Background minimization issues for next generation hard X-ray focusing telescopes

The hard X-ray band (10 - 100 keV) has been only observed so far by collimated and coded aperture mask instruments, with a sensitivity and an angular resolution lower than two orders of magnitude as respects the current X-ray focusing telescopes operating below 10 - 15 keV. The technological advance in X-ray mirrors and detection systems is now able to extend the X-ray focusing technique to the hard X-ray domain, filling the gap in terms of observational performances and providing a totally new deep view on some of the most energetic phenomena of the Universe. In order to reach a sensitivity of 1 muCrab in the 10 - 40 keV energy range, a great care in the background minimization is required, a common issue for all the hard X-ray focusing telescopes. In the present PhD thesis, a comprehensive analysis of the space radiation environment, the payload design and the resulting prompt X-ray background level is presented, with the aim of driving the feasibility study of the shielding system and assessing the scientific requirements of the future hard X-ray missions. A Geant4 based multi-mission background simulator, BoGEMMS, is developed to be applied to any high energy mission for which the shielding and instruments performances are required. It allows to interactively create a virtual model of the telescope and expose it to the space radiation environment, tracking the particles along their path and filtering the simulated background counts as a real observation in space. Its flexibility is exploited to evaluate the background spectra of the Simbol-X and NHXM mission, as well as the soft proton scattering by the X-ray optics and the selection of the best shielding configuration. Altough the Simbol-X and NHXM missions are the case studies of the background analysis, the obtained results can be generalized to any future hard X-ray telescope. For this reason, a simplified, ideal payload model is also used to select the major sources of background in LEO. All the results are original contributions to the assessment studies of the cited missions, as part of the background groups activities.

Design and implementation of a novel multi-constellation FPGA-based dual frequency GNSS receiver for space applications

The PhD activity described in the document is part of the Microsatellite and Microsystem Laboratory of the II Faculty of Engineering, University of Bologna. The main objective is the design and development of a GNSS receiver for the orbit determination of microsatellites in low earth orbit. The development starts from the electronic design and goes up to the implementation of the navigation algorithms, covering all the aspects that are involved in this type of applications. The use of GPS receivers for orbit determination is a consolidated application used in many space missions, but the development of the new GNSS system within few years, such as the European Galileo, the Chinese COMPASS and the Russian modernized GLONASS, proposes new challenges and offers new opportunities to increase the orbit determination performances. The evaluation of improvements coming from the new systems together with the implementation of a receiver that is compatible with at least one of the new systems, are the main activities of the PhD. The activities can be divided in three section: receiver requirements definition and prototype implementation, design and analysis of the GNSS signal tracking algorithms, and design and analysis of the navigation algorithms. The receiver prototype is based on a Virtex FPGA by Xilinx, and includes a PowerPC processor. The architecture follows the software defined radio paradigm, so most of signal processing is performed in software while only what is strictly necessary is done in hardware. The tracking algorithms are implemented as a combination of Phase Locked Loop and Frequency Locked Loop for the carrier, and Delay Locked Loop with variable bandwidth for the code. The navigation algorithm is based on the extended Kalman filter and includes an accurate LEO orbit model.

Daniello Bartoli, Il Giappone, Edizione critica

La tesi di ricerca ha portato alla realizzazione di un’edizione critica del Giappone di Daniello Bartoli (1660): per la prima volta la «seconda parte» dell’Asia trova, in questo lavoro, una trascrizione integrale condotta con moderni criteri filologi. Quanto all’esegesi la ricerca ha visto la compilazione di tre «Schedari»: un «Indice dei nomi», che vede l’identificazione dei personaggi storici citati esplicitamente nell’opera, ne traccia un rapido profilo biografico e ne fornisce precisa e aggiornata bibliografia. Per quanto riguarda i missionari evocati dall’autore nel testo, questa sezione indica se (e dove) si tratta di personaggio o di fonte (registrando, nel caso, il luogo o i luoghi in cui Bartoli ricorre a tale testimonianza); un «Indice dei luoghi», che dà l’indicazione moderna del luogo citato e ne fornisce il riscontro con i repertori più aggiornati; un «Lessico» riservato ai termini giapponesi presenti nel testo che vengono spiegati e, là dove possibile, studiati nella loro storia, nella loro presenza nella coeva letteratura di viaggio e corredati di utili riferimenti bibliografici. Le pagine introduttive inquadrano l’opera di Bartoli sia nell’orizzonte biografico dell’autore sia nel milieu gesuitico barocco, fornendo puntuali coordinate storiche grazie alle quali recuperare il più ampio contesto delle missioni gesuitiche nell’Estremo Oriente tra Cinque e Seicento. Particolare attenzione è stata riservata al modo di intendere il compito dello storico da parte di Bartoli: una storiografia la sua che s’intreccia in modi affatto peculiari alle diverse forme stilistiche e dinamiche retoriche richieste dalle altre due grandi attività a cui egli dedicò impegno e passione: l’insegnamento e la predicazione.

