Lifetime of the Rohini A satellite

Details Lifetime of the Rohini A satellite Lifetime of the Rohini A satellite

Oct 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991baicz..42..295s&link_type=abstract

Astronomical Institutes of Czechoslovakia, Bulletin (ISSN 0004-6248), vol. 42, no. 5, Oct. 1991, p. 295-297.

Statistics

Computation

4

Orbit Decay, Satellite Drag, Satellite Lifetime, Atmospheric Models, Orbital Elements, Satellite Orbits, Thermosphere

Scientific paper

The second-order theory of drag effects is developed on the basis of the
model of the thermosphere total density distribution TD88. The
usefulness of the theory is illustrated by the computation of the Rohini
A satellite lifetime.

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