Bases moleculares de la resistencia a insecticidas en la mosca mediterránea de la fruta Ceratitis Capitata (Wiedemann)

La mosca mediterránea de la fruta Ceratitis capitata (Wiedemann, 1824) está considerada una de las plagas clave para la fruticultura. El malatión es un insecticida organofosforado que fue empleado mayoritariamente en España para el control de C. capitata hasta 2009, año en el que dejó de utilizarse por no estar incluido en el anexo I de la Directiva Europea 91/414/ECC. El incremento del uso del malatión, debido a las graves pérdidas económicas causadas por C. capitata, provocó la aparición de poblaciones de campo resistentes. El estudio de una población resistente a malatión, recogida en Castelló en 2004, permitió la identificación de dos mecanismos de resistencia: una mutación puntual (G328A) en la acetilcolinesterasa (AChE) y un mecanismo de resistencia metabólica, probablemente mediado por carboxilesterasas. Teniendo en cuenta estos antecedentes, nos propusimos estudiar los mecanismos implicados en la resistencia a malatión en C. capitata. Además, durante el desarrollo de esta Tesis, el malatión fue sustituido por otros insecticidas como el espinosad y la lambda-cialotrina para el control de la plaga. En este nuevo contexto, es extremadamente importante analizar la susceptibilidad de poblaciones de campo frente a espinosad y estudiar la posible existencia de resistencia cruzada a estos insecticidas, así como sentar las bases para el estudio de futuros mecanismos de resistencia. En primer lugar, analizamos mediante bioensayos con dosis discriminante la susceptibilidad a malatión y espinosad en doce poblaciones de C. capitata de Andalucía, Aragón, Cataluña, Comunidad Valenciana e Islas Baleares; y nuestros resultados sugirieron la presencia de individuos resistentes a malatión en la mayoría de las poblaciones analizadas. En el caso del espinosad, observamos que la susceptibilidad a este insecticida de origen biológico fue elevada en la mayoría de las poblaciones, sin embargo, la población recogida en Xàbia (Alicante) mostró un nivel de susceptibilidad unas dos veces menor al resto de poblaciones. Mediante la selección en laboratorio, obtuvimos dos líneas resistentes a malatión, W-4Km y W-10Km, con unos niveles de resistencia con respeto a la línea susceptible C de 178 y 400 veces, respectivamente. Además, se seleccionó por primera vez en C. capitata una línea altamente resistente a espinosad (Xàbia-W-100s), que actualmente es unas 500 veces más resistente que la línea de laboratorio C. Con el objetivo de escoger la estrategia más adecuada para el manejo de la plaga, estudiamos la susceptibilidad a diferentes tipos de insecticidas en la línea resistente a malatión W- 4Km. En esta línea detectamos resistencia cruzada moderada a los organofosforados fentión, diazinón, fosmet, triclorfón y metil-clorpirifos (de 7 a 16 veces) y frente al carbamato carbaril, al piretroide lambda-cialotrina y al quimioesterilizante lufenurón (de 4 a 6 veces). Por otra parte, la resistencia cruzada frente a espinosad fue baja (1,5 veces). Es importante destacar que los niveles de resistencia estimados frente a todos los insecticidas fueron de uno o dos órdenes de magnitud inferiores al observado en la línea W-4Km frente a malatión (178 veces), hecho que podría deberse, al menos, a dos posibles hipótesis: que la mutación AChE G328A confiera mayor insensibilidad al malaoxón (forma activa del malatión) que a otros insecticidas que tienen como diana la AChE y/o, en segundo lugar, que el mecanismo de resistencia mediado por carboxilesterasas hidrolice el malatión de manera más eficiente que los otros insecticidas analizados. En el estudio de nuevos mecanismos de resistencia en C. capitata, por un lado, analizamos la diversidad de enzimas citocromo P450, asociadas con resistencia metabólica en otras especies, y por otro lado, desarrollamos un sistema para la detección de nuevas mutaciones puntuales que pudiesen aparecer en los genes que codifican la AChE (Ccace2) y la aliesterasa (Ccae7). Mediante el empleo de cebadores degenerados obtuvimos 37 genes CYP, que codifican enzimas P450, pertenecientes a cinco familias. Posteriormente, en un estudio de inducción con fenobarbital, observamos que la expresión de cuatro de los seis genes analizados era susceptible de ser inducida. Por otro lado, se puso a punto un sistema que permite amplificar y secuenciar, a partir de DNA genómico, los exones de los genes Ccace2 y Ccae7 en los que se han encontrado mutaciones relacionadas con resistencia a insecticidas en otras especies. Los resultados obtenidos facilitarán el estudio de nuevos mecanismos de resistencia mediados por estas enzimas en C. capitata. Se diseñó un método PCR-RFLP para identificar los individuos portadores de la mutación AChE G328A (alelo de resistencia Ccace2R) sin la necesidad de realizar bioensayos y que, además, permite detectar resistencia cuando ésta se encuentra a baja frecuencia. Según el análisis realizado, el alelo Ccace2R se observó en 25 de las 27 localidades españolas muestreadas en el territorio español, incluyendo las Islas Baleares y Canarias. Sin embargo, este alelo no se detectó en poblaciones procedentes de once países y de cinco continentes. El análisis de la presencia del alelo Ccace2R en las líneas resistentes a malatión durante el proceso de selección en el laboratorio mostró una rápida disminución de los homocigotos, tanto para el alelo susceptible como para el alelo de resistencia, en favor de los individuos heterocigotos. Así, después de 52 generaciones de selección, se observó que la totalidad de los individuos analizados de la línea W-10Km presentaban un genotipo heterocigoto para la mutación AChE G328A. Este desequilibrio contradice la segregación mendeliana esperada para un gen con dos alelos pero podría ser explicado por la existencia de una duplicación del gen Ccace2. La demostración de la presencia de esta duplicación se realizó mediante: i) el cruzamiento de individuos heterocigotos de la línea W-10Km con homocigotos susceptibles de la línea C, que dio lugar a una descendencia en la que el 100% de los individuos eran heterocigotos; ii) la evaluación del número de copias del gen Ccace2 por PCR cuantitativa en tiempo real (qPCR), que resultó dos veces mayor en individuos de la línea W-10Km en comparación con los de la línea C; iii) el análisis del nivel de expresión de Ccace2, que fue el doble en la línea W-10Km con respecto a la línea C, y iv) el estudio de la actividad AChE, que resultó mayor en los individuos de la línea W-10Km. Según los resultados obtenidos, una duplicación del gen Ccace2 provoca la coexistencia en un mismo cromosoma del alelo silvestre y del alelo mutado y, además, las dos copias del gen Ccace2, al estar ligadas, producen una heterocigosis permanente (Ccace2RS). De esta manera se explica que el hecho de que 100% de los individuos de la línea W-10Km mostrasen un perfil de restricción correspondiente a un individuo heterocigoto ya que, en realidad, eran homocigotos estructurales para la duplicación (genotipo CCace2RS/RS). Se ha detectado un coste biológico asociado a la duplicación que consiste en un incremento en la mortalidad acumulada de los adultos a partir del séptimo día después de la emergencia. La descripción de la duplicación Ccace2RS supone la identificación de un nuevo mecanismo de resistencia a malatión en C. capitata. Finalmente, mediante el diseño de un método de doble PCR-RFLP se determinó la presencia de la duplicación Ccace2RS en la mayoría de las poblaciones españolas. La proporción de individuos portadores de la duplicación osciló entre el 5% y el 35%, observándose los mayores valores de frecuencia en las poblaciones de C. capitata recogidas en la cuenca mediterránea. Podemos por lo tanto concluir que la resistencia a malatión asociada a la mutación AChE G328A y a la duplicación Ccace2RS está ampliamente establecida en las poblaciones españolas de C. capitata. Nuestros resultados desaconsejan la utilización del malatión (si fuera de nuevo autorizado) o de otros organofosforados para el control de esta plaga. Además, una de las líneas resistentes a malatión mostró resistencia cruzada frente a insecticidas con diferentes modos de acción y que se utilizan actualmente para el control de C. capitata, tales como lambda-cialotrina y lufenurón. La alta susceptibilidad a espinosad observada en las poblaciones españolas, así como la reducida resistencia cruzada estimada para este insecticida, sugieren que su utilización es adecuada para el control de la plaga. Sin embargo, la utilización de un sólo insecticida puede entrañar riesgos por favorecer la selección de resistencia, de hecho, mediante selección en laboratorio se obtuvo una población altamente resistente a espinosad. Por tanto, es recomendable implementar programas