Noss Flight Segment Concept Study

机译：Noss飞行段概念研究

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An 11 ft wide by 26.5 ft long flat structure weighing almost 14,469 pounds evolved during a low level, inhouse conceptual design study for a national oceanic satellite system spacecraft that would stow directly in the space shuttle. Following STS launch to a 300 Km mission orbit inclination, transfer will be effected to a 800 Km Sun synchronous circular orbit. The instrument completement includes 2 altimeters, 1 scatterometer, 1 large antenna multichannel microwave radiometer, and a coastal zone scanner. The spacecraft, its instruments, and interfaces with STS and TDRSS are described. The mission timeline, potential problem areas, system drivers, and recommended study areas are discussed. Drawings and system block diagrams are included.

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作者
Tiuri, M.; Urpo, S.;
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年度 1979
页码 p.1-196
总页数 196
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Maritime satellites; Mission planning; Oceanographic parameters; Satellite design; Space shuttle payloads; Systems engineering; Engineering drawings; Global positioning system; Marine meteorology; Satellite instruments; Tdr satellites; Telemetry; Transfer orbi;

机译：海上卫星;任务规划;海洋参数;卫星设计;航天飞机有效载荷;系统工程;工程图;全球定位系统;海洋气象学;卫星仪器; Tdr卫星;遥测;转移orbi;

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Noss Flight Segment Concept Study

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