Searching for capture and escape trajectories around Jupiter using its Galilean satellites

Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)

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

Electrodynamic Tether at Jupiter I: Capture operation and constraints

Tethered spacecraft missions to the Jovian system suit the use of electrodynamic tethers because: 1) magnetic stresses are 100 times greater than at the Earth; 2) the stationary orbit is one-third the relative distance for Earth; and 3) moon Io is a nearby giant plasma source. The (bare) tether is a reinforced aluminum foil with tens of kilometer length L and a fraction of millimeter thickness h, which collects electrons as an efficient Langmuir probe and can tap Jupiter’s rotational energy for both propulsion and power. In this paper, the critical capture operation is explicitly formulated in terms of orbit geometry and established magnetic and thermal plasma models. The design parameters L and h and capture perijove radius rp face opposite criteria independent of tape width. Efficient capture requires a low rp and a high L 3/2/h ratio. However, combined bounds on tether bowing and tether tensile stress, arising from a spin made necessary by the low Jovian gravity gradient, require a high rp and a low L 5/2/h ratio. Bounds on tether temperature again require a high rp and a low L 3/8/(tether emissivity)1/4 ratio. Optimal design values are discussed.

Electrodynamic tethers for spacecraft propulsion

Relatively short electrodynamic tethers can use solar power to "push" against a planetary magnetic field to achieve propul sion without expenditure of propellant. The groundwork has been laid for this type of propulsion. Recent important milestones include retrieval of a tether in space (TSS-1, 1992), successful deployment of a 20-km-long tether in space (SEDS-1, 1993), and operation of an electrodynamic tether with tether current driven in both directions (PMG, 1993). The planned Propulsive Small Expendable Deployer System (ProSEDS) experiment will use the flight-proven Small Expendable Deployer System (SEDS) to deploy a 5-km bare copper tether from a Delta II upper stage to achieve -0,4 N drag thrust, thus deorbiting the stage, The experiment will use a predominantly "bare" tether for current collection in lieu of the endmass collector and insulated tether approach used on previous missions, Theory and ground-based plasma chamber testing indicate that the bare tether is a highly efficient current collector. The flight experiment is a precursor to utilization of the technology on the International Space tation (JSS) for reboost and the electrodynamic tether pper stage demonstration misión which will be capable of orbit raising, lowering, and inclination changes—all using electrodynamic thrust. In addition, the use of this type of propulsion may be attractive for future missions to Jupiter.

La roca magica: Uses of natural zeolites in agriculture and industry

For nearly 200 years since their discovery in 1756, geologists considered the zeolite minerals to occur as fairly large crystals in the vugs and cavities of basalts and other traprock formations. Here, they were prized by mineral collectors, but their small abundance and polymineralic nature defied commercial exploitation. As the synthetic zeolite (molecular sieve) business began to take hold in the late 1950s, huge beds of zeolite-rich sediments, formed by the alteration of volcanic ash (glass) in lake and marine waters, were discovered in the western United States and elsewhere in the world. These beds were found to contain as much as 95% of a single zeolite; they were generally flat-lying and easily mined by surface methods. The properties of these low-cost natural materials mimicked those of many of their synthetic counterparts, and considerable effort has made since that time to develop applications for them based on their unique adsorption, cation-exchange, dehydration–rehydration, and catalytic properties. Natural zeolites (i.e., those found in volcanogenic sedimentary rocks) have been and are being used as building stone, as lightweight aggregate and pozzolans in cements and concretes, as filler in paper, in the take-up of Cs and Sr from nuclear waste and fallout, as soil amendments in agronomy and horticulture, in the removal of ammonia from municipal, industrial, and agricultural waste and drinking waters, as energy exchangers in solar refrigerators, as dietary supplements in animal diets, as consumer deodorizers, in pet litters, in taking up ammonia from animal manures, and as ammonia filters in kidney-dialysis units. From their use in construction during Roman times, to their role as hydroponic (zeoponic) substrate for growing plants on space missions, to their recent success in the healing of cuts and wounds, natural zeolites are now considered to be full-fledged mineral commodities, the use of which promise to expand even more in the future.

The Jordan and the Rhine; or, The East and the West. Being the result of five years' residence in Syria, and five years' residence in Germany.

Mode of access: Internet.

Travels and adventures of the Rev. Joseph Wolff.

Edited by Alfred Gatty.

Les juifs d'Europe et de Palestine : voyage de MM. Keith, Black, Bonar et Mac Cheyne, envoyés par l'Église d'Écosse /

Includes index.

An die Verehrer, Freunde und Schüler Jerusalems̓, Spaldings̓ Tellers̓, Herders̓ und Löfflers̓ /

Mode of access: Internet.

