首页> 美国政府科技报告 >SPACE SHUTTLE SORTIE PAYLOAD CREW SAFETY AND SYSTEMS COMPATIBILITY CRITERIA VOLUME III - SYSTEMS COMPATIBILITY DESIGN AND VERIFICATION CRITERIA
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SPACE SHUTTLE SORTIE PAYLOAD CREW SAFETY AND SYSTEMS COMPATIBILITY CRITERIA VOLUME III - SYSTEMS COMPATIBILITY DESIGN AND VERIFICATION CRITERIA

机译:spaCE sHUTTLE sORTIE paYLOaD船员安全和系统兼容性标准第III卷 - 系统兼容性设计和验证标准

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This study final report is submitted to NASA/JSC by TRW Systems Group in accordance with contract NAS9-12741. As part of the effort to reduce the costs of shuttle payloads, this sture was performed to determine the minimum, mandatory design and verification criteria necessary to insure that sortie payloads are compatible with the space shuttie system;distinguishing them from those criteria related primarily to mission success, configuration choices, management prerogatives, or other cost-benefit variables which are, therefore, discretionary to payload project management. Results from an investigation of past practices in spacecraft and aircraft programs served as a baseline of information used to identify and determine candidate criteria and also to develop a design and verification categorization methodology which distinguishes candidate criteria as mandatory or discretionary. This study concluded that utilization of the mandatory design criteria, presented in this report, as the basis for sortie payload specifications will produce basic systems compatibility between the orbiter and its sortie payloads at reduced costs. Also, when additional criteria are generated due to changes in subsystems, designs, or guideline the categorization methodology developed can aid managerial decision-making concerning these criteria. To a limited degree, the compatibility criteria as defined in this study reflect a portion of the total system safety effort involved in a manned space program.

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  • 作者单位
  • 年度 1973
  • 页码 1-75
  • 总页数 75
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 工业技术;
  • 关键词

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