de control integrado y de manejo de la resistencia en C. capitata utilizando distintos sistemas de control e insecticidas con diferentes mecanismos de acción que permitan su sostenibilidad en el tiempo. Los sistemas de detección de alelos de resistencia desarrollados en este trabajo permitirán la detección precoz de resistencia en campo, facilitando la decisión sobre el sistema de control más adecuado. Además, los conocimientos generados podrán contribuir al desarrollo de nuevos sistemas de detección para otros mecanismos de resistencia. Abstract. The Mediterranean fruit fly, Ceratitis capitata (Wiedemann, 1824), is considered one of the most harmful pests in fruit crops. Until 2009, when malathion use was banned due to its not inclusion in the Annex I of Directive 91/414/EEC, the application of this organophosphate (OP) insecticide in Spain increased gradually due to the large economic losses caused by C. capitata. The increase in the frequency of treatments resulted in the development of resistant field populations. The study of a malathion-resistant population, collected in 2004 in Castelló (Comunidad Valenciana), allowed the identification of two resistance mechanisms: a single point mutation (G328A) in the target acetylcholinesterase (AChE), as well as a metabolic resistance mechanism, most likely carboxylesterase-mediated. Taking all the preceding into account, we studied the malathion resistance mechanisms in C. capitata. During the development of this PhD Thesis malathion use was banned by the European Union, being replaced by other insecticides, such as spinosad and lambda-cyhalotrin. Within this new working frame, the need to analyse the possible existence of cross-resistance to these insecticides and the susceptibility to spinosad in field populations was raised. This would define the baseline for future studies on resistance mechanisms. Firstly, through discriminant dose bioassays, we analysed malathion and spinosad susceptibility in twelve C. capitata populations from Andalucia, Aragon, Cataluña, C. Valenciana and the Baleares Islands. Our results suggest the presence of malathion-resistant individuals in most of the populations analysed. Regarding spinosad, we noticed a high susceptibility to this biologically derived insecticide in most of the populations, but in the one collected in Xabia (Alicante), which had a susceptibility level two times lower than the rest of populations. Through laboratory selection, we obtained two malathion-resistant strains, W-4Km and W-10Km, with resistance levels 178- and 400-fold, respectively, compared to the control susceptible C strain. Besides, a strain highly-resistant to spinosad (Xabia-W-100s), 500-times more resistant than control C strain, was selected. In order to decide the most appropriate management strategy for the pest, we studied the susceptibility to different insecticides in the malathion-resistant W-4Km strain. We detected a moderated cross-resistance to the OPs fenthion, diazinon, phosmet, trichlorphon and methylchlorpyrifos (7- to 16-fold), and to the carbamate carbaryl, the pyretroid lambda-cyhalotrin and the chemosterilizer lufenuron (4- to 6-fold). On the other hand, cross-resistance to spinosad was low (1.5-fold). It is important to note that resistance levels to all insecticides were one or two orders of magnitude less than that observed against malathion in W-4Km strain (178-fold), a fact that might be due to, at least, two possible causes: mutation AChE G328A may provide a higher insensitivity to malaoxon (the active form of malathion) than to other insecticides having AChE as target, and/or, secondly, the carboxylesterase-mediated resistance mechanism hydrolyzes malathion more efficiently than all other analysed insecticides. To investigate new resistance mechanisms in C. capitata we analysed the diversity of the cytochrome P450 enzymes, which have been associated to metabolic resistance in insects, and we developed a new method to detect single point mutations in acetylcholinesterase (Ccace2) and aliesterase (Ccae7) genes that could appear. Using degenerate primers we obtained 37 CYP genes, coding P450 enzymes, included in five families. Afterwards, in a phenobarbital-induction study, we observed that the expression of 4 out of the 6 analysed genes could be induced. On the other hand, a system was set up to amplify and to sequence from genomic DNA the exons of genes Ccace2 and Ccae7 where mutations related to insecticide resistance have been found in other species. The results obtained could facilitate the study of new resistance mechanisms in C. capitata mediated by these enzymes. A PCR-RFLP method was designed to detect the presence of the mutation AChE G328A (resistance allele Ccace2R), with no need to perform bioassays and allowing detecting resistance at low frequency. According to the analysis, the resistance allele was found in 25 out of 27 sampled locations in Spain, including the Balearic and the Canary Islands. However, this allele was not detected in other populations collected in 11 countries from 5 continents. The follow-up of the presence of the allele Ccace2R in the malathion-resistant strains during the selection process in the laboratory showed a quick decrease in homozygous individuals, for both the susceptible and the resistant alleles, favouring heterozygous. Thus, after 52 generations of selection, all the individuals analysed from W-10Km strain showed a heterozygous genotype for mutation AChE G328A, contradicting mendelian segregation as expected for a gene with two alleles. Afterwards, we were able to demonstrate that this was caused by the presence of a duplication of the gene coding acetylcholinesterase by: i) crossing heterozygous individuals from W-10Km strain with susceptible homozygous from C strain, originating a F1 population in which 100% of individuals were heterozygous; ii) evaluating the number of copies of gen Ccace2 by quantitative PCR in real time (qPCR), that happened to be twice higher in individuals from W-10Km VII strain when compared with C strain; iii) analysing the level of expression of Ccace2, twice in W- 10Km strain when compared to C strain; iv) studying the acetylcholinesterase activity, that was higher in individuals from W-10Km strain. According to these results, duplication of gen Ccace2 originates the coexistence of the susceptible and the resistant allele in the same chromosome. The two linked copies of the gene Ccace2 provoke the existence of permanent heterozygosis (Ccace2RS). This explains why the 100% of individuals from W-10Km strain showed an heterozygous restriction pattern since, in fact, they were structural homozygotes for the duplication (genotype Ccace2RS/RS). A biological cost has been detected associated to this duplication, consisting in a rise in accumulated adult mortality from the seventh day after emergence. The Ccace2RS duplication described in this study represents a new resistance mechanism to malathion in C. capitata. Finally, by the design of a double PCR-RFLP method, the presence of Ccace2RS duplication was confirmed in most of the Spanish populations. We observed that the proportion of individuals carrying the duplication oscillated between 5 and 35%, the frequency being higher in those C. capitata populations collected in the area of the Mediterranean basin. Therefore, we can conclude that malathion resistance associated to mutation AChE G328A and to Ccace2RS duplication are widely distributed in Spanish populations of C. capitata. Our results advice against the use of malathion (if it came to be newly authorized for use) or other OPs for the control of this pest. Besides, one of the malathion-resistant strains showed cross-resistance against insecticides with diverse action modes that are currently used for pest control, such as lambdacyhalotrin and lufenuron. High susceptibility to spinosad in the Spanish populations, as well as the reduced cross-resistance estimated for this insecticide suggests its adequacy for Medfly control. However, the use of a single insecticide is a risky strategy since it favours the selection of resistance. In fact, a population highly resistant to spinosad was obtained through laboratory selection. Therefore, it is advisable to implement integrated pest management (IPM) and resistance management programs for C. capitata control. Using insecticides with different modes of action and diverse control systems would contribute to the sustainability of the pest control. The resistance allele detection systems developed through this work will allow the early detection of resistance in the field, making possible the selection of the most appropriate method for pest control. Besides, the generated knowledge may also contribute to the development of new detection systems for other resistance mechanisms.

