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A geopause satellite system conceptA typical Geopause satellite orbit has a 14 hour period, a mean height of about 4.6 earth radii, and is nearly circular, polar, and normal to the ecliptic. At this height only a relatively few gravity terms have uncertainties corresponding to orbital perturbations above the decimeter level. The orbit is at the geopotential boundary, the geopause. The few remaining environmental quantities which may be significant can be determined by means of orbit analysis and accelerometers. The Geopause satellite system also provides the tracking geometry and coverage needed for determining the orbit, the tracking system biases and the station locations. Five or more fundamental stations well distributed in longitude can view Geopause over the North Pole. Geopause also provides the basic capability for satellite-to-satellite tracking of drag-free satellites for mapping the gravity field and altimeter satellites for surveying the sea surface topography.
Document ID
19740007431
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Siry, J. W.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1971
Subject Category
Space Vehicles
Report/Patent Number
X-550-71-503
NASA-TM-X-70548
Report Number: X-550-71-503
Report Number: NASA-TM-X-70548
Meeting Information
Meeting: Intern. Symp. on the use of Artificial Satellites for Geodesy
Location: Washington, DC
Country: United States
Start Date: April 1, 1971
Sponsors: Am. Geophys. Union
Accession Number
74N15544
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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