Diversity of lithologic components at Meridiani Planum, Mars: Insights from Mössbauer spectroscopic investigations

The two Mars Exploration Rovers (MER), Spirit and Opportunity, landed on the Martian surface in January 2004 and have since collected a wealth of information about their landing sites. As part of their payload, the miniaturised Mössbauer spectrometer MIMOS II contributes to the success of the mission by identifying Iron-bearing minerals and by determining Iron oxidation states in them. The basis of this work is the data set obtained at Opportunity’s landing site at Meridiani Planum. A portion of this data set is evaluated with different methods, with the aim to thoroughly characterize lithologic components at Meridiani Planum and possible relations between them.rnMIMOS II is able to measure Mössbauer spectra at different energies simultaneously, bearing information from different sampling depths of the investigated target. The ability of depth-selective Mössbauer spectroscopy to characterize weathered surface layers is illustrated through its application to two suitable rock targets that were investigated on Mars. In both cases, an enhanced concentration of Iron oxides at the rock surface was detected, pointing to a low degree of aqueous alteration. rnThe mineral hematite (α-Fe2O3) is present in the matrix of outcrop rocks and in spherules weathering from the outcrop. Simultaneous fitting of Mössbauer spectra was applied to data sets obtained on both target types to characterize the hematite component in detail. This approach reveals that two hematite populations are present, both in the outcrop matrix as well as in spherules. The hematite component with a comparably high degree of crystallinity and/or chemical purity is present in the outcrop matrix. The investigation of hematite at Meridiani Planum has shown that simultaneous fitting is a suitable and useful method to evaluate a large, correlated set of Mössbauer spectra.rnOpportunity encountered loose, cm-sized rocks along its traverse. Based on their composition and texture, these “cobbles” can be divided into three different groups. Outcrop fragments are impact-derived ejecta from local outcrop rocks. Cobbles of meteoritic origin contain the minerals kamacite (Fe,Ni) and troilite (FeS) and exhibit high Ni contents. Melt-bearing impact breccias bear similarities to local outcrop rocks and basaltic soil, with a phase composition and texture consistent with a formation scenario involving partial melting and inclusion of small, bright outcrop clasts. rnIron meteorites on the Martian surface experience weathering through the presence of even trace amounts of water due to their metallic nature. Opportunity encountered and investigated four Iron meteorites, which exhibit evidence for physical and chemical weathering. Discontinuous coatings contain Iron oxides, pointing to the influence of limited amounts of water. rnA terrestrial analogue site for Meridiani Planum is the Rio Tinto basin in south-west Spain. With its deposits of sulfate- and iron-oxide-bearing minerals, the region provides an adequate test bed for instrumentation for future Mars missions. In-situ investigations at Rio Tinto were carried out with a special focus on the combined use of Mössbauer spectroscopy with MIMOS II and Raman spectroscopy with a field-portable instrument. The results demonstrate that the two instruments provide complementary information about investigated samples.