Evaluation/Optimization of reservoir operation rules for flood management using an integrated hydrologic-hydraulic framework

Se ha presentado la evaluación y optimización de las reglas de operación de un embalse para gestión de avenidas usando un entorno integrado hidrológico- hidráulico de tipo Monte Carlo. Some reservoirs play a major role in flood protection, managing the floods and reducing or delaying the peak discharges in the river downstream. However, the changing environment (natural and anthropological changes) requires the development of more elaborated strategies for reservoir operation. Three factors are relevant: 1) the natural variability of inflow hydrographs, 2) the competition for reservoir storage capacity between flood control and other uses, and 3) the existence of built-up areas on downstream river reaches. A framework for evaluation/optimization of reservoir operation rules for flood management in a changing environment is presented in this study. The study was carried out using an integrated hydrologic – hydraulic model in a Monte Carlo framework.

Methodologies for Collision Risk Computation = Metodologías para Cálculo de Riesgo de Colisión

Esta tesis aborda metodologías para el cálculo de riesgo de colisión de satélites. La minimización del riesgo de colisión se debe abordar desde dos puntos de vista distintos. Desde el punto de vista operacional, es necesario filtrar los objetos que pueden presentar un encuentro entre todos los objetos que comparten el espacio con un satélite operacional. Puesto que las órbitas, del objeto operacional y del objeto envuelto en la colisión, no se conocen perfectamente, la geometría del encuentro y el riesgo de colisión deben ser evaluados. De acuerdo con dicha geometría o riesgo, una maniobra evasiva puede ser necesaria para evitar la colisión. Dichas maniobras implican un consumo de combustible que impacta en la capacidad de mantenimiento orbital y por tanto de la visa útil del satélite. Por tanto, el combustible necesario a lo largo de la vida útil de un satélite debe ser estimado en fase de diseño de la misión para una correcta definición de su vida útil, especialmente para satélites orbitando en regímenes orbitales muy poblados. Los dos aspectos, diseño de misión y aspectos operacionales en relación con el riesgo de colisión están abordados en esta tesis y se resumen en la Figura 3. En relación con los aspectos relacionados con el diseño de misión (parte inferior de la figura), es necesario evaluar estadísticamente las características de de la población espacial y las teorías que permiten calcular el número medio de eventos encontrados por una misión y su capacidad de reducir riesgo de colisión. Estos dos aspectos definen los procedimientos más apropiados para reducir el riesgo de colisión en fase operacional. Este aspecto es abordado, comenzando por la teoría descrita en [Sánchez-Ortiz, 2006]T.14 e implementada por el autor de esta tesis en la herramienta ARES [Sánchez-Ortiz, 2004b]T.15 proporcionada por ESA para la evaluación de estrategias de evitación de colisión. Esta teoría es extendida en esta tesis para considerar las características de los datos orbitales disponibles en las fases operacionales de un satélite (sección 4.3.3). Además, esta teoría se ha extendido para considerar riesgo máximo de colisión cuando la incertidumbre de las órbitas de objetos catalogados no es conocida (como se da el caso para los TLE), y en el caso de querer sólo considerar riesgo de colisión catastrófico (sección 4.3.2.3). Dichas mejoras se han incluido en la nueva versión de ARES [Domínguez-González and Sánchez-Ortiz, 2012b]T.12 puesta a disposición a través de [SDUP,2014]R.60. En fase operacional, los catálogos que proporcionan datos orbitales de los objetos espaciales, son procesados rutinariamente, para identificar posibles encuentros que se analizan en base a algoritmos de cálculo de riesgo de colisión para proponer maniobras de evasión. Actualmente existe una única fuente de datos públicos, el catálogo TLE (de sus siglas en inglés, Two Line Elements). Además, el Joint Space Operation Center (JSpOC) Americano proporciona mensajes con alertas de colisión (CSM) cuando el sistema de vigilancia americano identifica un posible encuentro. En función de los datos usados en fase operacional (TLE o CSM), la estrategia de evitación puede ser diferente debido a las características de dicha información. Es preciso conocer las principales características de los datos disponibles (respecto a la precisión de los datos orbitales) para estimar los posibles eventos de colisión encontrados por un satélite a lo largo de su vida útil. En caso de los TLE, cuya precisión orbital no es proporcionada, la información de precisión orbital derivada de un análisis estadístico se puede usar también en el proceso operacional así como en el diseño de la misión. En caso de utilizar CSM como base de las operaciones de evitación de colisiones, se conoce la precisión orbital de los dos objetos involucrados. Estas características se han analizado en detalle, evaluando estadísticamente las características de ambos tipos de datos. Una vez concluido dicho análisis, se ha analizado el impacto de utilizar TLE o CSM en las operaciones del satélite (sección 5.1). Este análisis se ha publicado en una revista especializada [Sánchez-Ortiz, 2015b]T.3. En dicho análisis, se proporcionan recomendaciones para distintas misiones (tamaño del satélite y régimen orbital) en relación con las estrategias de evitación de colisión para reducir el riesgo de colisión de manera significativa. Por ejemplo, en el caso de un satélite en órbita heliosíncrona en régimen orbital LEO, el valor típico del ACPL que se usa de manera extendida es 10-4. Este valor no es adecuado cuando los esquemas de evitación de colisión se realizan sobre datos TLE. En este caso, la capacidad de reducción de riesgo es prácticamente nula (debido a las grandes incertidumbres de los datos TLE) incluso para tiempos cortos de predicción. Para conseguir una reducción significativa del riesgo, sería necesario usar un ACPL en torno a 10-6 o inferior, produciendo unas 10 alarmas al año por satélite (considerando predicciones a un día) o 100 alarmas al año (con predicciones a tres días). Por tanto, la principal conclusión es la falta de idoneidad de los datos TLE para el cálculo de eventos de colisión. Al contrario, usando los datos CSM, debido a su mejor precisión orbital, se puede obtener una reducción significativa del riesgo con ACPL en torno a 10-4 (considerando 3 días de predicción). Incluso 5 días de predicción pueden ser considerados con ACPL en torno a 10-5. Incluso tiempos de predicción más largos se pueden usar (7 días) con reducción del 90% del riesgo y unas 5 alarmas al año (en caso de predicciones de 5 días, el número de maniobras se mantiene en unas 2 al año). La dinámica en GEO es diferente al caso LEO y hace que el crecimiento de las incertidumbres orbitales con el tiempo de propagación sea menor. Por el contrario, las incertidumbres derivadas de la determinación orbital son peores que en LEO por las diferencias en las capacidades de observación de uno y otro régimen orbital. Además, se debe considerar que los tiempos de predicción considerados para LEO pueden no ser apropiados para el caso de un satélite GEO (puesto que tiene un periodo orbital mayor). En este caso usando datos TLE, una reducción significativa del riesgo sólo se consigue con valores pequeños de ACPL, produciendo una alarma por año cuando los eventos de colisión se predicen a un día vista (tiempo muy corto para implementar maniobras de evitación de colisión).Valores más adecuados de ACPL se encuentran entre 5•10-8 y 10-7, muy por debajo de los valores usados en las operaciones actuales de la mayoría de las misiones GEO (de nuevo, no se recomienda en este régimen orbital basar las estrategias de evitación de colisión en TLE). Los datos CSM permiten una reducción de riesgo apropiada con ACPL entre 10-5 y 10-4 con tiempos de predicción cortos y medios (10-5 se recomienda para predicciones a 5 o 7 días). El número de maniobras realizadas sería una en 10 años de misión. Se debe notar que estos cálculos están realizados para un satélite de unos 2 metros de radio. En el futuro, otros sistemas de vigilancia espacial (como el programa SSA de la ESA), proporcionarán catálogos adicionales de objetos espaciales con el objetivo de reducir el riesgo de colisión de los satélites. Para definir dichos sistemas de vigilancia, es necesario identificar las prestaciones del catalogo en función de la reducción de riesgo que se pretende conseguir. Las características del catálogo que afectan principalmente a dicha capacidad son la cobertura (número de objetos incluidos en el catalogo, limitado principalmente por el tamaño mínimo de los objetos en función de las limitaciones de los sensores utilizados) y la precisión de los datos orbitales (derivada de las prestaciones de los sensores en relación con la precisión de las medidas y la capacidad de re-observación de los objetos). El resultado de dicho análisis (sección 5.2) se ha publicado en una revista especializada [Sánchez-Ortiz, 2015a]T.2. Este análisis no estaba inicialmente previsto durante la tesis, y permite mostrar como la teoría descrita en esta tesis, inicialmente definida para facilitar el diseño de misiones (parte superior de la figura 1) se ha extendido y se puede aplicar para otros propósitos como el dimensionado de un sistema de vigilancia espacial (parte inferior de la figura 1). La principal diferencia de los dos análisis se basa en considerar las capacidades de catalogación (precisión y tamaño de objetos observados) como una variable a modificar en el caso de un diseño de un sistema de vigilancia), siendo fijas en el caso de un diseño de misión. En el caso de las salidas generadas en el análisis, todos los aspectos calculados en un análisis estadístico de riesgo de colisión