Seismic data from Colle Gnifetti glacie saddle around borehole KCI, Swiss Alps

Two seismic surveys were carried out on the high-altitude glacier saddle, Colle Gnifetti, Monte Rosa, Italy/Switzerland. Explosive and vibroseismic sources were tested to explore the best way to generate seismic waves to deduce shallow and intermediate properties (<100 m) of firn and ice. The explosive source (SISSY) excites strong surface and diving waves, degrading data quality for processing; no englacial reflections besides the noisy bed reflector are visible. However, the strong diving waves are analyzed to derive the density distribution of the firn pack, yielding results similar to a nearby ice core. The vibrator source (ElViS), used in both P- and SH-wave modes, produces detectable laterally coherent reflections within the firn and ice column. We compare these with ice-core and radar data. The SH-wave data are particularly useful in providing detailed, high-resolution information on firn and ice stratigraphy. Our analyses demonstrate the potential of seismic methods to determine physical properties of firn and ice, particularly density and potentially also crystal-orientation fabric.

Pollen and non-pollen palynomorph records of the Holocene part of the composite sediment core TMD from lake Tso Moriri (NW India) and of modern surface samples from the Tso Moriri region

The high-altitude lake Tso Moriri (32°55'46'' N, 78°19'24'' E; 4522 m a.s.l.) is situated at the margin of the ISM and westerly influences in the Trans-Himalayan region of Ladakh. Human settlements are rare and domestic and wild animals are concentrating at the alpine meadows. A set of modern surface samples and fossil pollen from deep-water TMD core was evaluated with a focus on indicator types revealing human impact, grazing activities and lake system development during the last ca. 12 cal ka BP. Furthermore, the non-pollen palynomorph (NPP) record, comprising remains of limnic algae and invertebrates as well as fungal spores and charred plant tissue fragments, were examined in order to attest palaeolimnic phases and human impact, respectively. Changes in the early and middle Holocene limnic environment are mainly influenced by regional climatic conditions and glacier-fed meltwater flow in the catchment area. The NPP record indicates low lake productivity with high influx of freshwater between ca. 11.5 and 4.5 cal ka BP which is in agreement with the regional monsoon dynamics and published climate reconstructions. Geomorphologic observations suggest that during this period of enhanced precipitation the lake had a regular outflow and contributed large amounts of water to the Sutlej River, the lower reaches of which were integral part of the Indus Civilization area. The inferred minimum fresh water input and maximum lake productivity between ca. 4.5-1.8 cal ka BP coincides with the reconstruction of greatest aridity and glaciation in the Korzong valley resulting in significantly reduced or even ceased outflow. We suggest that lowered lake levels and river discharge on a larger regional scale may have caused irrigation problems and harvest losses in the Indus valley and lowlands occupied by sedentary agricultural communities. This scenario, in turn, supports the theory that, Mature Harappan urbanism (ca. 4.5-3.9 cal ka BP) emerged in order to facilitate storage, protection, administration, and redistribution of crop yields and secondly, the eventual collapse of the Harappan Culture (ca. 3.5-3 cal ka BP) was promoted by prolonged aridity. There is no clear evidence for human impact around Tso Moriri prior to ca. 3.7 cal ka BP, with a more distinct record since ca. 2.7 cal ka BP. This suggests that the sedimentary record from Tso Moriri primarily archives the regional climate history.

Vanadium-Doped In and Sn Sulphides: Photocatalysts able to use the whole visible light spectrum

Using photocatalysis for energy applications depends, more than for environmental purposes or selective chemical synthesis, on converting as much of the solar spectrum as possible; the best photocatalyst, titania, is far from this. Many efforts are pursued to use better that spectrum in photocatalysis, by doping titania or using other materials (mainly oxides, nitrides and sulphides) to obtain a lower bandgap, even if this means decreasing the chemical potential of the electron-hole pairs. Here we introduce an alternative scheme, using an idea recently proposed for photovoltaics: the intermediate band (IB) materials. It consists in introducing in the gap of a semiconductor an intermediate level which, acting like a stepstone, allows an electron jumping from the valence band to the conduction band in two steps, each one absorbing one sub-bandgap photon. For this the IB must be partially filled, to allow both sub-bandgap transitions to proceed at comparable rates; must be made of delocalized states to minimize nonradiative recombination; and should not communicate electronically with the outer world. For photovoltaic use the optimum efficiency so achievable, over 1.5 times that given by a normal semiconductor, is obtained with an overall bandgap around 2.0 eV (which would be near-optimal also for water phtosplitting). Note that this scheme differs from the doping principle usually considered in photocatalysis, which just tries to decrease the bandgap; its aim is to keep the full bandgap chemical potential but using also lower energy photons. In the past we have proposed several IB materials based on extensively doping known semiconductors with light transition metals, checking first of all with quantum calculations that the desired IB structure results. Subsequently we have synthesized in powder form two of them: the thiospinel In2S3 and the layered compound SnS2 (having bandgaps of 2.0 and 2.2 eV respectively) where the octahedral cation is substituted at a â?10% level with vanadium, and we have verified that this substitution introduces in the absorption spectrum the sub-bandgap features predicted by the calculations. With these materials we have verified, using a simple reaction (formic acid oxidation), that the photocatalytic spectral response is indeed extended to longer wavelengths, being able to use even 700 nm photons, without largely degrading the response for above-bandgap photons (i.e. strong recombination is not induced) [3b, 4]. These materials are thus promising for efficient photoevolution of hydrogen from water; work on this is being pursued, the results of which will be presented.

