VISUALIZATION AND VERIFICATION METHOD FOR FAILURE NETWORK ANALYSIS OF SPACE LAUNCH VEHICLES

被引:0
|
作者
Fujimoto, Keiichiro [1 ]
Oyama, Akira [1 ]
Fujii, Kozo [1 ]
Iizuka, Nobuyuki
Okita, Koichi
机构
[1] Japan Aerosp Explorat Agcy, JAXAs Digital Innovat Ctr, Sagamihara, Kanagawa 2298510, Japan
关键词
Failure mode and effect analysis; fault tree analysis; failure network analysis; component interface; failure propagation; rocket engine; N2; chart;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Comprehensive failure network analysis method was studied for liquid rocket engine development which includes failure propagation through various types of component interfaces in order to achieve exhaustive enumeration of possible failures and to identify actions to eliminate or reduce the potential failure. New failure network visualization method was developed in order to make it easier to understand complicated failure propagation mechanism among multiple system levels. Verification analysis method is developed in which it is verified all of user-specified component interfaces are contained in the failure network analysis result. The perceived component interface is specified by the analyzer and the failure propagation in the result of failure analysis is summarized in two separate N2 charts. By comparing with these two N2 charts, unperceived component interface and the unconsidered failure propagation can be found. It is found to be promising approach to achieve exhaustive enumeration especially for forgettable component interface.
引用
收藏
页码:977 / 982
页数:6
相关论文
共 50 条
  • [31] The UKS path to launch: The national space technology strategy for launch technologies, vehicles and services
    Bradford, Andy
    Davies, Phil
    Ratcliffe, Andy
    Baker, Adam
    Bennett, Andy
    JBIS - Journal of the British Interplanetary Society, 2017, 70 (09): : 313 - 318
  • [32] CHOICE OF A FAMILY OF LAUNCH VEHICLES FOR A MULTIPLE-LAUNCH SPACE RESEARCH PROGRAM.
    Sollogub, A.V.
    Ofitserov, V.P.
    1978, 16 (04): : 420 - 426
  • [33] SPACE LAUNCHERS - LAUNCH FAILURE - BOARDROOM FRACAS
    WALGATE, R
    NATURE, 1986, 321 (6070) : 549 - 549
  • [34] LAUNCH FAILURE DENTS INDIA SPACE PLANS
    JAYARAMAN, KS
    NATURE, 1993, 365 (6445) : 382 - 382
  • [35] A Neural Network Adaptive Fault-Tolerant Control Method for Launch Vehicles with the Limited Faults
    Zhu H.
    Wu Y.
    Rong Y.
    Qin X.
    Chen Y.
    Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2020, 38 (03): : 668 - 676
  • [36] A MODERN LOAD RELIEF GUIDANCE SCHEME FOR SPACE LAUNCH VEHICLES
    Orr, Jeb S.
    Russell, Colter W.
    PROCEEDINGS OF THE 44TH ANNUAL AMERICAN ASTRONAUTICAL SOCIETY GUIDANCE, NAVIGATION, AND CONTROL CONFERENCE, AAS 2022, 2024, : 755 - 774
  • [37] A review of flaws and damage in space launch vehicles: Motors and engines
    Dhital, Dipesh
    Lee, Jung R.
    Farrar, Charles
    Mascarenas, David
    JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2014, 25 (05) : 524 - 540
  • [38] LONG-RANGE PLANNING FOR LAUNCH VEHICLES IN SPACE PROGRAM
    WELLER, AE
    FLETCHER, BL
    BATTELLE TECHNICAL REVIEW, 1967, 16 (12): : 3 - &
  • [39] Cryogenic Moisture Uptake in Foam Insulation for Space Launch Vehicles
    Fesmire, James E.
    Coffman, Brekke E.
    Sass, Jared P.
    Williams, Martha K.
    Smith, Trent M.
    Meneghelli, Barry J.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2012, 49 (02) : 220 - 230
  • [40] SPACE ROTOR - A EUROPEAN PROJECT FOR RECOVERY OF HEAVY LAUNCH VEHICLES
    KRETZ, M
    SPACEFLIGHT, 1966, 8 (10): : 369 - &