Details
Originalsprache | Englisch |
---|---|
Aufsatznummer | 48 |
Fachzeitschrift | Microgravity Science and Technology |
Jahrgang | 35 |
Ausgabenummer | 5 |
Publikationsstatus | Veröffentlicht - 7 Sept. 2023 |
Abstract
ASJC Scopus Sachgebiete
- Ingenieurwesen (insg.)
- Allgemeiner Maschinenbau
- Physik und Astronomie (insg.)
- Allgemeine Physik und Astronomie
- Mathematik (insg.)
- Angewandte Mathematik
- Mathematik (insg.)
- Modellierung und Simulation
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in: Microgravity Science and Technology, Jahrgang 35, Nr. 5, 48, 07.09.2023.
Publikation: Beitrag in Fachzeitschrift › Artikel › Forschung › Peer-Review
}
TY - JOUR
T1 - A Dual-Species Atom Interferometer Payload for Operation on Sounding Rockets
AU - Elsen, Michael
AU - Piest, Baptist
AU - Adam, Fabian
AU - Anton, Oliver
AU - Arciszewski, Paweł
AU - Bartosch, Wolfgang
AU - Becker, Dennis
AU - Böhm, Jonas
AU - Boles, Sören
AU - Döringshoff, Klaus
AU - Guggilam, Priyanka
AU - Hellmig, Ortwin
AU - Imwalle, Isabell
AU - Kanthak, Simon
AU - Kürbis, Christian
AU - Koch, Matthias
AU - Lachmann, Maike Diana
AU - Mihm, Moritz
AU - Müntinga, Hauke
AU - Nepal, Ayush Mani
AU - Oberschulte, Tim
AU - Ohr, Peter
AU - Papakonstantinou, Alexandros
AU - Prat, Arnau
AU - Reichelt, Christian
AU - Sommer, Jan
AU - Spindeldreier, Christian
AU - Warner, Marvin
AU - Wendrich, Thijs
AU - Wenzlawski, André
AU - Blume, Holger
AU - Braxmaier, Claus
AU - Lüdtke, Daniel
AU - Peters, Achim
AU - Rasel, Ernst Maria
AU - Sengstock, Klaus
AU - Wicht, Andreas
AU - Windpassinger, Patrick
AU - Grosse, Jens
AU - Bleeke, Kai
N1 - Funding Information: The QUANTUS IV - MAIUS project is a collaboration of Zentrum für angewandte Raumfahrttechnologie und Mikrogravitation Bremen, Leibniz Universität Hannover, Humboldt-Universität zu Berlin, Johannes Gutenberg-Universität Mainz and Ferdinand-Braun-Institut, Leibniz-Institut für Höchstfrequenztechnik. It is supported by the German Space Agency DLR with funds provided by the Federal Ministry for economic affairs and climate action (BMWK) under grant number DLR 50WP 1431-1435. We acknowledge support from Deutsches Zentrum für Luft- und Raumfahrt - Raumfahrtbetrieb, Oberpfaffenhofen, Deutsches Zentrum für Luft- und Raumfahrt - Simulations- und Softwaretechnik, Braunschweig. Funded by the Deutsche Forschungsgemeinschaft (DFG, German Research Foundation) under Germany’s Excellence Strategy - EXC-2123 QuantumFrontiers - 390837967
PY - 2023/9/7
Y1 - 2023/9/7
N2 - 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.
AB - 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.
KW - physics.atom-ph
KW - Atom interferometry
KW - Atom optics
KW - Sounding rocket
KW - Quantum optics
KW - Microgravity
KW - Bose-Einstein condensate
UR - http://www.scopus.com/inward/record.url?scp=85170042703&partnerID=8YFLogxK
U2 - 10.1007/s12217-023-10068-7
DO - 10.1007/s12217-023-10068-7
M3 - Article
VL - 35
JO - Microgravity Science and Technology
JF - Microgravity Science and Technology
SN - 0938-0108
IS - 5
M1 - 48
ER -