Informed maintenance for next generation reusable launch systems

被引:4
|
作者
Fox, JJ [1 ]
Gormley, TJ [1 ]
机构
[1] NASA, Kennedy Space Ctr, Kennedy Space Ctr, FL 32899 USA
关键词
D O I
10.1016/S0094-5765(01)00064-9
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Perhaps the most substantial single obstacle to progress of space exploration and utilization of space for human benefit is the safety & reliability and the inherent cost of launching to, and returning from, space. The primary influence in the high costs of current launch systems (the same is true for commercial and military aircraft and most other reusable systems) is the operations, maintenance and infrastructure portion of the program's total life cycle costs. Reusable Launch Vehicle (RLV) maintenance and design have traditionally been two separate engineering disciplines with often conflicting objectives - maximizing ease of maintenance versus optimizing performance, size and cost. Testability analysis, an element of Informed Maintenance (IM), has been an ad hoc, manual effort, in which maintenance engineers attempt to identify an efficient method of troubleshooting for the given product, with little or no control over product design. Therefore, testability deficiencies in the design cannot be rectified. It is now widely recognized that IM must be engineered into the product at the design stage itself, so that an optimal compromise is achieved between system maintainability and performance. The elements of IM include testability analysis, diagnostics/prognostics, automated maintenance scheduling, automated logistics coordination, paperless documentation and data mining. IM derives its heritage from complimentary NASA science, space and aeronautic enterprises such as the on-board autonomous Remote Agent Architecture recently flown on NASA's Deep Space 1 Probe as well as commercial industries that employ quick turnaround operations. Commercial technologies and processes supporting NASA's IM initiatives include condition based maintenance technologies from Boeing's Commercial 777 Aircraft and Lockheed-Martin's F-22 Fighter, automotive computer diagnostics and autonomous controllers that enable 100,000 mile maintenance free operations, and locomotive monitoring system software. This paper will summarize NASA's long-term strategy, development, and implementation plans for Informed Maintenance for next generation RLVs. This will be done through a convergence into a single IM vision the work being performed throughout NASA, industry and academia. Additionally, a current status of IM development throughout NASA programs such as the Space Shuttle, X-33, X-34 and X-37 will be provided and will conclude with an overview of near-term work that is being initiated in FY00 to support NASA's 2(nd) Generation Reusable Launch Vehicle Program. (C) 2001 AIAA. Published by Elsevier Science Ltd.
引用
收藏
页码:439 / 449
页数:11
相关论文
共 50 条
  • [21] Reusable launch vehicle
    Aerospace Engineering (Warrendale, Pennsylvania), 1994, 14 (05):
  • [22] REUSABLE LAUNCH VEHICLES
    RUPPE, HO
    SPACE POLICY, 1985, 1 (03) : 339 - 340
  • [23] Fault-tolerant optimal trajectory generation for reusable launch vehicles
    Shaffer, Patrick J.
    Ross, I. Michael
    Oppenheimer, Michael W.
    Doman, David B.
    Bollino, Kevin P.
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2007, 30 (06) : 1794 - 1802
  • [24] Footprint generation for reusable launch vehicles using a direct pseudospectral method
    Fahroo, F
    Doman, DB
    Ngo, AD
    PROCEEDINGS OF THE 2003 AMERICAN CONTROL CONFERENCE, VOLS 1-6, 2003, : 2163 - 2168
  • [25] Who will fly the next-generation launch vehicle?
    Nelson, DA
    AEROSPACE AMERICA, 1999, 37 (04) : 30 - +
  • [26] Robust Approach and Landing Trajectory Generation for Reusable Launch Vehicles in Winds
    Jiang, Zhesheng
    Ordonez, Raul
    2008 IEEE INTERNATIONAL CONFERENCE ON CONTROL APPLICATIONS, VOLS 1 AND 2, 2008, : 158 - 163
  • [28] Improving safety and reliability of next generation launch vehicles
    Maggio, G
    Pelaccio, DG
    Cook, SA
    Anderson, DM
    SPACE SAFETY, RESCUE AND QUALITY 1999-2000, 2001, 102 : 131 - 141
  • [29] Next Generation Avionics System Of Future Launch Vehicle
    Qi, Guangping
    Duan, Ran
    Sun, Haifeng
    Zhou, Hu
    Xiang, Zongyou
    Li, Wenting
    PROCEEDINGS OF THE 2015 JOINT INTERNATIONAL MECHANICAL, ELECTRONIC AND INFORMATION TECHNOLOGY CONFERENCE (JIMET 2015), 2015, 10 : 1215 - 1219
  • [30] Commercialization and internationalization of the next-generation launch system
    Bille, MA
    Richie, GE
    Bille, DA
    SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM (STAIF-96), PTS 1-3: 1ST CONFERENCE ON COMMERCIAL DEVELOPMENT OF SPACE; 1ST CONFERENCE ON NEXT GENERATION LAUNCH SYSTEMS; 2ND SPACECRAFT THERMAL CONTROL SYMPOSIUM; 13TH SYMPOSIUM ON SPACE NUCLEAR POWER AND PROPULSION - FUTURE SPACE AND EARTH SCIENCE MISSIONS - SPECIAL TOPIC; REMOTE SENSING FOR COMMERCIAL, CIVIL AND SCIENCE APPLICATIONS - SPECIAL TOPIC, 1996, (361): : 521 - 526