son importantes para diseño de misión (con el objetivo de calcular la estrategia de evitación y la cantidad de combustible a utilizar), mientras que en el caso de un diseño de un sistema de vigilancia, los aspectos más importantes son el número de maniobras y falsas alarmas (fiabilidad del sistema) y la capacidad de reducción de riesgo (efectividad del sistema). Adicionalmente, un sistema de vigilancia espacial debe ser caracterizado por su capacidad de evitar colisiones catastróficas (evitando así in incremento dramático de la población de basura espacial), mientras que el diseño de una misión debe considerar todo tipo de encuentros, puesto que un operador está interesado en evitar tanto las colisiones catastróficas como las letales. Del análisis de las prestaciones (tamaño de objetos a catalogar y precisión orbital) requeridas a un sistema de vigilancia espacial se concluye que ambos aspectos han de ser fijados de manera diferente para los distintos regímenes orbitales. En el caso de LEO se hace necesario observar objetos de hasta 5cm de radio, mientras que en GEO se rebaja este requisito hasta los 100 cm para cubrir las colisiones catastróficas. La razón principal para esta diferencia viene de las diferentes velocidades relativas entre los objetos en ambos regímenes orbitales. En relación con la precisión orbital, ésta ha de ser muy buena en LEO para poder reducir el número de falsas alarmas, mientras que en regímenes orbitales más altos se pueden considerar precisiones medias. En relación con los aspectos operaciones de la determinación de riesgo de colisión, existen varios algoritmos de cálculo de riesgo entre dos objetos espaciales. La Figura 2 proporciona un resumen de los casos en cuanto a algoritmos de cálculo de riesgo de colisión y como se abordan en esta tesis. Normalmente se consideran objetos esféricos para simplificar el cálculo de riesgo (caso A). Este caso está ampliamente abordado en la literatura y no se analiza en detalle en esta tesis. Un caso de ejemplo se proporciona en la sección 4.2. Considerar la forma real de los objetos (caso B) permite calcular el riesgo de una manera más precisa. Un nuevo algoritmo es definido en esta tesis para calcular el riesgo de colisión cuando al menos uno de los objetos se considera complejo (sección 4.4.2). Dicho algoritmo permite calcular el riesgo de colisión para objetos formados por un conjunto de cajas, y se ha presentado en varias conferencias internacionales. Para evaluar las prestaciones de dicho algoritmo, sus resultados se han comparado con un análisis de Monte Carlo que se ha definido para considerar colisiones entre cajas de manera adecuada (sección 4.1.2.3), pues la búsqueda de colisiones simples aplicables para objetos esféricos no es aplicable a este caso. Este análisis de Monte Carlo se considera la verdad a la hora de calcular los resultados del algoritmos, dicha comparativa se presenta en la sección 4.4.4. En el caso de satélites que no se pueden considerar esféricos, el uso de un modelo de la geometría del satélite permite descartar eventos que no son colisiones reales o estimar con mayor precisión el riesgo asociado a un evento. El uso de estos algoritmos con geometrías complejas es más relevante para objetos de dimensiones grandes debido a las prestaciones de precisión orbital actuales. En el futuro, si los sistemas de vigilancia mejoran y las órbitas son conocidas con mayor precisión, la importancia de considerar la geometría real de los satélites será cada vez más relevante. La sección 5.4 presenta un ejemplo para un sistema de grandes dimensiones (satélite con un tether). Adicionalmente, si los dos objetos involucrados en la colisión tienen velocidad relativa baja (y geometría simple, Caso C en la Figura 2), la mayor parte de los algoritmos no son aplicables requiriendo implementaciones dedicadas para este caso particular. En esta tesis, uno de estos algoritmos presentado en la literatura [Patera, 2001]R.26 se ha analizado para determinar su idoneidad en distintos tipos de eventos (sección 4.5). La evaluación frete a un análisis de Monte Carlo se proporciona en la sección 4.5.2. Tras este análisis, se ha considerado adecuado para abordar las colisiones de baja velocidad. En particular, se ha concluido que el uso de algoritmos dedicados para baja velocidad son necesarios en función del tamaño del volumen de colisión proyectado en el plano de encuentro (B-plane) y del tamaño de la incertidumbre asociada al vector posición entre los dos objetos. Para incertidumbres grandes, estos algoritmos se hacen más necesarios pues la duración del intervalo en que los elipsoides de error de los dos objetos pueden intersecar es mayor. Dicho algoritmo se ha probado integrando el algoritmo de colisión para objetos con geometrías complejas. El resultado de dicho análisis muestra que este algoritmo puede ser extendido fácilmente para considerar diferentes tipos de algoritmos de cálculo de riesgo de colisión (sección 4.5.3). Ambos algoritmos, junto con el método Monte Carlo para geometrías complejas, se han implementado en la herramienta operacional de la ESA CORAM, que es utilizada para evaluar el riesgo de colisión en las actividades rutinarias de los satélites operados por ESA [Sánchez-Ortiz, 2013a]T.11. Este hecho muestra el interés y relevancia de los algoritmos desarrollados para la mejora de las operaciones de los satélites. Dichos algoritmos han sido presentados en varias conferencias internacionales [Sánchez-Ortiz, 2013b]T.9, [Pulido, 2014]T.7,[Grande-Olalla, 2013]T.10, [Pulido, 2014]T.5, [Sánchez-Ortiz, 2015c]T.1. ABSTRACT This document addresses methodologies for computation of the collision risk of a satellite. Two different approaches need to be considered for collision risk minimisation. On an operational basis, it is needed to perform a sieve of possible objects approaching the satellite, among all objects sharing the space with an operational satellite. As the orbits of both, satellite and the eventual collider, are not perfectly known but only estimated, the miss-encounter geometry and the actual risk of collision shall be evaluated. In the basis of the encounter geometry or the risk, an eventual manoeuvre may be required to avoid the conjunction. Those manoeuvres will be associated to a reduction in the fuel for the mission orbit maintenance, and thus, may reduce the satellite operational lifetime. Thus, avoidance manoeuvre fuel budget shall be estimated, at mission design phase, for a better estimation of mission lifetime, especially for those satellites orbiting in very populated orbital regimes. These two aspects, mission design and operational collision risk aspects, are summarised in Figure 3, and covered along this thesis. Bottom part of the figure identifies the aspects to be consider for the mission design phase (statistical characterisation of the space object population data and theory computing the mean number of events and risk reduction capability) which will define the most appropriate collision avoidance approach at mission operational phase. This part is covered in this work by starting from the theory described in [Sánchez-Ortiz, 2006]T.14 and implemented by this author in ARES tool [Sánchez-Ortiz, 2004b]T.15 provided by ESA for evaluation of collision avoidance approaches. This methodology has been now extended to account for the particular features of the available data sets in operational environment (section 4.3.3). Additionally, the formulation has been extended to allow evaluating risk computation approached when orbital uncertainty is not available (like the TLE case) and when only catastrophic collisions are subject to study (section 4.3.2.3). These improvements to the theory have been included in the new version of ESA ARES tool [Domínguez-González and Sánchez-Ortiz, 2012b]T.12 and available through [SDUP,2014]R.60. At the operation phase, the real catalogue data will be processed on a routine basis, with adequate collision risk computation algorithms to propose conjunction avoidance manoeuvre optimised for every event. The optimisation of manoeuvres in an operational basis is not approached along this document. Currently, American Two Line Element (TLE) catalogue is the only public source of data providing orbits of objects in space to identify eventual conjunction events. Additionally, Conjunction Summary Message (CSM) is provided by Joint Space Operation Center (JSpOC) when the American system identifies a possible collision among satellites and debris. Depending on the data used for collision avoidance evaluation, the conjunction avoidance approach may be different. The main features of currently available data need to be analysed (in regards to accuracy) in order to perform estimation of eventual encounters to be found along the mission lifetime. In the case of TLE, as these data is not provided with accuracy information, operational collision avoidance may be also based on statistical accuracy information as the one used in the mission design approach. This is not the case for CSM data, which includes the state vector and orbital accuracy of the two involved objects. This aspect has been analysed in detail and is depicted in the document, evaluating in statistical way the characteristics of both data sets in regards to the main aspects related to collision avoidance. Once the analysis of data set was completed, investigations on the impact of those features in the most convenient avoidance approaches have been addressed (section 5.1). This analysis is published in a peer-reviewed journal [Sánchez-Ortiz, 2015b]T.3. The analysis provides recommendations for different mission types (satellite size and orbital regime) in regards to the most appropriate collision avoidance approach for relevant risk reduction. The risk reduction capability is very much dependent on the accuracy of the catalogue utilized to identify eventual collisions. Approaches based on