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In this chapter, the key technologies and the instrumentation required for the subsurface exploration of ocean worlds are discussed. The focus is laid on Jupiter’s moon Europa and Saturn’s moon Enceladus because they have the highest potential for such missions in the near future. The exploration of their oceans requires landing on the surface, penetrating the thick ice shell with an ice-penetrating probe, and probably diving with an underwater vehicle through dozens of kilometers of water to the ocean floor, to have the chance to find life, if it exists. Technologically, such missions are extremely challenging. The required key technologies include power generation, communications, pressure resistance, radiation hardness, corrosion protection, navigation, miniaturization, autonomy, and sterilization and cleaning. Simpler mission concepts involve impactors and penetrators or – in the case of Enceladus – plume-fly-through missions.
Berücksichtigung von No Fault Found im Diagnose- und Instandhaltungssystem von Schienenfahrzeugen
(2020)
Intermittierende und nicht reproduzierbare Fehler, auch als No Fault Found bezeichnet, treten in praktisch allen Bereichen auf und sorgen für hohe Kosten. Diese sind häufig auf unpräzise Fehlerbeschreibungen zurückzuführen. Im vorliegenden Beitrag werden Anpassungen der Vorgehensweise bei der Entwicklung und Anpassungen des Diagnosesystems vorgeschlagen.
For short take-off and landing (STOL) aircraft, a parallel hybrid-electric propulsion system potentially offers superior performance compared to a conventional propulsion system, because the short-take-off power requirement is much higher than the cruise power requirement. This power-matching problem can be solved with a balanced hybrid propulsion system. However, there is a trade-off between wing loading, power loading, the level of hybridization, as well as range and take-off distance. An optimization method can vary design variables in such a way that a minimum of a particular objective is attained. In this paper, a comparison between the optimization results for minimum mass, minimum consumed primary energy, and minimum cost is conducted. A new initial sizing algorithm for general aviation aircraft with hybrid-electric propulsion systems is applied. This initial sizing methodology covers point performance, mission performance analysis, the weight estimation process, and cost estimation. The methodology is applied to the design of a STOL general aviation aircraft, intended for on-demand air mobility operations. The aircraft is sized to carry eight passengers over a distance of 500 km, while able to take off and land from short airstrips. Results indicate that parallel hybrid-electric propulsion systems must be considered for future STOL aircraft.
Dimensionen 1-2019: Magazin der FH Aachen University of Applied Sciences - Wir sind FH Aachen!
(2019)
Inhaltsverzeichnis:
6 Wir sind FH!
8 Steigen Sie ein : Wir nehmen Sie mit auf eine Reise der Roboter und Maschinen
18 Grenzenlose Förderung : Das Stipendienprogramm geht in das zehnte Jahr
20 Marias neue Kleider : Wissenschaftler unterstützen die Domschatzkammer
24 Die Sprengstoffschnüffler : Fliegerbomben im Erdreich: Neues Verfahren auf Basis der Neutronenaktivierungsanalyse
26 Geschafft! : Erster marokkanischer Elektrotechnikstudent macht seinen Doppelabschluss an der FH Aachen
28 Maßgeschneidert : Dr. Denise Milinnus vom INB entwickelt digitale Biosensoren für die personalisierte Medizin
32 Auf Höhenflügen : Tobias Barth macht außergewöhnliche Luftaufnahmen
36 Über alle Berge : Talentscouting eröffnet neue Wege
38 Der etwas andere Reiseführer : FH-Studentinnen entwerfen Stadtplan für junge Menschen
42 Warum kommt mein Zug zu spät? : FH-Experten im Interview über Probleme und Lösungen der Schiene
48 Der Alina-Weg : Alina Richter promoviert bei der Volkswaren-Konzernforschung
51 Selbst ist die Frau : Die 31-jährige Meral Dural studiert erfolgreich Elektrotechnik am FH-Campus Jülich
52 An der Schnittstelle : INFORM-Professur für angewandte Mathematik und Informatik
53 Kopfnuss
54 Einmal scannen bitte : Forschungsprojekt am MASKOR-Institut wird vom Bund gefördert
56 Inspiriert vom Tier- und Pflanzenmeer : FH-Absolventin Lara Bispinck gewinnt "Future Impact Maker"
