Interaction potential between atomic oxygen and polymer surfaces in Low Earth Orbit

被引:0
|
作者
Chen, Laiwen [1 ]
Lee, Chun-Hian [1 ]
机构
[1] Beijing Univ Aeronaut & Astronaut, Natl Lab Computat Fluid Dynam, Beijing 100083, Peoples R China
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In the present work, an interaction potential between an incident reactive particle and a. material surface is constructed. The potential is formulated based on the unit bond index-quadratic exponential potential model and two adjustable factors characterizing the correlations of equilibrium-length scales and of attractive potential. In addition, the effective potential between monomers is obtained by Lifshitz's theory. The interaction of atomic oxygen with Kapton(R) is computed as a test case using the potential functions developed in the present paper in conjunction with the molecular dynamic model constructed by Lee and Chen (Lee, C.-H., and Chen, L. W., "Reactive Probability of Atomic Oxygen with Material Surfaces in Low Earth Orbit," Journal of Spacecraft and Rockets, Vol. 37, No. 2, 2000, pp. 252-256). The reactive probability computed by the present model is found to be 16.8% lower than for the STS-46 flight data, and the law of the incident angle-dependency deduced from the flight data is also confirmed by the numerical simulation. The numerical value of the accommodation factor computed in this task is 0.1368, which lies between the values of 0.1165, computed via the hard-sphere model, and 0.68, obtained from the ground test for atomic oxygen interacting with Kapton at an impingement angle of 45 deg and energy of 1.5 eV. The effects of the two adjustable factors given in. the potential model are also briefly discussed.
引用
收藏
页码:487 / 496
页数:10
相关论文
共 50 条
  • [21] THE MATERIALS CHEMISTRY OF ATOMIC OXYGEN - LOW-EARTH-ORBIT AND THE LABORATORY
    KOONTZ, SL
    CROSS, JB
    ABSTRACTS OF PAPERS OF THE AMERICAN CHEMICAL SOCIETY, 1993, 206 : 55 - IEC
  • [22] Atomic-oxygen undercutting of protected polymers in low earth orbit
    Banks, BA
    Snyder, A
    Miller, SK
    de Groh, KK
    Demko, R
    JOURNAL OF SPACECRAFT AND ROCKETS, 2004, 41 (03) : 335 - 339
  • [23] A comparison of atomic oxygen degradation in low earth orbit and in a plasma etcher
    Townsend, JA
    19TH SPACE SIMULATION CONFERENCE: COST EFFECTIVE TESTING FOR THE 21ST CENTURY, 1996, 3341 : 249 - 258
  • [24] Atomic Oxygen Environment Analysis Technology for Low Earth Orbit Spacecraft
    An Jing
    Zhang Wei
    Yang Dongsheng
    2017 PROGNOSTICS AND SYSTEM HEALTH MANAGEMENT CONFERENCE (PHM-HARBIN), 2017, : 646 - 650
  • [25] Property changes in materials due to atomic oxygen in the low Earth orbit
    Goto, Aki
    Umeda, Kaori
    Yukumatsu, Kazuki
    Kimoto, Yugo
    CEAS SPACE JOURNAL, 2021, 13 (03) : 415 - 432
  • [26] INFLUENCE OF ATOMIC OXYGEN ON SPACE TRIBOLOGY IN A LOW-EARTH-ORBIT
    OHMAE, N
    WEAR, 1993, 168 (1-2) : 99 - 103
  • [27] Synergistic effects of atomic oxygen and thermal cycling in low earth orbit on polymer-matrixed space material
    Zhai, Ruiqiong
    Yang, Xiaoning
    Jiang, Lixiang
    Gao, Hong
    Zhang, Yuxin
    Jiao, Zilong
    HELIYON, 2023, 9 (08)
  • [28] Use of quartz crystal microbalance on the polymer degradation studies regarding atomic oxygen activities in low earth orbit
    Tagawa, M
    Yokota, K
    Kinoshita, H
    Ohmae, N
    PROCEEDINGS OF THE 9TH INTERNATIONAL SYMPOSIUM ON MATERIALS IN A SPACE ENVIRONMENT, 2003, 540 : 247 - 252
  • [29] Erosion of surfaces in low earth orbit by atomic oxygen:: KMC simulation of graphite+O(3P).
    Kelly, KL
    Tully, JC
    ABSTRACTS OF PAPERS OF THE AMERICAN CHEMICAL SOCIETY, 2003, 226 : U320 - U320
  • [30] Issues and consequences of atomic oxygen undercutting of protected polymers in low Earth orbit
    Banks, BA
    Snyder, A
    Miller, SK
    Demko, R
    PROTECTION OF MATERIALS AND STRUCTURES FROM SPACE ENVIRONMENT, 2003, 5 : 235 - 243