CSM data are recommended against the TLE based approach. Some approaches based on the maximum risk associated to envisaged encounters are demonstrated to report a very large number of events, which makes the approach not suitable for operational activities. Accepted Collision Probability Levels are recommended for the definition of the avoidance strategies for different mission types. For example for the case of a LEO satellite in the Sun-synchronous regime, the typically used ACPL value of 10-4 is not a suitable value for collision avoidance schemes based on TLE data. In this case the risk reduction capacity is almost null (due to the large uncertainties associated to TLE data sets, even for short time-to-event values). For significant reduction of risk when using TLE data, ACPL on the order of 10-6 (or lower) seems to be required, producing about 10 warnings per year and mission (if one-day ahead events are considered) or 100 warnings per year (for three-days ahead estimations). Thus, the main conclusion from these results is the lack of feasibility of TLE for a proper collision avoidance approach. On the contrary, for CSM data, and due to the better accuracy of the orbital information when compared with TLE, ACPL on the order of 10-4 allows to significantly reduce the risk. This is true for events estimated up to 3 days ahead. Even 5 days ahead events can be considered, but ACPL values down to 10-5 should be considered in such case. Even larger prediction times can be considered (7 days) for risk reduction about 90%, at the cost of larger number of warnings up to 5 events per year, when 5 days prediction allows to keep the manoeuvre rate in 2 manoeuvres per year. Dynamics of the GEO orbits is different to that in LEO, impacting on a lower increase of orbits uncertainty along time. On the contrary, uncertainties at short prediction times at this orbital regime are larger than those at LEO due to the differences in observation capabilities. Additionally, it has to be accounted that short prediction times feasible at LEO may not be appropriate for a GEO mission due to the orbital period being much larger at this regime. In the case of TLE data sets, significant reduction of risk is only achieved for small ACPL values, producing about a warning event per year if warnings are raised one day in advance to the event (too short for any reaction to be considered). Suitable ACPL values would lay in between 5•10-8 and 10-7, well below the normal values used in current operations for most of the GEO missions (TLE-based strategies for collision avoidance at this regime are not recommended). On the contrary, CSM data allows a good reduction of risk with ACPL in between 10-5 and 10-4 for short and medium prediction times. 10-5 is recommended for prediction times of five or seven days. The number of events raised for a suitable warning time of seven days would be about one in a 10-year mission. It must be noted, that these results are associated to a 2 m radius spacecraft, impact of the satellite size are also analysed within the thesis. In the future, other Space Situational Awareness Systems (SSA, ESA program) may provide additional catalogues of objects in space with the aim of reducing the risk. It is needed to investigate which are the required performances of those catalogues for allowing such risk reduction. The main performance aspects are coverage (objects included in the catalogue, mainly limited by a minimum object size derived from sensor performances) and the accuracy of the orbital data to accurately evaluate the conjunctions (derived from sensor performance in regards to object observation frequency and accuracy). The results of these investigations (section 5.2) are published in a peer-reviewed journal [Sánchez-Ortiz, 2015a]T.2. This aspect was not initially foreseen as objective of the thesis, but it shows how the theory described in the thesis, initially defined for mission design in regards to avoidance manoeuvre fuel allocation (upper part of figure 1), is extended and serves for additional purposes as dimensioning a Space Surveillance and Tracking (SST) system (bottom part of figure below). The main difference between the two approaches is the consideration of the catalogue features as part of the theory which are not modified (for the satellite mission design case) instead of being an input for the analysis (in the case of the SST design). In regards to the outputs, all the features computed by the statistical conjunction analysis are of importance for mission design (with the objective of proper global avoidance strategy definition and fuel allocation), whereas for the case of SST design, the most relevant aspects are the manoeuvre and false alarm rates (defining a reliable system) and the Risk Reduction capability (driving the effectiveness of the system). In regards to the methodology for computing the risk, the SST system shall be driven by the capacity of providing the means to avoid catastrophic conjunction events (avoiding the dramatic increase of the population), whereas the satellite mission design should consider all type of encounters, as the operator is interested on avoiding both lethal and catastrophic collisions. From the analysis of the SST features (object coverage and orbital uncertainty) for a reliable system, it is concluded that those two characteristics are to be imposed differently for the different orbital regimes, as the population level is different depending on the orbit type. Coverage values range from 5 cm for very populated LEO regime up to 100 cm in the case of GEO region. The difference on this requirement derives mainly from the relative velocity of the encounters at those regimes. Regarding the orbital knowledge of the catalogues, very accurate information is required for objects in the LEO region in order to limit the number of false alarms, whereas intermediate orbital accuracy can be considered for higher orbital regimes. In regards to the operational collision avoidance approaches, several collision risk algorithms are used for evaluation of collision risk of two pair of objects. Figure 2 provides a summary of the different collision risk algorithm cases and indicates how they are covered along this document. The typical case with high relative velocity is well covered in literature for the case of spherical objects (case A), with a large number of available algorithms, that are not analysed in detailed in this work. Only a sample case is provided in section 4.2. If complex geometries are considered (Case B), a more realistic risk evaluation can be computed. New approach for the evaluation of risk in the case of complex geometries is presented in this thesis (section 4.4.2), and it has been presented in several international conferences. The developed algorithm allows evaluating the risk for complex objects formed by a set of boxes. A dedicated Monte Carlo method has also been described (section 4.1.2.3) and implemented to allow the evaluation of the actual collisions among a large number of simulation shots. This Monte Carlo runs are considered the truth for comparison of the algorithm results (section 4.4.4). For spacecrafts that cannot be considered as spheres, the consideration of the real geometry of the objects may allow to discard events which are not real conjunctions, or estimate with larger reliability the risk associated to the event. This is of particular importance for the case of large spacecrafts as the uncertainty in positions of actual catalogues does not reach small values to make a difference for the case of objects below meter size. As the tracking systems improve and the orbits of catalogued objects are known more precisely, the importance of considering actual shapes of the objects will become more relevant. The particular case of a very large system (as a tethered satellite) is analysed in section 5.4. Additionally, if the two colliding objects have low relative velocity (and simple geometries, case C in figure above), the most common collision risk algorithms fail and adequate theories need to be applied. In this document, a low relative velocity algorithm presented in the literature [Patera, 2001]R.26 is described and evaluated (section 4.5). Evaluation through comparison with Monte Carlo approach is provided in section 4.5.2. The main conclusion of this analysis is the suitability of this algorithm for the most common encounter characteristics, and thus it is selected as adequate for collision risk estimation. Its performances are evaluated in order to characterise when it can be safely used for a large variety of encounter characteristics. In particular, it is found that the need of using dedicated algorithms depend on both the size of collision volume in the B-plane and the miss-distance uncertainty. For large uncertainties, the need of such algorithms is more relevant since for small uncertainties the encounter duration where the covariance ellipsoids intersect is smaller. Additionally, its application for the case of complex satellite geometries is assessed (case D in figure above) by integrating the developed algorithm in this thesis with Patera’s formulation for low relative velocity encounters. The results of this analysis show that the algorithm can be easily extended for collision risk estimation process suitable for complex geometry objects (section 4.5.3). The two algorithms, together with the Monte Carlo method, have been implemented in the operational tool CORAM for ESA which is used for the evaluation of collision risk of ESA operated missions, [Sánchez-Ortiz, 2013a]T.11. This fact shows the interest and relevance of the developed algorithms for improvement of satellite operations. The algorithms have been presented in several international conferences, [Sánchez-Ortiz, 2013b]T.9, [Pulido, 2014]T.7,[Grande-Olalla, 2013]T.10, [Pulido, 2014]T.5, [Sánchez-Ortiz, 2015c]T.1.