60 Schmusekurs mit dem Tiger : FH Aachen führt Kooperationsverbund mit taiwanesischen Hochschulen an
62 Impressum
A light-addressable potentiometric sensor (LAPS) is a field-effect-based (bio-) chemical sensor, in which a desired sensing area on the sensor surface can be defined by illumination. Light addressability can be used to visualize the concentration and spatial distribution of the target molecules, e.g., H+ ions. This unique feature has great potential for the label-free imaging of the metabolic activity of living organisms. The cultivation of those organisms needs specially tailored surface properties of the sensor. O2 plasma treatment is an attractive and promising tool for rapid surface engineering. However, the potential impacts of the technique are carefully investigated for the sensors that suffer from plasma-induced damage. Herein, a LAPS with a Ta2O5 pH-sensitive surface is successfully patterned by plasma treatment, and its effects are investigated by contact angle and scanning LAPS measurements. The plasma duration of 30 s (30 W) is found to be the threshold value, where excessive wettability begins. Furthermore, this treatment approach causes moderate plasma-induced damage, which can be reduced by thermal annealing (10 min at 300 °C). These findings provide a useful guideline to support future studies, where the LAPS surface is desired to be more hydrophilic by O2 plasma treatment.
Impressum | Inhalt 03
Thomas Tünnemann | Unterwegs...am Wege 04
Projekte 06
Annelie Wirtz | Arrivato 08
Sebastian Rupp | Tracce Passate 18
Henri Boh | Terrazze sopra il lago 28
Hermann Stuzmann | L´Ammissione è Gratuita 32
Vivienne Scheidz | IL Potere dei Simboli 34
Felix Keller | Strada Infinita 38
Moran Dorner | Catturato nel Posto 42
Kevin Osterkamp | Vortice 46
Kristina Foidle | La Vespa e il Fico 52
Simon Rix | Sognare Sulla Strada 58
Jennifer Sikora | Strada Pietrosa 66
Sabrina Frömbgen | Bolla di Pensiero 72
Miriam Azzab | Il Momento 78
Georg Mörke | Sentiero stretto 84
Saskia Frömbgen | Nuova Prospetiva 90
Frank Drehsen | A grado a grado 96
Caronlin Grün | Le prospettive 100
Thomas Tünnemann | Flusso nella Foresta 104
Atmosphärisches
Auf die Küche | Kulinarisches 114
Carpe Diem | Fotografisches 116
Recent analysis of scientific data from Cassini and earth-based observations gave evidence for a global ocean under a surrounding solid ice shell on Saturn's moon Enceladus. Images of Enceladus' South Pole showed several fissures in the ice shell with plumes constantly exhausting frozen water particles, building up the E-Ring, one of the outer rings of Saturn. In this southern region of Enceladus, the ice shell is considered to be as thin as 2 km, about an order of magnitude thinner than on the rest of the moon. Under the ice shell, there is a global ocean consisting of liquid water. Scientists are discussing different approaches the possibilities of taking samples of water, i.e. by melting through the ice using a melting probe. FH Aachen UAS developed a prototype of maneuverable melting probe which can navigate through the ice that has already been tested successfully in a terrestrial environment. This means no atmosphere and or ambient pressure, low ice temperatures of around 100 to 150K (near the South Pole) and a very low gravity of 0,114 m/s^2 or 1100 μg. Two of these influencing measures are about to be investigated at FH Aachen UAS in 2017, low ice temperature and low ambient pressure below the triple point of water. Low gravity cannot be easily simulated inside a large experiment chamber, though. Numerical simulations of the melting process at RWTH Aachen however are showing a gravity dependence of melting behavior. Considering this aspect, VIPER provides a link between large-scale experimental simulations at FH Aachen UAS and numerical simulations at RWTH Aachen. To analyze the melting process, about 90 seconds of experiment time in reduced gravity and low ambient pressure is provided by the REXUS rocket. In this time frame, the melting speed and contact force between ice and probes are measured, as well as heating power and a two-dimensional array of ice temperatures. Additionally, visual and infrared cameras are used to observe the melting process.