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Satellite drags on Emcore


Publisher
Elsevier Science
Year
2003
Tongue
English
Weight
106 KB
Volume
16
Category
Article
ISSN
0961-1290

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Two methods have been used to compute and compare the perturbations in perigee distance for an artificial Earth satellite. The two methods have used different air density models. The first (Helali, 1987) used the TD model, formulated by Sehnel(1986a), which contains terms that describe all the princ