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
  • [21] Evaluation of Exergy Efficiency Optimization of Space Launch Vehicles
    White, Christopher J. J.
    Dyas, Jeffrey E. E.
    Mesmer, Bryan L. L.
    JOURNAL OF AEROSPACE INFORMATION SYSTEMS, 2023, 20 (07): : 426 - 436
  • [22] Comparison of basic launch vehicles of leading space countries
    Korotkiy, YG
    SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM - 1998, PTS 1-3: 1ST CONF ON GLOBAL VIRTUAL PRESENCE; 1ST CONF ON ORBITAL TRANSFER VEHICLES; 2ND CONF ON APPLICAT OF THERMOPHYS IN MICROGRAV; 3RD CONF ON COMMERCIAL DEV OF SPACE; 3RD CONF ON NEXT GENERAT LAUNCH SYST; 15TH SYMP ON SPACE NUCL POWER AND PROPULSION, 1998, (420): : 943 - 948
  • [23] Rigid body separation dynamics for space launch vehicles
    Rao, B.N.
    Jeyakumar, D.
    Biswas, K.K.
    Swaminathan, S.
    Janardhana, E.
    Aeronautical Journal, 2006, 110 (1107): : 289 - 302
  • [24] 文献“Environmental Testing for Launch and Space Vehicles”点评
    冯振兴
    航天器环境工程, 2007, (01) : 54 - 62
  • [25] A Generalized Staging Optimization Program For Space Launch Vehicles
    Civek-Coskun, Ezgi
    Ozgoren, Kemal
    PROCEEDINGS OF 6TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES (RAST 2013), 2013, : 857 - 862
  • [26] Rigid body separation dynamics for space launch vehicles
    Rao, BN
    Jeyakumar, D
    Biswas, KK
    Swaminathan, S
    Janardhana, E
    AERONAUTICAL JOURNAL, 2006, 110 (1107): : 289 - 302
  • [27] Aircraft operability methods applied to space launch vehicles
    Young, D
    SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM, PTS 1-3: 1ST CONFERENCE ON FUTURE SCIENCE & EARTH SCIENCE MISSIONS; 1ST CONFERENCE ON SYNERGISTIC POWER & PROPULSION SYSTEMS TECHNOLOGY; 1ST CONFERENCE ON APPLICATIONS OF THERMOPHYSICS IN MICROGRAVITY; 2ND CONFERENCE ON COMMERCIAL DEVELOPMENT OF SPACE; - 2ND CONFERENCE ON NEXT GENERATION LAUNCH SYSTEMS; 14TH SYMPOSIUM ON SPACE NUCLEAR POWER AND PROPULSION, 1997, (387): : 1151 - 1153
  • [28] Stability analysis of explicit guidance laws for space launch vehicles with varying thrust integrals
    Song, Eun-Jung
    Cho, Sang-bum
    Park, Chang-Su
    Roh, Woong-Rae
    Joh, Miok
    ADVANCES IN SPACE RESEARCH, 2011, 48 (01) : 133 - 145
  • [29] Performance analysis of IMU-augmented GNSS tracking systems for space launch vehicles
    Braun, Benjamin
    Markgraf, Markus
    Montenbruck, Oliver
    CEAS SPACE JOURNAL, 2016, 8 (02) : 117 - 133
  • [30] Improved iterative guidance method for launch vehicles
    Ma Z.
    Xu Z.
    Tang S.
    Zhang Q.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2021, 42 (02):