Development of an X-ray spectrometric system and feasibility tests of Silicon Drift Detector for medical and space applications

The thesis work concerns X-ray spectrometry for both medical and space applications and is divided into two sections. The first section addresses an X-ray spectrometric system designed to study radiological beams and is devoted to the optimization of diagnostic procedures in medicine. A parametric semi-empirical model capable of efficiently reconstructing diagnostic X-ray spectra in 'middle power' computers was developed and tested. In addition, different silicon diode detectors were tested as real-time detectors in order to provide a real-time evaluation of the spectrum during diagnostic procedures. This project contributes to the field by presenting an improved simulation of a realistic X-ray beam emerging from a common X-ray tube with a complete and detailed spectrum that lends itself to further studies of added filtration, thus providing an optimized beam for different diagnostic applications in medicine. The second section describes the preliminary tests that have been carried out on the first version of an Application Specific Integrated Circuit (ASIC), integrated with large area position-sensitive Silicon Drift Detector (SDD) to be used on board future space missions. This technology has been developed for the ESA project: LOFT (Large Observatory for X-ray Timing), a new medium-class space mission that the European Space Agency has been assessing since February of 2011. The LOFT project was proposed as part of the Cosmic Vision Program (2015-2025).

Aufbau eines flugzeuggetragenen Massenspektrometers zur Messung von HNO 3 und HONO und Quantifizierung der HNO 3-Aufnahme in Eispartikel in Kondensstreifen und Zirren

Im Zuge dieser Arbeit ist ein Massenspektrometer zur flugzeuggetragenen Messung von HNO3 und HONO auf dem neuen deutschen Forschungsflugzeug HALO aufgebaut worden (AIMS - Atmospheric chemical Ionization Mass Spectrometer). Die Ionisation der HNO3- und HONO-Moleküle erfolgt chemisch durch Reaktion mit SF5- -Ionen. Basierend auf den Ergebnissen von Laborversuchen wurden die Betriebsparameter optimiert, die Einzelkomponenten im HALO-Rack zusammengestellt und eine Einlassleitung entworfen, die Wandeffekte minimiert und Untergrundmessungen und HNO3-Kalibrationen im Flug ermöglicht. Die Empfindlichkeit der Messung von HNO3 und HONO wurde ebenso im Labor untersucht wie Interferenzen mit Wasserdampf und Ozon. Die HONO-Vergleichskampagne FIONA am Europäischen Photoreaktor (EUPHORE) in Valencia war die erste Messkampagne mit AIMS. Bei den offenen Vergleichsmessungen stimmten die von AIMS gemessenen HONO-Mischungsverhältnisse innerhalb +-20% mit dem Median von 9 weiteren HONO-Messungen überein. Die ersten flugzeuggetragenen Messungen mit AIMS werden im Verlauf der HALO-Missionen ML-CIRRUS und TACTS stattfinden. Neben dem Aufbau und der Charakterisierung von AIMS war die Analyse der Aufnahme von HNO3 in Eispartikel von Kondensstreifen und Zirren Gegenstand dieser Arbeit. Die Aufnahme von HNO3 in Kondensstreifeneispartikel wurde erstmals systematisch anhand einer Flugzeugmesskampagne (CIRRUS-III) untersucht. Während CIRRUS-III im November 2006 wurden Zirren und zufällig knapp 40 persistente Kondensstreifen über Deutschland und Nordeuropa beprobt. Die Messungen fanden in Höhen zwischen 10 und 11.5 km und bei Temperaturen zwischen 210 und 230 K statt. Die HNO3-Konzentration wurde mit Hilfe von NOy-Messungen bestimmt. Im Mittel war in Kondensstreifen ein größerer Anteil des Gesamt-HNO3 in den Eispartikeln gebunden (6 %) als in Zirren (3 %). Das Gasphasenäquivalent des eisgebundenen HNO3 betrug in Zirren durchschnittlich 6 pmol/mol, in Kondensstreifen 14 pmol/mol und in jungen Kondensstreifen (Alter<1 h) 21 pmol/mol. Das Mischungsverhältnis von HNO3 zu H2O in Eispartikeln war in Kondensstreifen leicht höher als in Zirren unter ähnlichen meteorologischen Bedingungen. Ursächlich für die höheren Werte in persistenten Kondensstreifen sind wahrscheinlich die hohen HNO3-Konzentrationen in den Abgasfahnen der Flugzeuge bei der Kondensstreifenbildung. Die beobachtete Abnahme des HNO3/H2O-Molverhältnisses mit zunehmendem Effektivdurchmesser der Eispartikel deutet an, dass die HNO3-Konzentrationen in Eispartikeln von jungen Kondensstreifen durch die Aufnahme von Abgas-HNO3 in die gefrierenden Aerosolpartikel bestimmt wird. Die Konzentrationen in älteren Kondensstreifen werden zunehmend durch das Vergraben von Umgebungs-HNO3 in wachsenden Eispartikeln kontrolliert. Diese Studie leistet einen Beitrag zu einem besseren Prozessverständnis der HNO3-Aufnahme in atmosphärische Eispartikel. Sie motiviert die Nutzung persistenter Kondensstreifen als atmosphärisches Labor zur Untersuchung der Spurengasaufnahme in wachsende Eispartikel.

