Abstract
A parachute-borne instrument package for performing measurements in the lower ionosphere between 80 and 40 km altitude has been developed by the ESTEC Space Science Department. The parachute probe is a piggy-back on Skylark rockets. It is ejected from the rocket during ascent at about 45 km height and braked by a drag parachute to an apogee of about 80 km. At this height an internal timer releases the drag parachute of 0.75 m diameter and the main parachute of 2.5 m diameter is deployed. The package descends to an altitude of 15 km where two thirds of the rigging lines are cut off by explosive bolts, triggered by a barometric switch. The package then falls rapidly to the ground, thus reducing the potential air traffic risk. A schematic view of the rocket and probe trajectories and of the sequence of events is shown in Figure 1.
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References
Berkeljon, R., Englert, G., Jaeschke, R., Köhn, D., Pedersen, A., and Scheper, R.: 1970, ‘A rocket-borne, ejectable instrument package with parachute’, ESRO TN-102 (ESTEC).
Hale, L. C., Hoult, D. P., and Baker, D. C.: 1968, in Space Research VIII, North Holland Publ. Co., Amsterdam, pp. 320–331.
Pedersen, A.: 1966, ‘Measurements of ion concentrations in the D-region of the ionosphere’, Uppsala Ionosphere Observatory, Report No. 15, pp. 9-32.
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© 1971 D. Reidel Publishing Company, Dordrecht-Holland
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Jaeschke, R., Pedersen, A. (1971). Ion Densities in the Lower D-Region Measured with a Parachuted Probe. In: Fiocco, G. (eds) Mesospheric Models and Related Experiments. Astrophysics and Space Science Library, vol 25. Springer, Dordrecht. https://doi.org/10.1007/978-94-010-3114-1_26
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DOI: https://doi.org/10.1007/978-94-010-3114-1_26
Publisher Name: Springer, Dordrecht
Print ISBN: 978-94-010-3116-5
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