Arid
报告编号NASA-CR-161143, LMSC-D614921-A-PT-1
来源IDNTRS_Document_ID: 19790009716
The 25 kW power module evolution study. Part 1: Payload requirements and growth scenarios
[unavailable]
英文摘要Payload power level requirements and their general impact on the baseline and growth versions of the 25 kW power module during the 1983 to 1990 period are discussed. Extended duration Orbiter sortie flight, supported by a power module, with increased payload power requirements per flight, and free-flyer payload missions are included. Other payload disciplines considered, but not emphasized for the 1983 to 1986 period include astrophysics/astronomy, earth observations, solar power satellite, and life sciences. Of these, only the solar power satellite is a prime driver for the power module.
英文关键词ELECTRIC POWER SUPPLIES MISSION PLANNING SPACE MISSIONS SPACE SHUTTLE PAYLOADS SPACE TRANSPORTATION SYSTEM SYSTEMS ENGINEERING COMMUNICATION SATELLITES LARGE SPACE STRUCTURES MULTIMISSION MODULAR SPACECRAFT SATELLITE CONFIGURATIONS SPACE COMMERCIALIZATION SPACE PROCESSING SPACEBORNE EXPERIMENTS SPACELAB PAYLOADS
出版年1978
报告类型Technical Report
语种英语
国家美国
URLhttp://hdl.handle.net/2060/19790009716
资源类型科技报告
条目标识符http://119.78.100.177/qdio/handle/2XILL650/258758
推荐引用方式
GB/T 7714
[unavailable]. The 25 kW power module evolution study. Part 1: Payload requirements and growth scenarios,1978.
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