An Integrated Transmission-Media Noise Calibration Software For Deep-Space Radio Science Experiments

The thesis describes the implementation of a calibration, format-translation and data conditioning software for radiometric tracking data of deep-space spacecraft. All of the available propagation-media noise rejection techniques available as features in the code are covered in their mathematical formulations, performance and software implementations. Some techniques are retrieved from literature and current state of the art, while other algorithms have been conceived ex novo. All of the three typical deep-space refractive environments (solar plasma, ionosphere, troposphere) are dealt with by employing specific subroutines. Specific attention has been reserved to the GNSS-based tropospheric path delay calibration subroutine, since it is the most bulky module of the software suite, in terms of both the sheer number of lines of code, and development time. The software is currently in its final stage of development and once completed will serve as a pre-processing stage for orbit determination codes. Calibration of transmission-media noise sources in radiometric observables proved to be an essential operation to be performed of radiometric data in order to meet the more and more demanding error budget requirements of modern deep-space missions. A completely autonomous and all-around propagation-media calibration software is a novelty in orbit determination, although standalone codes are currently employed by ESA and NASA. The described S/W is planned to be compatible with the current standards for tropospheric noise calibration used by both these agencies like the AMC, TSAC and ESA IFMS weather data, and it natively works with the Tracking Data Message file format (TDM) adopted by CCSDS as standard aimed to promote and simplify inter-agency collaboration.

Strahlungsinduzierte Mukositis als Risiko der Raumfahrt : Modelluntersuchungen an Röntgen- und Schwerionen-bestrahlten organotypischen Mundschleimhaut-Modellen

