A Dual-Species Atom Interferometer Payload for Operation on Sounding Rockets
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 e...
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| Veröffentlicht in: | Microgravity science and technology 2023-09, Vol.35 (5), p.48, Article 48 |
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| creator | Elsen, Michael Piest, Baptist Adam, Fabian Anton, Oliver Arciszewski, Paweł Bartosch, Wolfgang Becker, Dennis Bleeke, Kai Böhm, Jonas Boles, Sören Döringshoff, Klaus Guggilam, Priyanka Hellmig, Ortwin Imwalle, Isabell Kanthak, Simon Kürbis, Christian Koch, Matthias Lachmann, Maike Diana Mihm, Moritz Müntinga, Hauke Nepal, Ayush Mani Oberschulte, Tim Ohr, Peter Papakonstantinou, Alexandros Prat, Arnau Reichelt, Christian Sommer, Jan Spindeldreier, Christian Warner, Marvin Wendrich, Thijs Wenzlawski, André Blume, Holger Braxmaier, Claus Lüdtke, Daniel Peters, Achim Rasel, Ernst Maria Sengstock, Klaus Wicht, Andreas Windpassinger, Patrick Grosse, Jens |
| description | 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. |
| doi_str_mv | 10.1007/s12217-023-10068-7 |
| format | Article |
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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.</description><identifier>ISSN: 1875-0494</identifier><identifier>ISSN: 0938-0108</identifier><identifier>EISSN: 1875-0494</identifier><identifier>DOI: 10.1007/s12217-023-10068-7</identifier><language>eng</language><publisher>Dordrecht: Springer Netherlands</publisher><subject>Aerospace Technology and Astronautics ; Atom interferometry ; Bose-Einstein condensates ; Classical and Continuum Physics ; Control equipment ; Control systems ; Engineering ; Frequency ranges ; Ground support equipment ; Ground support systems ; Interferometry ; Matter waves ; Modular design ; Sounding rockets ; Space Exploration and Astronautics ; Space Sciences (including Extraterrestrial Physics ; Static loads ; Thermal control systems ; Ultracold atoms ; Vibratory loads</subject><ispartof>Microgravity science and technology, 2023-09, Vol.35 (5), p.48, Article 48</ispartof><rights>The Author(s) 2023</rights><rights>The Author(s) 2023. 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Technol</addtitle><description>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.</description><subject>Aerospace Technology and Astronautics</subject><subject>Atom interferometry</subject><subject>Bose-Einstein condensates</subject><subject>Classical and Continuum Physics</subject><subject>Control equipment</subject><subject>Control systems</subject><subject>Engineering</subject><subject>Frequency ranges</subject><subject>Ground support equipment</subject><subject>Ground support systems</subject><subject>Interferometry</subject><subject>Matter waves</subject><subject>Modular design</subject><subject>Sounding rockets</subject><subject>Space Exploration and Astronautics</subject><subject>Space Sciences (including Extraterrestrial Physics</subject><subject>Static loads</subject><subject>Thermal control systems</subject><subject>Ultracold atoms</subject><subject>Vibratory 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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.</abstract><cop>Dordrecht</cop><pub>Springer Netherlands</pub><doi>10.1007/s12217-023-10068-7</doi><oa>free_for_read</oa></addata></record> |
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| ispartof | Microgravity science and technology, 2023-09, Vol.35 (5), p.48, Article 48 |
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| source | SpringerLink Journals - AutoHoldings |
| subjects | Aerospace Technology and Astronautics Atom interferometry Bose-Einstein condensates Classical and Continuum Physics Control equipment Control systems Engineering Frequency ranges Ground support equipment Ground support systems Interferometry Matter waves Modular design Sounding rockets Space Exploration and Astronautics Space Sciences (including Extraterrestrial Physics Static loads Thermal control systems Ultracold atoms Vibratory loads |
| title | A Dual-Species Atom Interferometer Payload for Operation on Sounding Rockets |
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