The new NASA orbital debris engineering model ORDEM2000

被引:0
|
作者
Liou, JC
Matney, M
Anz-Meador, P
Kessler, DJ
Jansen, M
Theall, JR
机构
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
A new orbital debris engineering model, ORDEM2000, has been developed by the Orbital Debris Program Office at NASA Johnson Space Center. The new model uses a more rigorous mathematical method to derive debris populations from observation and measurement data. It also uses a direct approach to build the debris environment. This new approach eliminates several limitations and assumptions utilized in the previous model (ORDEM96). The new model provides a better description of the current debris environment than ORDEM96 does. It is expected that ORDEM2000 will soon replace ORDEM96 as the standard model to evaluate the debris risk for the International Space Station (ISS) and for future Shuttle missions.
引用
收藏
页码:309 / 313
页数:5
相关论文
共 50 条
  • [41] Internal effects model for spacecraft modules perforated by orbital debris
    Schonberg, WP
    Serrano, J
    Williamsen, JE
    JOURNAL OF SPACECRAFT AND ROCKETS, 1997, 34 (03) : 325 - 333
  • [42] Adapting a Ground-Based Laser Ranging System at NASA-GSFC for Identification and Tracking of Orbital Debris
    Coyle, D. Barry
    Stysley, Paul R.
    McGarry, Jan F.
    Hull, Scott M.
    Getzandanner, Kenneth M.
    Young, Romae P.
    LASER RADAR TECHNOLOGY AND APPLICATIONS XVIII, 2013, 8731
  • [43] EXTENSION OF A SIMPLE MATHEMATICAL MODEL FOR ORBITAL DEBRIS PROLIFERATION AND MITIGATION
    Lafleur, Jarret M.
    SPACEFLIGHT MECHANICS 2011, PTS I-III, 2011, 140 : 1037 - +
  • [44] Development of orbital debris environment model in the low earth orbit
    Uramoto, K
    Hanada, T
    SPACE ACTIVITIES AND COOPERATION CONTRIBUTING TO ALL PACIFIC BASIN COUNTRIES, 2004, 117 : 927 - 938
  • [45] Tracking and data relay satellites H, I, J compliance with NASA's orbital debris policy: A case study
    Gagosian, JS
    Furber, RD
    Malek, SC
    GUIDANCE AND CONTROL 1997, 1997, 94 : 119 - 130
  • [46] Some consequences of force model uncertainty on probability of collision with orbital debris
    Akella, MR
    Junkins, JL
    Alfriend, KT
    ASTRODYNAMICS 1997, 1998, 97 : 111 - 121
  • [47] Some consequences of force model uncertainty on probability of collision with orbital debris
    Akella, Maruthi R.
    Junkins, John L.
    Alfriend, Kyle T.
    Journal of the Chinese Society of Mechanical Engineers, Transactions of the Chinese Institute of Engineers, Series C/Chung-Kuo Chi Hsueh Kung Ch'eng Hsuebo Pao, 1998, 19 (01): : 1 - 7
  • [48] A minimalist empirical orbital debris/meteoroid hazard model for the space shuttle
    Matney, Mark
    Christiansen, Eric
    SPACE DEBRIS AND SPACE TRAFFIC MANAGEMENT SYMPOSIUM 2005, 2006, 112 : 109 - +
  • [49] Sensitivity analysis of the orbital debris environment using the EVOLVE 4.0 model
    Reynolds, R
    Eichler, P
    Bade, A
    Krisko, P
    Johnson, N
    SPACE DEBRIS, 1999, 23 (01): : 175 - 185
  • [50] Engineering model to avoid debris flight in the event of contact detonation
    Zircher, Tobias
    BETON- UND STAHLBETONBAU, 2022, 117 (10) : 805 - 811