Während ausgedehnter Weltraumflüge zum Mond und Mars wäre die Besatzung eines Raumschiffs dicht ionisierender Schwerionenstrahlung, der sogenannten kosmischen Strahlung, ausgesetzt. Da bei vielen Krebspatienten die orale Mukositis als eine gravierende Nebenwirkung bei der herkömmlichen Strahlentherapie auftritt, könnte diese Erkrankung ein medizinisches Problem während ausgedehnter Weltraumflüge darstellen. Allerdings liegen bislang keine Untersuchungen über eine mögliche Mukositis-induzierte Wirkung von Schwerionenstrahlung vor. Um das Risiko strahlungsinduzierter oraler Mukositis durch kosmische Strahlung abzuschätzen, wurden dreidimensionale organotypische Mundschleimhaut-Modelle 12C Schwerionen- bzw. Röntgenstrahlung ausgesetzt und nach definierten Inkubationszeiten kryokonserviert. Aus dem Material wurden Kryoschnitte gefertigt, mit denen anschließend histologische und immunhistologische Fluoreszenzfärbungen zum Nachweis von zum Beispiel Kompaktheitsverlust, Doppelstrangbrüchen der DNA und NF-κB-Aktivierung durchgeführt wurden. Die Ausschüttung von Tumornekrosefaktor α, Interleukin 1β, Interleukin 6 und Interleukin 8 wurde in Probenüberständen mittels ELISA analysiert. Das Hauptaugenmerk dieser Studie lag dabei auf den frühen durch Strahlung verursachten Effekten. rnIm Rahmen dieser Dissertation wurde ein dreidimensionales Mundschleimhaut-Modell etabliert, das verglichen mit humaner Mundschleimhaut viele organotypische Differenzierungsmarker und in vivo-ähnliche Reaktionen auf bestimmte Reize zeigte. Nach einer Bestrahlung mit schweren Kohlenstoffionen bzw. mit Röntgenstrahlung wurden strahlungsinduzierte Effekte auf mehreren Ebenen detektiert. Bereits 1 h nach Bestrahlung konnten dosisabhängig vermehrte Doppelstrangbrüche in der DNA detektiert werden, wobei bei gleicher Dosis Schwerionenstrahlung im Durchschnitt doppelt so viele DSB verursachte wie Röntgenstrahlung. Das Mundschleimhaut-Modell reagierte auf beide Strahlungsarten mit einer Aktivierung des Transkriptionsfaktors NF-κB p50, wobei Röntgenstrahlung diese Aktivierung früher induzierte als Schwerionen. Eine strahlungsinduzierte Aktivierung von NF-κB p65 wurde in den organotypischen Kulturen zu den untersuchten Zeitpunkten nicht beobachtet. Im Vergleich zu nicht bestrahlten Kulturen waren die Konzentrationen von Interleukin 6 und Interleukin 8 unabhängig von der Strahlungsqualität nach Bestrahlung signifikant erhöht. Interleukin-1β dagegen wurde nur nach Röntgenbestrahlung signifikant vermehrt ausgeschüttet. In Schwerionen-bestrahlten Proben wurden zwar tendenziell höhere Konzentrationen beobachtet, statistische Signifikanzen ergaben sich aber nicht. Die Analysen zur TNF-α- und IFN-γ-Ausschüttung in bestrahlten organotypischen Kulturen ergaben innerhalb des gewählten Beobachtungszeitraums von 48 h keine strahlungsinduzierten Effekte. Bei den Untersuchungen der Proliferation in den Zellen der bestrahlten organotypischen Kulturen wurde bereits 24 h nach Röntgenstrahlung und 3 Tage nach Schwerionenstrahlung eine deutliche verminderte Proliferation beobachtet. Des Weiteren zeigte das Mundschleimhaut-Modell unabhängig von Strahlungsqualitäten einen eindeutigen Verlust in der Zellintegrität und daraus resultierenden Kompaktheitsverlust des Gewebes, was in der in vivo-Situation wahrscheinlich einer Gewebedegeneration entspricht. rnNach Bestrahlung mit sowohl Röntgenstrahlung als auch schweren Ionen wurden im gewählten Mukosa-Modell innerhalb von 48 h nach Behandlung strahlungsinduzierte proinflammatorische Marker eindeutig und reproduzierbar detektiert. Dies deutet darauf hin, dass während langer extraterrestrischer Expeditionen das Risiko der oralen Mukositis einkalkuliert und mit den daraus folgenden Konsequenzen gerechnet werden muss.rn

Analysis of aircraft load spectrum by means of flight simulator

Damage tolerance analysis is a quite new methodology based on prescribed inspections. The load spectra used to derive results of these analysis strongly influence the final defined inspections programs that for this reason must be as much as possible representative of load acting on the considered structural component and at the same time, obtained reducing both cost and time. The principal purpose of our work is in improving the actual condition developing a complete numerical Damage Tolerance analysis, able to prescribe inspection programs on typical aircraft critical components, respecting DT regulations, starting from much more specific load spectrum then those actually used today. In particular, these more specific load spectrum to design against fatigue have been obtained through an appositively derived flight simulator developed in a Matlab/Simulink environment. This dynamic model has been designed so that it can be used to simulate typical missions performing manually (joystick inputs) or completely automatic (reference trajectory need to be provided) flights. Once these flights have been simulated, model’s outputs are used to generate load spectrum that are then processed to get information (peaks, valleys) to perform statistical and/or comparison consideration with other load spectrum. However, also much more useful information (loads amplitude) have been extracted from these generated load spectrum to perform the previously mentioned predictions (Rainflow counting method is applied for this purpose). The entire developed methodology works in a complete automatic way, so that, once some specified input parameters have been introduced and different typical flights have been simulated both, manually or automatically, it is able to relate the effects of these simulated flights with the reduction of residual strength of the considered component.

