Author:
Sperling Richard,Raupert Marvin,Lotz Christoph,Overmeyer Ludger
Abstract
AbstractIn order to develop hardware that can be used in space, tests under those space conditions are often important to ensure the functionality in advance. Facilities that are used to recreate gravity conditions of space include space stations, satellites, parabolic flights and earthbound facilities. Drop towers are earthbound facilities, that can replicate the gravitational conditions of free falling in space by dropping objects. Those objects would not experience any measurable force due to gravity according to Einstein’s famous thought experiment. The Einstein-Elevator is one of the first active driven drop towers with an experiment carrier falling inside a gondola. A major indicator for the quality of the facility is the residual acceleration of the payload. With the Einstein-Elevators current setup vibrations of the experiment carrier cause measurable residual accelerations of higher than $$10^{-3}$$
10
-
3
g. To achieve the targeted 0-g-quality with a residual acceleration of less than 1 $$\mu $$
μ
g (microgravity) in the Einstein-Elevator, a new experiment carrier is required that minimizes the residual acceleration for a payload. This paper describes a design of the experiment carrier for the Einstein-Elevator that is able to reach microgravity and analyzes its functionality using FEM-simulations.
Funder
Deutsches Zentrum für Luft- und Raumfahrt, Institut für Satellitengeodäsie und Inertialsensorik
Gottfried Wilhelm Leibniz Universität Hannover
Publisher
Springer Science and Business Media LLC
Reference22 articles.
1. Labeaga-Martínez, N., Sanjurjo-Rivo, M., Díaz-Álvarez, J. & Martínez-Frías, J. Additive manufacturing for a moon village. Procedia Manuf. 13, 794–801. https://doi.org/10.1016/j.promfg.2017.09.186 (2017).
2. Do, S., Owens, A., Ho, K., Schreiner, S. & de Weck, O. An independent assessment of the technical feasibility of the mars one mission plan: Updated analysis. Acta Astronaut. 120, 192–228. https://doi.org/10.1016/j.actaastro.2015.11.025 (2016).
3. Fortov, V. E. et al. Dynamics of macroparticles in a dusty plasma under microgravity conditions (first experiments on board the ISS). J. Exp. Theor. Phys. 96(4), 704–718. https://doi.org/10.1134/1.1574544 (2003).
4. Zhao, H., Qiu, J. & Wang, Y. System Design and Flight Results of China SJ-10 Recoverable Microgravity Experimental Satellite 13–46 (Springer Singapore, 2019).
5. Stamminger, A. et al. Maius-1 - vehicle, subsystems design and mission operations, Vol. SP-730 183–190 (ESA Communications, 2015). https://elib.dlr.de/99281/.