NDLI: Noss flight segment concept study

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Noss flight segment concept study

Content Provider	NASA Technical Reports Server (NTRS)
Copyright Year	1979
Description	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.
File Size	17436387
Page Count	196
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19810003614
Archival Resource Key	ark:/13960/t6p030501
Language	English
Publisher Date	1979-11-09
Access Restriction	Open
Subject Keyword	Astronautics (general) Engineering Drawings Satellite Instruments Global Positioning System Tdr Satellites Space Shuttle Payloads Telemetry Oceanographic Parameters Maritime Satellites Systems Engineering Transfer Orbits Satellite Design Marine Meteorology Mission Planning Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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