Sets of equations presented may be used for calculating complete trajectories of satellites from outer space to ground under influence of air drag and gravity, including oblateness effects, and to apply these to several examples of entry trajectories starting from circular orbit.
Three-dimensional orbits of earth satellites, including effects of earth oblateness and atmospheric rotation
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 12-4-58A
1958
85 pages
Report
English
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