Physics
Scientific paper
May 1985
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1985p%26ss...33..479m&link_type=abstract
Planetary and Space Science (ISSN 0032-0633), vol. 33, May 1985, p. 479-491. Research sponsored by the Science and Engineering R
Physics
4
Circular Orbits, Gas-Solid Interfaces, Lift, Orbit Perturbation, Satellite Orbits, Ers-1 (Esa Satellite), Euler-Lagrange Equation, Flat Surfaces, Satellite Drag, Satellite Orientation, Skylab 1, Solar Activity Effects, Solar Collectors
Scientific paper
A theory is developed to evaluate the effect of aerodynamic lift on near circular satellite orbits. Consideration is given to a flat surface at constant altitude with respect to the velocity vector; and a sun oriented plate. In both cases the gas-surface interaction was restricted to diffuse or specular reflection. Numerical results are also presented for the nominal orbit of the ERS 1 satellite. It is shown that radial perturbations of the order of 1 cm every 5 days are likely during periods of moderate solar activity. During periods of high solar activity, however, a 10-fold increase in the severity of the effect is predicted. The effects of aerodynamic lift on stabilized satellites at altitudes of less than 800 km are illustrated in a hypothetical study of the orbital inclination of Skylab 1.
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