The Reliability Modeling and Evaluation of a Cusped Field Thruster When Undertaking a Gravitational Wave Detection Mission

被引:0
作者
Chen, Yu [1 ]
Wu, Jianing [2 ]
Shen, Yan [1 ,3 ]
Cao, Shuai [1 ,3 ]
机构
[1] Sun Yat Sen Univ, Sch Aeronaut & Astronaut, Shenzhen 518107, Peoples R China
[2] Sun Yat Sen Univ, Sch Adv Mfg, Shenzhen 518107, Peoples R China
[3] Sun Yat Sen Univ, Sch Aeronaut & Astronaut, Shenzhen Key Lab Intelligent Microsatellite Conste, Shenzhen 518107, Peoples R China
关键词
cusped field thruster; reliability; failure physics; small sample; gravitational wave detection mission; EROSION;
D O I
10.3390/aerospace11050329
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The propulsion system, particularly electric propulsion, holds immense significance in the context of gravitational wave detection missions. One of the key factors of a deep space exploration mission is the lifetime of the electric propulsion. Ensuring the high reliability of the propulsion system is of paramount importance; however, achieving this is challenging in the absence of adequate failure data. Conducting ground tests for a thruster tends to encounter two limitations: a lack of failure data and time constraints. To address these challenges, we propose a semi-physics sputtering method that combines a physical erosion model with empirical processes. In this study, we focus on evaluating the lifespan of a cusped field thruster (CFT) for potential application in gravitational wave detection missions. Our analysis revolves around modeling non-conservative forces in a space environment and examining their impact on a thruster's longevity. The results indicate that, in gravitational wave missions, the survival rate of a thruster's lifespan at 8000 h is 0.75. At a constant voltage of 500 V, the maximum corrosion depth after 5000 h is 3.1 mm, while the minimum is 0.49 mm.
引用
收藏
页数:16
相关论文
共 32 条
  • [1] Amaro-Seoane P, 2017, Arxiv, DOI arXiv:1702.00786
  • [2] Hall-Effect Thrusters for Deep-Space Missions: A Review
    Bapat, Archit
    Salunkhe, Pramod B.
    Patil, Aakash, V
    [J]. IEEE TRANSACTIONS ON PLASMA SCIENCE, 2022, 50 (02) : 189 - 202
  • [3] Review of Plasma-Induced Hall Thruster Erosion
    Brown, Nathan P.
    Walker, Mitchell L. R.
    [J]. APPLIED SCIENCES-BASEL, 2020, 10 (11):
  • [4] Performance and plume evolutions during the lifetime test of a Hall-effect thruster
    Cao, Shuai
    Wang, Xuan
    Ren, Junxue
    Ouyang, Ning
    Zhang, Guangchuan
    Zhang, Zhe
    Tang, Haibin
    [J]. ACTA ASTRONAUTICA, 2020, 170 : 509 - 520
  • [5] Cho S., 2012, P 48 AIAA ASME SAE A
  • [6] Courtney D.G., 2007, P 30 INT EL PROP C F
  • [7] Comparing Direct and Indirect Thrust Measurements from Passively Fed Ionic Electrospray Thrusters
    Courtney, Daniel G.
    Dandavino, Simon
    Shea, Herbert
    [J]. JOURNAL OF PROPULSION AND POWER, 2016, 32 (02) : 392 - 407
  • [8] Effects of cusped field thruster on the performance of drag-free control system
    Cui, K.
    Liu, H.
    Jiang, W. J.
    Sun, Q. Q.
    Hu, P.
    Yu, D. R.
    [J]. ACTA ASTRONAUTICA, 2018, 144 : 193 - 200
  • [9] Thrust noise cause analysis and suppression of a cusped field thruster
    Cui, Kai
    Liu, Hui
    Jiang, Wenjia
    Yu, Daren
    [J]. ACTA ASTRONAUTICA, 2021, 179 : 322 - 329
  • [10] Danzmann K, 1997, CLASSICAL QUANT GRAV, V14, P1399, DOI 10.1088/0264-9381/14/6/002