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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.
20 years after the successful ground deployment test of a (20 m) 2 solar sail at DLR Cologne, and in the light of the upcoming U.S. NEAscout mission, we provide an overview of the progress made since in our mission and hardware design studies as well as the hardware built in the course of our solar sail technology development. We outline the most likely and most efficient routes to develop solar sails for useful missions in science and applications, based on our developed `now-term' and near-term hardware as well as the many practical and managerial lessons learned from the DLR-ESTEC Gossamer Roadmap. Mission types directly applicable to planetary defense include single and Multiple NEA Rendezvous ((M)NR) for precursor, monitoring and follow-up scenarios as well as sail-propelled head-on retrograde kinetic impactors (RKI) for mitigation. Other mission types such as the Displaced L1 (DL1) space weather advance warning and monitoring or Solar Polar Orbiter (SPO) types demonstrate the capability of near-term solar sails to achieve asteroid rendezvous in any kind of orbit, from Earth-coorbital to extremely inclined and even retrograde orbits. Some of these mission types such as SPO, (M)NR and RKI include separable payloads. For one-way access to the asteroid surface, nanolanders like MASCOT are an ideal match for solar sails in micro-spacecraft format, i.e. in launch configurations compatible with ESPA and ASAP secondary payload platforms. Larger landers similar to the JAXA-DLR study of a Jupiter Trojan asteroid lander for the OKEANOS mission can shuttle from the sail to the asteroids visited and enable multiple NEA sample-return missions. The high impact velocities and re-try capability achieved by the RKI mission type on a final orbit identical to the target asteroid's but retrograde to its motion enables small spacecraft size impactors to carry sufficient kinetic energy for deflection.
Design and Development of a Novel Self-Igniting Microwave Plasma Jet for Industrial Applications
(2019)
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
Praxistransfer in der tertiären Bildungsforschung: Modelle, Gelingensbedingungen und Nachhaltigkeit
(2019)
A review of guidelines and best practices for subsonic aerodynamic simulations using RANS CFD
(2019)
In this paper, an approach to propulsion system modelling for hybrid-electric general aviation aircraft is presented. Because the focus is on general aviation aircraft, only combinations of electric motors and reciprocating combustion engines are explored. Gas turbine hybrids will not be considered. The level of the component's models is appropriate for the conceptual design stage. They are simple and adaptable, so that a wide range of designs with morphologically different propulsive system architectures can be quickly compared. Modelling strategies for both mass and efficiency of each part of the propulsion system (engine, motor, battery and propeller) will be presented.