• Medientyp: E-Artikel; Sonstige Veröffentlichung
  • Titel: A Dual-Species Atom Interferometer Payload for Operation on Sounding Rockets
  • Beteiligte: Elsen, Michael [VerfasserIn]; Piest, Baptist [VerfasserIn]; Adam, Fabian [VerfasserIn]; Anton, Oliver [VerfasserIn]; Arciszewski, Paweł [VerfasserIn]; Bartosch, Wolfgang [VerfasserIn]; Becker, Dennis [VerfasserIn]; Bleeke, Kai [VerfasserIn]; Böhm, Jonas [VerfasserIn]; Boles, Sören [VerfasserIn]; Döringshoff, Klaus [VerfasserIn]; Guggilam, Priyanka [VerfasserIn]; Hellmig, Ortwin [VerfasserIn]; Imwalle, Isabell [VerfasserIn]; Kanthak, Simon [VerfasserIn]; Kürbis, Christian [VerfasserIn]; Koch, Matthias [VerfasserIn]; Lachmann, Maike Diana [VerfasserIn]; Mihm, Moritz [VerfasserIn]; Müntinga, Hauke [VerfasserIn]; Nepal, Ayush Mani [VerfasserIn]; Oberschulte, Tim [VerfasserIn]; Ohr, Peter [VerfasserIn]; Papakonstantinou, Alexandros [VerfasserIn]; [...]
  • Erschienen: Heidelberg : Springer, 2023
  • Erschienen in: Microgravity Science and Technology 35 (2023), Nr. 5 ; Microgravity Science and Technology
  • Ausgabe: published Version
  • Sprache: Englisch
  • DOI: https://doi.org/10.15488/16231; https://doi.org/10.1007/s12217-023-10068-7
  • Schlagwörter: Microgravity ; Atom interferometry ; Bose-Einstein condensate ; Atom optics ; Sounding rocket ; Quantum optics
  • Entstehung:
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  • Beschreibung: We report on the design and the construction of a sounding rocket payload capable of performing atom interferometry with Bose-Einstein condensates of 41 K and 87 Rb. The apparatus is designed to be launched in two consecutive missions with a VSB-30 sounding rocket and is qualified to withstand the expected vibrational loads of 1.8 g root-mean-square in a frequency range between 20–2000 Hz and the expected static loads during ascent and re-entry of 25 g. We present a modular design of the scientific payload comprising a physics package, a laser system, an electronics system and a battery module. A dedicated on-board software provides a largely automated process of predefined experiments. To operate the payload safely in laboratory and flight mode, a thermal control system and ground support equipment has been implemented and will be presented. The payload presented here represents a cornerstone for future applications of matter wave interferometry with ultracold atoms on satellites.
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