

Effects of the geometry of the inner permanent magnet cover on the discharge characteristics and cover erosion of 100-watt-class Hall thrusters

内永磁体盖的几何形状对100瓦级霍尔推力器放电特性和盖腐蚀的影响

VACUUM

IF3.9

2025-03-010

PRE

Improving specific impulse of Hall thruster by pulse power technology

利用脉冲功率技术提高霍尔推力器的比冲动

ACTA ASTRONAUTICA

IF3.4

2025-02-010

PRE

Effects of magnetic conduction ring on the discharge characteristics and the inner cover erosion of a 100 W Hall thruster

磁场传导环对100 W霍尔推进器放电特性和内罩侵蚀的影响

ADVANCES IN SPACE RESEARCH

IF2.8

2025-01-010

PRE

Effects of anode voltage and mass flow rate on the erosion of inner permanent magnet conducting cover in a 100 W Hall thruster

阳极电压和质量流量对100 W霍尔推力器内永磁导电罩腐蚀的影响

JOURNAL OF PHYSICS D-APPLIED PHYSICS

IF3.2

2024-12-270

PRE

Study on combustion characteristics of ammonium perchlorate enhanced hydroxylamine nitrate-based electronically controlled solid propellant

CHEMICAL ENGINEERING JOURNAL

IF13.2

2024-11-010

PRE