CO2and Rn degassing from the natural analog of Campo de Calatrava(Spain): Implications for monitoring of CO2storage sites

Natural analogs offer a valuable opportunity to investigate the long-term impacts associated with thepotential leakage in geological storage of CO2.Degassing of CO2and radon isotopes (222Rn?220Rn) from soil, gas vents and thermal water dischargeswas investigated in the natural analog of Campo de Calatrava Volcanic Field (CCVF; Central Spain) todetermine the CO2?Rn relationships and to assess the role of CO2as carrier gas for radon. Furthermore,radon measurements to discriminate between shallow and deep gas sources were evaluated under theperspective of their applicability in monitoring programs of carbon storage projects.CO2flux as high as 5000 g m?2d?1and222Rn activities up to 430 kBq m?3were measured;220Rn activi-ties were one order of magnitude lower than those of222Rn. The222Rn/220Rn ratios were used to constrainthe source of the Campo de Calatrava soil gases since a positive correlation between radon isotopic ratiosand CO2fluxes was observed. Thus, in agreement with previous studies, our results indicate a deepmantle-related origin of CO2for both free and soil gases, suggesting that carbon dioxide is an efficientcarrier for Rn. Furthermore, it was ascertained that the increase of222Rn in the soil gases was likely pro-duced by two main processes: (i) direct transport by a carrier gas, i.e., CO2and (ii) generation at shallowlevel due to the presence of relatively high concentrations of dissolved U and Ra in the thermal aquiferof Campo de Calatrava.The diffuse CO2soil flux and radon isotopic surveys carried out in the Campo de Calatrava VolcanicFields can also be applicable to geochemical monitoring programs in CCS (Carbon Capture and Storage)areas as these parameters are useful to: (i) constrain CO2leakages once detected and (ii) monitor both theevolution of the leakages and the effectiveness of subsequent remediation activities. These measurementscan also conveniently be used to detect diffuse leakages.

Impacto en la seguridad operacional por la introducción de nuevos procedimientos en cabina debido a la implantación de futuros conceptos de separación entre aeronaves en la fase de vuelos en ruta

A menudo, la fase del vuelo en ruta sobre áreas de baja densidad de tráfico, se desarrollan en espacios aéreos de alta cota, en los que el servicio de vigilancia es deficiente o simplemente no existente. En este tipo de espacio aéreo garantizar las separaciones entre aeronaves desde el segmento terrestre requiere de procedimientos adecuados a los medios disponibles y que, en general, desembocan en la utilización de unas mínimas de separación muy grandes. En este tipo de espacio aéreo, se ha planteado desde distintos organismos la posibilidad de delegar la responsabilidad de la separación a la aeronave, desarrollando ésta las funciones necesarias para poder asumir tal responsabilidad sin disminuir los umbrales de seguridad. Para que la aeronave pueda asumir la responsabilidad de la separación es necesario dotar a las tripulaciones de nuevos medios técnicos y procedimientos operacionales, los cuales trabajando de forma continua y automática permitan el desarrollo seguro del vuelo en esas circunstancias. El planteamiento de algunos de estos sistemas embarcados así como su validación desde el punto de vista de su aceptación por las tripulaciones es el objetivo del trabajo de investigación realizado y cuyos resultados se presentan en esta tesis. El sistema que se propone trata de resolver los riesgos con los tráficos circundantes garantizando la auto‐separación en vuelo de crucero, evitando y resolviendo conflictos. La aeronave que detecta un riesgo/conflicto negocia una propuesta de solución con la aeronave “intrusa”, una vez la propuesta ha sido negociada, el piloto confirma la maniobra a realizar por la aeronave, la aeronave radiodifunde un mensaje con las intenciones de la maniobra, seguidamente el piloto automático maniobra el avión para implementar la solución y el director de vuelo muestra al piloto la maniobra que se está realizando. ABSTRACT The flight in route phase over areas of low traffic density is usually performed in high altitude airspace, in which the surveillance system is deficient or simply nonexistent. In this type of airspace, to guarantee the separation between aircrafts from the ground, adequate procedures are required to be used with the available systems, and this generally leads to the use of high separation minima. Also, in this type of airspace, it has been discussed by several organizations the possibility of delegating the responsibility of the aircraft separation to the aircraft itself, it carrying out the necessary functions to take on such responsibility without lowering the safety threshold. In order for the aircraft to take on the responsibility of the separation, it is necessary to provide the crew with new technical means and operational procedures, which will result in safe flight under those circumstances. The discussion of some of these systems and their validation from the point of view of acceptance by the crews is the objective of this achieved research work, the findings of which are presented here. The proposed system assists in the surveillance providing the autopilot with information to guarantee the self‐separation with the surrounding in flight traffic, avoiding and solving conflicts. The aircraft which detects the risk/conflict starts a negotiation with the intruder aircraft for finding a conflict resolution, then the pilot of the aircraft approves the solution maneuver and the aircraft broadcasts a message with the maneuver which will be executed. The autopilot maneuvers the aircraft to execute the solution, the evolution of which is shown in the proposed system display and the flight director.

FWS/0BS.

79/39

FWS/0BS.

80/29

FWS/0BS.

81/22

FWS/0BS.

82/69

FWS/0BS.

82/58.1

FWS/0BS.

81/55

FWS/0BS.

79/9