A Dual-Species Atom Interferometer Payload for Operation on Sounding Rockets
Abstract
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.
Details
- Organisation(s)
-
Institute of Quantum Optics
Quantum Sensing
Architectures and Systems Section
QuantumFrontiers
- External Organisation(s)
-
Center of Applied Space Technology and Microgravity (ZARM)
University of Bremen
DLR-Institute for Satellite Geodesy and Inertial Sensing
Ulm University
Ferdinand-Braun-Institut gGmbH, Leibniz-Institut für Höchstfrequenztechnik (FBH)
Universität Hamburg
Humboldt-Universität zu Berlin (HU Berlin)
Johannes Gutenberg University Mainz
DLR-Institute for Software Technology
- Type
- Article
- Journal
- Microgravity Science and Technology
- Volume
- 35
- ISSN
- 0938-0108
- Publication date
- 07.09.2023
- Publication status
- Published
- Peer reviewed
- Yes
- ASJC Scopus subject areas
- General Engineering, General Physics and Astronomy, Applied Mathematics, Modelling and Simulation
- Electronic version(s)
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https://doi.org/10.1007/s12217-023-10068-7 (Access:
Open
)