The AMPTE IRM Spacecraft

The AMPTE Ion Release Module (IRM) together with the other two AMPTE spacecraft, UKS and CCE, were successfully launched with a Delta 3924 vehicle on August 16, 1984 from Cape Canaveral, Florida. The IRM satellite was designed, built, and tested by the Max-Planck-Institut für extraterrestrische Phys...

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Veröffentlicht in:IEEE transactions on geoscience and remote sensing 1985-05, Vol.GE-23 (3), p.192-201
Hauptverfasser: Hausler, B., Melzner, F., Stocker, J., Valenzuela, A., Bauer, O. H., Parigger, P., Sigritz, K., Schoning, R., Seidenschwang, E., Eberl, F., Kaiser, K.-h., Lieb, W., Merz, B., Pagel, U., Wiezorrek, E., Genzel, J. P.
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Sprache:eng
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Zusammenfassung:The AMPTE Ion Release Module (IRM) together with the other two AMPTE spacecraft, UKS and CCE, were successfully launched with a Delta 3924 vehicle on August 16, 1984 from Cape Canaveral, Florida. The IRM satellite was designed, built, and tested by the Max-Planck-Institut für extraterrestrische Physik. It carries 16 barium and lithium release containers and a plasna diagnostic instrument set. This paper discusses the requirements imposed on the spacecraft design by the mission and the scientific instruments and gives a description of the major spacecraft systems. Finally, a short summary of the first events in the mission is presented.
ISSN:0196-2892
1558-0644
DOI:10.1109/TGRS.1985.289513