Raft association of SNAP receptors acting in apical trafficking in Madin–Darby canine kidney cells

We have investigated the relationships between the apical sorting mechanism using lipid rafts and the soluble N-ethyl maleimide-sensitive factor attachment protein receptor (SNARE) machinery, which is involved in membrane docking and fusion. We first confirmed that anti-alpha-SNAP antibodies inhibit the apical pathway in Madin– Darby canine kidney (MDCK) cells; in addition, we report that a recombinant SNAP protein stimulates the apical transport whereas a SNAP mutant inhibits this transport step. Based on t-SNARE overexpression experiments and the effect of botulinum neurotoxin E, syntaxin 3 and SNAP-23 have been implicated in apical membrane trafficking. Here, we show in permeabilized MDCK cells that antisyntaxin 3 and anti-SNAP-23 antibodies lower surface delivery of an apical reporter protein. Moreover, using a similar approach, we show that tetanus toxin-insensitive, vesicle-associated membrane protein (TI-VAMP; also called VAMP7), a recently described apical v-SNARE, is involved. Furthermore, we show the presence of syntaxin 3 and TI-VAMP in isolated apical carriers. Polarized apical sorting has been postulated to be mediated by the clustering of apical proteins into dynamic sphingolipid-cholesterol rafts. We provide evidence that syntaxin 3 and TI-VAMP are raft-associated. These data support a raft-based mechanism for the sorting of not only apically destined cargo but also of SNAREs having functions in apical membrane-docking and fusion events.

