Abstract
The effect of atmospheric drag on a satellite makes it possible to measure atmospheric density. Two approaches have been proposed: (1) Accelerometers may be mounted in the satellite to measure the vehicle acceleration which, together with the satellite mass, determines the drag force; (2) Alternatively, a drag-free satellite control system may be used. In this approach, an unsupported, shielded proof mass is used as a reference. The satellite is forced to follow the proof mass by thrustors which are actuated whenever the satellite approaches the proof mass. The proof mass is shielded by the satellite and is therefore free of drag, and the satellite follows the same orbit. Therefore, the control thrust must equal the drag force on the average. By measuring the control, the drag can be determined. Each approach has advantages and disadvantages. The relative measurement accuracy and bandwidth, calibration techniques, operating convenience and the effect of orbit longevity as a function of payload are discussed.
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© 1970 D. Reidel Publishing Company, Dordrecht, Holland
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DeBra, D.B. (1970). A Comparison of Satellite Drag Measurement Techniques. In: Partel, G.A. (eds) Space Engineering. Astrophysics and Space Science Library, vol 15. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-7551-7_39
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DOI: https://doi.org/10.1007/978-94-011-7551-7_39
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