Application of ERS-1 and Topex/Poseidon altimetry using precise orbits

The work described in this thesis concerns the application of radar altimetry, collected from the ERS-1 and TOPEX/POSEIDON missions, to precise satellite orbits computed at Aston University. The data is analysed in a long arc fashion to determine range biases, time tag biases, sea surface topographies and to assess the radial accuracy of the generated orbits through crossover analysis. A sea surface variability study is carried out for the North Sea using repeat altimeter profiles from ERS-1 and TOPEX/POSEIDON in order to verify two local U.K. models for ocean tide and storm surge effects. An on-side technique over the English Channel is performed to compute the ERS-1, TOPEX and POSEIDON altimeter range biases by using a combination of altimetry, precise orbits determined by short arc methods, tide gauge data, GPS measurements, geoid, ocean tide and storm surge models. The remaining part of the thesis presents some techniques for the short arc correction of long arc orbits. Validation of this model is achieved by way of comparison with actual SEASAT short arcs. Simulations are performed for the ERS-1 microwave tracking system, PRARE, using the range data to determine time dependent orbit corrections. Finally, a brief chapter is devoted to the recovery of errors in station coordinates by the use of multiple short arcs.

Requirements, Issues, and Challenges for Sense and Avoid in Unmanned Aircraft Systems

The sense and avoid capability is one of the greatest challenges that has to be addressed to safely integrate unmanned aircraft systems into civil and nonsegregated airspace. This paper gives a review of existing regulations, recommended practices, and standards in sense and avoid for unmanned aircraft systems. Gaps and issues are identified, as are the different factors that are likely to affect actual sense and avoid requirements. It is found that the operational environment (flight altitude, meteorological conditions, and class of airspace) plays an important role when determining the type of flying hazards that the unmanned aircraft system might encounter. In addition, the automation level and the data-link architecture of the unmanned aircraft system are key factors that will definitely determine the sense and avoid system requirements. Tactical unmanned aircraft, performing similar missions to general aviation, are found to be the most challenging systems from an sense and avoid point of view, and further research and development efforts are still needed before their seamless integration into nonsegregated airspace

Post-shock thermochemistry in hypervelocity CO2 and air flow

This work represents ongoing efforts to study high-enthalpy carbon dioxide flows in anticipation of the upcoming Mars Science Laboratory (MSL) and future missions to the red planet. The work is motivated by observed anomalies between experimental and numerical studies in hypervelocity impulse facilities for high enthalpy carbon dioxide flows. In this work, experiments are conducted in the Hypervelocity Expansion Tube (HET) which, by virtue of its flow acceleration process, exhibits minimal freestream dissociation in comparison to reflected shock tunnels. This simplifies the comparison with computational result as freestream dissociation and considerable thermochemical excitation can be neglected. Shock shapes of the MSL aeroshell and spherical geometries are compared with numerical simulations incorporating detailed CO2 thermochemical modeling. The shock stand-off distance has been identified in the past as sensitive to the thermochemical state and as such, is used here as an experimental measurable for comparison with CFD and two different theoretical models. It is seen that models based upon binary scaling assumptions are not applicable for the low-density, small-scale conditions of the current work. Mars Science Laboratory shock shapes at zero angle of attack are also in good agreement with available data from the LENS X expansion tunnel facility, confi rming results are facility-independent for the same type of flow acceleration, and indicating that the flow velocity is a suitable first-order matching parameter for comparative testing. In an e ffort to address surface chemistry issues arising from high-enthalpy carbon dioxide ground-test based experiments, spherical stagnation point and aeroshell heat transfer distributions are also compared with simulation. Very good agreement between experiment and CFD is seen for all shock shapes and heat transfer distributions fall within the non-catalytic and super-catalytic solutions. We also examine spatial temperature profiles in the non-equilibrium relaxation region behind a stationary shock wave in a hypervelocity air Mach 7.42 freestream. The normal shock wave is established through a Mach reflection from an opposing wedge arrangement. Schlieren images confirm that the shock con guration is steady and the location is repeatable. Emission spectroscopy is used to identify dissociated species and to make vibrational temperature measurements using both the nitric oxide and the hydroxyl radical A-X band sequences. Temperature measurements are presented at selected locations behind the normal shock. LIFBASE is used as the simulation spectrum software for OH temperature-fitting, however the need to access higher vibrational and rotational levels for NO leads to the use of an in-house developed algorithm. For NO, results demonstrate the contribution of higher vibrational and rotational levels to the spectra at the conditions of this study. Very good agreement is achieved between the experimentally measured NO vibrational temperatures and calculations performed using an existing state-resolved, three-dimensional forced harmonic oscillator thermochemical model. The measured NO A-X vibrational temperatures are significantly higher than the OH A-X temperatures.