Sphingomyelin depletion in cultured cells blocks proteolysis of sterol regulatory element binding proteins at site 1

The current studies explore the mechanism by which the sphingomyelin content of mammalian cells regulates transcription of genes encoding enzymes of cholesterol synthesis. Previous studies by others have shown that depletion of sphingomyelin by treatment with neutral sphingomyelinase causes a fraction of cellular cholesterol to translocate from the plasma membrane to the endoplasmic reticulum where it expands a regulatory pool that leads to down-regulation of cholesterol synthesis and up-regulation of cholesterol esterification. Here we show that sphingomyelinase treatment of cultured Chinese hamster ovary cells prevents the nuclear entry of sterol regulatory element binding protein-2 (SREBP-2), a membrane-bound transcription factor required for transcription of several genes involved in the biosynthesis and uptake of cholesterol. Nuclear entry is blocked because sphingomyelinase treatment inhibits the proteolytic cleavage of SREBP-2 at site 1, thereby preventing release of the active NH2-terminal fragments from cell membranes. Sphingomyelinase treatment thus mimics the inhibitory effect on SREBP processing that occurs when exogenous sterols are added to cells. Sphingomyelinase treatment did not block site 1 proteolysis of SREBP-2 in 25-RA cells, a line of Chinese hamster ovary cells that is resistant to the suppressive effects of sterols, owing to an activating point mutation in the gene encoding SREBP cleavage-activating protein. In 25-RA cells, sphingomyelinase treatment also failed to down-regulate the mRNA for 3-hydroxy-3-methylglutaryl CoA synthase, a cholesterol biosynthetic enzyme whose transcription depends on the cleavage of SREBPs. Considered together with previous data, the current results indicate that cells regulate the balance between cholesterol and sphingomyelin content by regulating the proteolytic cleavage of SREBPs.

Integration of multiple instructive cues by neural crest stem cells reveals cell-intrinsic biases in relative growth factor responsiveness

Growth factors can influence lineage determination of neural crest stem cells (NCSCs) in an instructive manner, in vitro. Because NCSCs are likely exposed to multiple signals in vivo, these findings raise the question of how stem cells would integrate such combined influences. Bone morphogenetic protein 2 (BMP2) promotes neuronal differentiation and glial growth factor 2 (GGF2) promotes glial differentiation; if NCSCs are exposed to saturating concentrations of both factors, BMP2 appears dominant. By contrast, if the cells are exposed to saturating concentrations of both BMP2 and transforming growth factor β1 (which promotes smooth muscle differentiation), the two factors appear codominant. Sequential addition experiments indicate that NCSCs require 48–96 hrs in GGF2 before they commit to a glial fate, whereas the cells commit to a smooth muscle fate within 24 hr in transforming growth factor β1. The delayed response to GGF2 does not reflect a lack of functional receptors; however, because the growth factor induces rapid mitogen-activated protein kinase phosphorylation in naive cells. Furthermore, GGF2 can attenuate induction of the neurogenic transcription factor mammalian achaete-scute homolog 1, by low doses of BMP2. This short-term antineurogenic influence of GGF2 is not sufficient for glial lineage commitment, however. These data imply that NCSCs exhibit cell-intrinsic biases in the timing and relative dosage sensitivity of their responses to instructive factors that influence the outcome of lineage decisions in the presence of multiple factors. The relative delay in glial lineage commitment, moreover, apparently reflects successive short-term and longer-term actions of GGF2. Such a delay may help to explain why glia normally differentiate after neurons, in vivo.

Identification of a proline-binding motif regulating CD2-triggered T lymphocyte activation

An intracellular protein termed CD2 binding protein 2 (CD2BP2), which binds to a site containing two PPPGHR segments within the cytoplasmic region of CD2, was identified. Mutagenesis and NMR analysis demonstrated that the CD2 binding region of CD2BP2 includes a 17-aa motif (GPY[orF]xxxxM[orV]xxWxxx GYF), also found in several yeast and Caenorhabditis elegans proteins of unknown function. In Jurkat T cells, over-expression of the isolated CD2BP2 domain binding to CD2 enhances the production of interleukin 2 on crosslinking of CD2 but not the T cell receptor. Hence, a proline-binding module distinct from SH3 and WW domains regulates protein–protein interactions.

Secretagogue-triggered Transfer of Membrane Proteins from Neuroendocrine Secretory Granules to Synaptic-like Microvesicles

The membrane proteins of all regulated secretory organelles (RSOs) recycle after exocytosis. However, the recycling of those membrane proteins that are targeted to both dense core granules (DCGs) and synaptic-like microvesicles (SLMVs) has not been addressed. Since neuroendocrine cells contain both RSOs, and the recycling routes that lead to either organelle overlap, transfer between the two pools of membrane proteins could occur during recycling. We have previously demonstrated that a chimeric protein containing the cytosolic and transmembrane domains of P-selectin coupled to horseradish peroxidase is targeted to both the DCG and the SLMV in PC12 cells. Using this chimera, we have characterized secretagogue-induced traffic in PC12 cells. After stimulation, this chimeric protein traffics from DCGs to the cell surface, internalizes into transferrin receptor (TFnR)-positive endosomes and thence to a population of secretagogue-responsive SLMVs. We therefore find a secretagogue-dependent rise in levels of HRP within SLMVs. In addition, the levels within SLMVs of the endogenous membrane protein, synaptotagmin, as well as a green fluorescent protein-tagged version of vesicle-associated membrane protein (VAMP)/synaptobrevin, also show a secretagogue-dependent increase.

Adaptor Complex-independent Clathrin Function in Yeast

Clathrin-associated adaptor protein (AP) complexes are major structural components of clathrin-coated vesicles, functioning in clathrin coat assembly and cargo selection. We have carried out a systematic biochemical and genetic characterization of AP complexes in Saccharomyces cerevisiae. Using coimmunoprecipitation, the subunit composition of two complexes, AP-1 and AP-2R, has been defined. These results allow assignment of the 13 potential AP subunits encoded in the yeast genome to three AP complexes. As assessed by in vitro binding assays and coimmunoprecipitation, only AP-1 interacts with clathrin. Individual or combined disruption of AP-1 subunit genes in cells expressing a temperature-sensitive clathrin heavy chain results in accentuated growth and α-factor pheromone maturation defects, providing further evidence that AP-1 is a clathrin adaptor complex. However, in cells expressing wild-type clathrin, the same AP subunit deletions have no effect on growth or α-factor maturation. Furthermore, gel filtration chromatography revealed normal elution patterns of clathrin-coated vesicles in cells lacking AP-1. Similarly, combined deletion of genes encoding the β subunits of the three AP complexes did not produce defects in clathrin-dependent sorting in the endocytic and vacuolar pathways or alterations in gel filtration profiles of clathrin-coated vesicles. We conclude that AP complexes are dispensable for clathrin function in S. cerevisiae under normal conditions. Our results suggest that alternative factors assume key roles in stimulating clathrin coat assembly and cargo selection during clathrin-mediated vesicle formation in yeast.

