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Empirical Parameters Determining the Lifetime of Artificial Earth Satellites

H. B. Wackernagel
Empirical Parameters Determining the Lifetime of Artificial Earth Satellites by H. B. Wackernagel PDF

Author : H. B. Wackernagel
Publisher :
Page : 8 pages
File Size : 15,50 MB
Release : 1959
Category : Artificial satellites
ISBN :

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The decay of the orbit of most artificial earth satellites can be described by the simple formula log N = R (log delta P sub N + Q) N is the revolution number reckoned backwards from the revolution of decay and delta P sub N a quantity defined in the text. The parameters R and Q are correlated to the ratio m/F of mass and effective cross section and to the height of the perigee q, respectively. (Author).

Determination of the Orbital Parameters of Artificial Satellites on the Basis of Observations from the Earth's Surface

T. M. ENEEV
Determination of the Orbital Parameters of Artificial Satellites on the Basis of Observations from the Earth's Surface by T. M. ENEEV PDF

Author : T. M. ENEEV
Publisher :
Page : 25 pages
File Size : 37,96 MB
Release : 1961
Category :
ISBN :

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Methods are presented for the determination of the orbital elements of a satellite and of the analysis of its motion on the basis of the processing of optical and radar observation data. The methods are designed for the utilization of high speed electronic computing machines. (Author).