NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Earth Reflected Solar Radiation Input to Spherical SatellitesA general calculation is given for the earth's albedo input to a spherical satellite, with the assumption that the earth can be considered a diffusely reflecting sphere. The results are presented in general form so that appropriate values for the solar constant and albedo of the earth can be used as more accurate values become available. The results are also presented graphically; the incident power is determined on the assumption that the mean solar constant is 1.353 x 10( exp 6) erg/(sq cm.sec) and the albedo of the earth is 0.34.
Document ID
19980227781
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Note (TN)
Authors
Cunningham, F. G.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1961
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TN-D-1099
Report Number: NASA-TN-D-1099
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available