A5000254342- Wave and Wind Energy Systems
- Offshore Engineering and Technologies
- Advanced Frequency and Time Standards
- Cold Atom Physics and Bose-Einstein Condensates
- Technology Adoption and User Behaviour
- Economic and Environmental Valuation
- Atomic and Subatomic Physics Research
- Consumer Retail Behavior Studies
- Modeling and Simulation Systems
- Electric Motor Design and Analysis
- Distributed systems and fault tolerance
- Digital Marketing and Social Media
- Simulation Techniques and Applications
- Mechanical stress and fatigue analysis
- Advanced Control Systems Optimization
- Parallel Computing and Optimization Techniques
- Education, Sociology, Communication Studies
- Engineering Structural Analysis Methods
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
2023
RheinMain University of Applied Sciences
2015
Abstract We report on the design and construction of a sounding rocket payload capable performing atom interferometry with Bose-Einstein condensates $$^{41}$$ <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML"><mml:msup><mml:mrow/><mml:mn>41</mml:mn></mml:msup></mml:math> K $$^{87}$$ xmlns:mml="http://www.w3.org/1998/Math/MathML"><mml:msup><mml:mrow/><mml:mn>87</mml:mn></mml:msup></mml:math> Rb. The apparatus is designed to be launched in two consecutive missions VSB-30 qualified...
Today's space missions and projects dealing with cutting-edge technologies often lead to the development of highly complex systems. To ensure fulfillment mission goals, these require support adequate software tools that are capable various project management tasks. However, due their high cost inflexibility, existing not always well suited for operation in field research. We seek fill this gap by developing a new suite at Institute Satellite Geodesy Inertial Sensing German Aerospace Center...
We report on the design and construction of a sounding rocket payload capable performing atom interferometry with Bose-Einstein condensates $^{41}$K $^{87}$Rb. The apparatus is designed to be launched in two consecutive missions VSB-30 qualified withstand expected vibrational loads 1.8 g root-mean-square frequency range between 20 - 2000 Hz static during ascent re-entry 25 g. present modular scientific comprising physics package, laser system, an electronics system battery module. A...