TY - RPRT A1 - Riegler, Clemens A1 - Werner, Lennart A1 - Kayal, Hakan T1 - MAPLE: Marsian Autorotation Probe Lander Experiment N2 - The first step towards aerial planetary exploration has been made. Ingenuity shows extremely promising results, and new missions are already underway. Rotorcraft are capable of flight. This capability could be utilized to support the last stages of Entry, Descent, and Landing. Thus, mass and complexity could be scaled down. Autorotation is one method of descent. It describes unpowered descent and landing, typically performed by helicopters in case of an engine failure. MAPLE is suggested to test these procedures and understand autorotation on other planets. In this series of experiments, the Ingenuity helicopter is utilized. Ingenuity would autorotate a ”mid-air-landing” before continuing with normal flight. Ultimately, the collected data shall help to understand autorotation on Mars and its utilization for interplanetary exploration. T3 - Raumfahrttechnik und Extraterrestrik - 2 KW - autorotation KW - descent KW - Mars KW - rotorcraft KW - landing KW - aerospace Y1 - 2022 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:bvb:20-opus-282390 ER - TY - THES A1 - Balagurin, Oleksii T1 - Designoptimierung von Sternsensoren für Pico- und Nanosatelliten T1 - Design optimization of star sensors for pico- and nanosatellites N2 - Die Raumfahrt ist eine der konservativsten Industriebranchen. Neue Entwicklungen von Komponenten und Systemen beruhen auf existierenden Standards und eigene Erfahrungen der Entwickler. Die Systeme sollen in einem vorgegebenen engen Zeitrahmen projektiert, in sehr kleiner Stückzahl gefertigt und schließlich aufwendig qualifiziert werden. Erfahrungsgemäß reicht die Zeit für Entwicklungsiterationen und weitgehende Perfektionierung des Systems oft nicht aus. Fertige Sensoren, Subsysteme und Systeme sind Unikate, die nur für eine bestimme Funktion und in manchen Fällen sogar nur für bestimmte Missionen konzipiert sind. Eine Neuentwicklung solcher Komponenten ist extrem teuer und risikobehaftet. Deswegen werden flugerprobte Systeme ohne Änderungen und Optimierung mehrere Jahre eingesetzt, ohne Technologiefortschritte zu berücksichtigen. Aufgrund des enormen finanziellen Aufwandes und der Trägheit ist die konventionelle Vorgehensweise in der Entwicklung nicht direkt auf Kleinsatelliten übertragbar. Eine dynamische Entwicklung im Low Cost Bereich benötigt eine universale und für unterschiedliche Anwendungsbereiche leicht modifizierbare Strategie. Diese Strategie soll nicht nur flexibel sein, sondern auch zu einer möglichst optimalen und effizienten Hardwarelösung führen. Diese Arbeit stellt ein Software-Tool für eine zeit- und kosteneffiziente Entwicklung von Sternsensoren für Kleinsatelliten vor. Um eine maximale Leistung des Komplettsystems zu erreichen, soll der Sensor die Anforderungen und Randbedingungen vorgegebener Anwendungen erfüllen und darüber hinaus für diese Anwendungen optimiert sein. Wegen der komplexen Zusammenhänge zwischen den Parametern optischer Sensorsysteme ist keine „straightforward" Lösung des Problems möglich. Nur durch den Einsatz computerbasierter Optimierungsverfahren kann schnell und effizient ein bestmögliches Systemkonzept für die gegebenen Randbedingungen ausgearbeitet werden. N2 - Aerospace is one of the most conservative industries. New developments of components and systems are based on existing standards and experience of developers. The systems should be projected in a given tight time frame, manufactured in very small quantities and finally qualified in a costly way. Experience shows that there is often insufficient time for development iterations and extensive perfection of the system. Finished sensors, subsystems and systems are unique, designed only for a specific function and in some cases even only for specific missions. New development of such components is extremely expensive and risky. For this reason, flight-proven systems are used for several years without modifications or optimization, and without taking technological advances into account. Due to the enormous financial effort and lethargy, the common approach to development is not directly applicable to small satellites. Dynamic development in the low-cost sector requires a universal strategy that can be easily modified for different applications. This strategy should not only be flexible, but also lead to the most optimal and efficient hardware solution. This work presents a software tool for a time and cost efficient development of star sensors for small satellites. In order to achieve maximal performance of the complete system, the sensor should fulfil the requirements and constraints of specified applications and, moreover, be optimized for these applications. Due to the complex interrelationships between the parameters of optical sensor systems, no straight forward solution of the problem is possible. Only by using computer based optimization methods, a best possible system concept for the given boundary conditions can be worked out quickly and efficiently. T3 - Raumfahrttechnik und Extraterrestrik - 1 KW - Sternsensor KW - CubeSat KW - Satellit KW - Optimisation KW - Star sensor KW - Star tracker Y1 - 2022 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:bvb:20-opus-258966 ER - TY - RPRT A1 - Riegler, Clemens A1 - Kayal, Hakan T1 - VELEX: Venus Lightning Experiment N2 - Lightning has fascinated humanity since the beginning of our existence. Different types of lightning like sprites and blue jets were discovered, and many more are theorized. However, it is very likely that these phenomena are not exclusive to our home planet. Venus’s dense and active atmosphere is a place where lightning is to be expected. Missions like Venera, Pioneer, and Galileo have carried instruments to measure electromagnetic activity. These measurements have indeed delivered results. However, these results are not clear. They could be explained by other effects like cosmic rays, plasma noise, or spacecraft noise. Furthermore, these lightning seem different from those we know from our home planet. In order to tackle these issues, a different approach to measurement is proposed. When multiple devices in different spacecraft or locations can measure the same atmospheric discharge, most other explanations become increasingly less likely. Thus, the suggested instrument and method of VELEX incorporates multiple spacecraft. With this approach, the question about the existence of lightning on Venus could be settled. T3 - Raumfahrttechnik und Extraterrestrik - 3 KW - Venus KW - Lightning KW - CubeSat KW - Balloon KW - Autorotation Y1 - 2022 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:bvb:20-opus-282481 ER - TY - RPRT A1 - Bösch, Carolin A1 - Stieler, Malena A1 - Lydon, Salomon A1 - Hesse, Martin A1 - Ali, Hassan A1 - Finzel, Matthias A1 - Faraz Ali, Syed A1 - Salian, Yash A1 - Alnoor, Hiba A1 - John, Jeena A1 - Lakkad, Harsh A1 - Bhosale, Devraj A1 - Jafarian, Timon A1 - Parvathi, Uma A1 - Ezzatpoor, Narges A1 - Datar, Tanuja T1 - Venus Research Station N2 - Because of the extreme conditions in the atmosphere, Venus has been less explored than for example Mars. Only a few probes have been able to survive on the surface for very short periods in the past and have sent data. The atmosphere is also far from being fully explored. It could even be that building blocks of life can be found in more moderate layers of the planet’s atmosphere. It can therefore be assumed that the planet Venus will increasingly become a focus of exploration. One way to collect significantly more data in situ is to build and operate an atmospheric research station over an extended period of time. This could carry out measurements at different positions and at different times and thus significantly expand our knowledge of the planet. In this work, the design of a Venus Research Station floating within the Venusian atmosphere is presented, which is complemented by the design of deployable atmospheric Scouts. The design of these components is done on a conceptual basis. T3 - Raumfahrttechnik und Extraterrestrik - 4 KW - Venus KW - Research Station Y1 - 2023 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:bvb:20-opus-328695 SN - 2747-9374 ER -