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.
Noss Flight Segment Concept Study
1979
196 pages
Report
Keine Angabe
Englisch
Unmanned Spacecraft , Astronautics , 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 orbits
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