Night Vision Imaging System (NVIS) certification requirements analysis of an Airbus Helicopters H135

The safe operation of nighttime flight missions would be enhanced using Night Vision Imaging Systems (NVIS) equipment. This has been clear to the military since 1970s and to the civil helicopters since 1990s. In these last months, even Italian Emergency Medical Service (EMS) operators require Night Vision Goggles (NVG) devices that therefore amplify the ambient light. In order to fly with this technology, helicopters have to be NVIS-approved. The author have supported a company, to quantify the potentiality of undertaking the certification activity, through a feasibility study. Even before, NVG description and working principles have been done, then specifications analysis about the processes to make a helicopter NVIS-approved has been addressed. The noteworthy difference between military specifications and the civilian ones highlights non-irrevelant lacks in the latter. The activity of NVIS certification could be a good investment because the following targets have been achieved: Reductions of the certification cost, of the operating time and of the number of non-compliance.

Source of funding in experimental studies of mobile phone use on health: Update of systematic review

A previous review showed that among 59 studies published in 1995–2005, industry-funded studies were least likely to report effects of controlled exposure to mobile phone radiation on health-related outcomes. We updated literature searches in 2005–2009 and extracted data on funding, conflicts of interest and results. Of 75 additional studies 12% were industry-funded, 44% had public and 19% mixed funding; funding was unclear in 25%. Previous findings were confirmed: industry-sponsored studies were least likely to report results suggesting effects. Interestingly, the proportion of studies indicating effects declined in 1995–2009, regardless of funding source. Source of funding and conflicts of interest are important in this field of research.

Civic Discipline: Geography in America, 1860-1890

Civic Discipline argues that the story of the origins of American geography is a distinctly "New York story." Wealthy businessmen began America's first geographical society - the American Geographical Society - in 1851, inspired by what geographical knowledge of the globe could offer an expanding American commercial Empire at home and abroad. AGS meetings were spectacularly popular among the public and press. At them, geography was cast as a science in the service of the public and civic good. Meanwhile though, AGS men's spatial and financial "missions" became closely linked. They helped improve derelict spaces in New York City and weighed in on controversial scientific questions of the day in the Arctic, yet the geographical knowledge they advanced - such as in the American West and in Central Africa - also created enormous personal wealth. Civic Discipline shows that it was not just that historical events shaped geography, but rather, that geography shaped historical events.

Io volcano observer (IVO) integrated approach to optimizing system design for radiation challenges

One of the major challenges for a mission to the Jovian system is the radiation tolerance of the spacecraft (S/C) and the payload. Moreover, being able to achieve science observations with high signal to noise ratios (SNR), while passing through the high flux radiation zones, requires additional ingenuity on the part of the instrument provider. Consequently, the radiation mitigation is closely intertwined with the payload, spacecraft and trajectory design, and requires a systems-level approach. This paper presents a design for the Io Volcano Observer (IVO), a Discovery mission concept that makes multiple close encounters with Io while orbiting Jupiter. The mission aims to answer key outstanding questions about Io, especially the nature of its intense active volcanism and the internal processes that drive it. The payload includes narrow-angle and wide-angle cameras (NAC and WAC), dual fluxgate magnetometers (FGM), a thermal mapper (ThM), dual ion and neutral mass spectrometers (INMS), and dual plasma ion analyzers (PIA). The radiation mitigation is implemented by drawing upon experiences from designs and studies for missions such as the Radiation Belt Storm Probes (RBSP) and Jupiter Europa Orbiter (JEO). At the core of the radiation mitigation is IVO's inclined and highly elliptical orbit, which leads to rapid passes through the most intense radiation near Io, minimizing the total ionizing dose (177 krads behind 100 mils of Aluminum with radiation design margin (RDM) of 2 after 7 encounters). The payload and the spacecraft are designed specifically to accommodate the fast flyby velocities (e.g. the spacecraft is radioisotope powered, remaining small and agile without any flexible appendages). The science instruments, which collect the majority of the high-priority data when close to Io and thus near the peak flux, also have to mitigate transient noise in their detectors. The cameras use a combination of shielding and CMOS detectors with extremely fast readout to mi- imize noise. INMS microchannel plate detectors and PIA channel electron multipliers require additional shielding. The FGM is not sensitive to noise induced by energetic particles and the ThM microbolometer detector is nearly insensitive. Detailed SNR calculations are presented. To facilitate targeting agility, all of the spacecraft components are shielded separately since this approach is more mass efficient than using a radiation vault. IVO uses proven radiation-hardened parts (rated at 100 krad behind equivalent shielding of 280 mils of Aluminum with RDM of 2) and is expected to have ample mass margin to increase shielding if needed.