As Forças Armadas de Cabo Verde : Missões de interesse público e a colaboração com entidades civis

O presente trabalho de investigação pretende analisar as missões das Forças Armadas de Cabo Verde e a colaboração com as entidades civis na realização das designadas “Outras Missões de Interesse Público”, em prol da segurança e do desenvolvimento de Cabo Verde. O trabalho começa com a revisão de literatura, fazendo-se o enquadramento geoestratégico e geopolítico de Cabo Verde, o enquadramento das Outras Missões de Interesse Pública imputadas às Forças Armadas de Cabo Verde com recurso à Constituição da República de Cabo Verde, Conceito Estratégico de Defesa e Segurança Nacional e o Regime Geral das Forças Armadas. De seguida, apresenta-se a colaboração das Forças Armadas com as Forças e Serviços de Segurança e Sistema Nacional de Proteção Civil. Abordam-se ainda os conceitos de segurança, defesa, ameaça e risco, tendo por base o modelo Português. De acordo com o modelo de análise aplicado, conclui-se que as Forças Armadas cabo-verdianas participam ativamente na realização das Outras Missões de Interesse Público em colaboração com entidades civil, nomeadamente as Forças e Serviços de Segurança, autarquias locais e empresas privadas que prestam serviço público, e maioria das vezes em regime permanente. As Forças Armadas possuem várias capacidades e meios para realização das Outras Missões de Interesse Público, e apresentam alguns constrangimentos, nomeadamente: a falta de pessoal, recursos financeiros e alguns meios técnicos (transportes, unidades de engenharia e meios de telecomunicação). Num país como Cabo Verde, a participação das Forças Armadas nestas missões é uma mais-valia, contribuindo para a segurança, desenvolvimento do país e para a própria sobrevivência das Forças Armadas. A colaboração da Forças Armadas com as entidades civis funciona normalmente e as principais dificuldades devem-se à complexidade de coordenação e articulação, que devem ser melhoradas. A estrutura e a organização das Forças Armadas de Cabo Verde, de um modo geral, são adequados ao cumprimento deste tipo de missões. Em suma, perante o quadro geoestratégico e geopolítico de Cabo Verde, é indispensável a colaboração das Forças Armadas com entidades civis na realização de Outras Missões de Interesse Público.

Advancing EDL technologies for future space missions : from ground testing facilities to ablative heatshields

Motivated by recent MSL results where the ablation rate of the PICA heatshield was over-predicted, and staying true to the objectives outlined in the NASA Space Technology Roadmaps and Priorities report, this work focuses on advancing EDL technologies for future space missions.

Due to the difficulties in performing flight tests in the hypervelocity regime, a new ground testing facility called the vertical expansion tunnel is proposed. The adverse effects from secondary diaphragm rupture in an expansion tunnel may be reduced or eliminated by orienting the tunnel vertically, matching the test gas pressure and the accelerator gas pressure, and initially separating the test gas from the accelerator gas by density stratification. If some sacrifice of the reservoir conditions can be made, the VET can be utilized in hypervelocity ground testing, without the problems associated with secondary diaphragm rupture.

The performance of different constraints for the Rate-Controlled Constrained-Equilibrium (RCCE) method is investigated in the context of modeling reacting flows characteristic to ground testing facilities, and re-entry conditions. The effectiveness of different constraints are isolated, and new constraints previously unmentioned in the literature are introduced. Three main benefits from the RCCE method were determined: 1) the reduction in number of equations that need to be solved to model a reacting flow; 2) the reduction in stiffness of the system of equations needed to be solved; and 3) the ability to tabulate chemical properties as a function of a constraint once, prior to running a simulation, along with the ability to use the same table for multiple simulations.

Finally, published physical properties of PICA are compiled, and the composition of the pyrolysis gases that form at high temperatures internal to a heatshield is investigated. A necessary link between the composition of the solid resin, and the composition of the pyrolysis gases created is provided. This link, combined with a detailed investigation into a reacting pyrolysis gas mixture, allows a much needed consistent, and thorough description of many of the physical phenomena occurring in a PICA heatshield, and their implications, to be presented.

Through the use of computational fluid mechanics and computational chemistry methods, significant contributions have been made to advancing ground testing facilities, computational methods for reacting flows, and ablation modeling.

How far to the nearest doctor? Stories of medical missions around the world, by Edward M. Dodd.

http://www.archive.org/details/howfartotheneare012020mbp