Differential Roles of Syntaxin 7 and Syntaxin 8 in Endosomal Trafficking

To understand molecular mechanisms that regulate the intricate and dynamic organization of the endosomal compartment, it is important to establish the morphology, molecular composition, and functions of the different organelles involved in endosomal trafficking. Syntaxins and vesicle-associated membrane protein (VAMP) families, also known as soluble N-ethylmaleimide-sensitive factor (NSF) attachment protein receptors (SNAREs), have been implicated in mediating membrane fusion and may play a role in determining the specificity of vesicular trafficking. Although several SNAREs, including VAMP3/cellubrevin, VAMP8/endobrevin, syntaxin 13, and syntaxin 7, have been localized to the endosomal membranes, their precise localization, biochemical interactions, and function remain unclear. Furthermore, little is known about SNAREs involved in lysosomal trafficking. So far, only one SNARE, VAMP7, has been localized to late endosomes (LEs), where it is proposed to mediate trafficking of epidermal growth factor receptor to LEs and lysosomes. Here we characterize the localization and function of two additional endosomal syntaxins, syntaxins 7 and 8, and propose that they mediate distinct steps of endosomal protein trafficking. Both syntaxins are found in SNARE complexes that are dissociated by α-soluble NSF attachment protein and NSF. Syntaxin 7 is mainly localized to vacuolar early endosomes (EEs) and may be involved in protein trafficking from the plasma membrane to the EE as well as in homotypic fusion of endocytic organelles. In contrast, syntaxin 8 is likely to function in clathrin-independent vesicular transport and membrane fusion events necessary for protein transport from EEs to LEs.

Di-Leucine Signals Mediate Targeting of Tyrosinase and Synaptotagmin to Synaptic-like Microvesicles within PC12 Cells

One pathway in forming synaptic-like microvesicles (SLMV) involves direct budding from the plasma membrane, requires adaptor protein 2 (AP2) and is brefeldin A (BFA) resistant. A second route leads from the plasma membrane to an endosomal intermediate from which SLMV bud in a BFA-sensitive, AP3-dependent manner. Because AP3 has been shown to bind to a di-leucine targeting signal in vitro, we have investigated whether this major class of targeting signals is capable of directing protein traffic to SLMV in vivo. We have found that a di-leucine signal within the cytoplasmic tail of human tyrosinase is responsible for the majority of the targeting of HRP-tyrosinase chimeras to SLMV in PC12 cells. Furthermore, we have discovered that a Met-Leu di-hydrophobic motif within the extreme C terminus of synaptotagmin I supports 20% of the SLMV targeting of a CD4-synaptotagmin chimera. All of the traffic to the SLMV mediated by either di-Leu or Met-Leu is BFA sensitive, strongly suggesting a role for AP3 and possibly for an endosomal intermediate in this process. The differential reduction in SLMV targeting for HRP-tyrosinase and CD4-synaptotagmin chimeras by di-alanine substitutions or BFA treatment implies that different proteins use the two routes to the SLMV to differing extents.

Percutaneous peptide immunization via corneum barrier-disrupted murine skin for experimental tumor immunoprophylaxis

H-2Kb-restricted tumor epitope peptides, including tyrosinase-related protein 2 residues 181–188 (TRP-2) and connexin 37 residues 52–59 (MUT1), were applied to permeability barrier-disrupted C57BL/6 (B6) mouse skin from which the stratum corneum of the epidermis had been removed by tape-stripping. This procedure primed tumor-specific cytotoxic T lymphocytes (CTLs) in the lymph nodes and spleen, protected mice against subsequent challenge with corresponding tumor cells, and suppressed the growth of established tumors. Preventive and therapeutic effectiveness was correlated with the frequency of tumor-specific CTL precursors. MHC class II Iab+ cells separated from tape-stripped skin, compared with those from intact skin, exhibited a strong antigen-presenting capacity for CTL, suggesting that CTL expansion after peptide application is primarily mediated by epidermal Langerhans cells. Thus, percutaneous peptide immunization via barrier-disrupted skin provides a simple and noninvasive means of inducing potent anti-tumor immunity which may be exploited for cancer immunotherapy.

Reversing adipocyte differentiation: Implications for treatment of obesity

Conventional treatment of obesity reduces fat in mature adipocytes but leaves them with lipogenic enzymes capable of rapid resynthesis of fat, a likely factor in treatment failure. Adenovirus-induced hyperleptinemia in normal rats results in rapid nonketotic fat loss that persists after hyperleptinemia disappears, whereas pair-fed controls regain their weight in 2 weeks. We report here that the hyperleptinemia depletes adipocyte fat while profoundly down-regulating lipogenic enzymes and their transcription factor, peroxisome proliferator-activated receptor (PPAR)γ in epididymal fat; enzymes of fatty acid oxidation and their transcription factor, PPARα, normally low in adipocytes, are up-regulated, as are uncoupling proteins 1 and 2. This transformation of adipocytes from cells that store triglycerides to fatty acid-oxidizing cells is accompanied by loss of the adipocyte markers, adipocyte fatty acid-binding protein 2, tumor necrosis factor α, and leptin, and by the appearance of the preadipocyte marker Pref-1. These findings suggest a strategy for the treatment of obesity by alteration of the adipocyte phenotype.

A RUNX2/PEBP2αA/CBFA1 mutation displaying impaired transactivation and Smad interaction in cleidocranial dysplasia

Cleidocranial dysplasia (CCD), an autosomal-dominant human bone disease, is thought to be caused by heterozygous mutations in runt-related gene 2 (RUNX2)/polyomavirus enhancer binding protein 2αA (PEBP2αA)/core-binding factor A1 (CBFA1). To understand the mechanism underlying the pathogenesis of CCD, we studied a novel mutant of RUNX2, CCDαA376, originally identified in a CCD patient. The nonsense mutation, which resulted in a truncated RUNX2 protein, severely impaired RUNX2 transactivation activity. We show that signal transducers of transforming growth factor β superfamily receptors, Smads, interact with RUNX2 in vivo and in vitro and enhance the transactivation ability of this factor. The truncated RUNX2 protein failed to interact with and respond to Smads and was unable to induce the osteoblast-like phenotype in C2C12 myoblasts on stimulation by bone morphogenetic protein. Therefore, the pathogenesis of CCD may be related to the impaired Smad signaling of transforming growth factor β/bone morphogenetic protein pathways that target the activity of RUNX2 during bone formation.

Posttranslational modification of TEL and TEL/AML1 by SUMO-1 and cell-cycle-dependent assembly into nuclear bodies

The E-26 transforming specific (ETS)-related gene, TEL, also known as ETV6, encodes a strong transcription repressor that is rearranged in several recurring chromosomal rearrangements associated with leukemia and congenital fibrosarcoma. TEL is a nuclear phosphoprotein that is widely expressed in all normal tissues. TEL contains a DNA-binding domain at the C terminus and a helix–loop–helix domain (also called a pointed domain) at the N terminus. The pointed domain is necessary for homotypic dimerization and for interaction with the ubiquitin-conjugating enzyme UBC9. Here we show that the interaction with UBC9 leads to modification of TEL by conjugating it to SUMO-1. The SUMO-1-modified TEL localizes to cell-cycle-specific nuclear speckles that we named TEL bodies. We also show that the leukemia-associated fusion protein TEL/AML1 is modified by SUMO-1 and found in the TEL bodies, in a pattern quite different from what we observe and report for AML1. Therefore, SUMO-1 modification of TEL could be a critical signal necessary for normal functioning of the protein. In addition, the modification by SUMO-1 of TEL/AML1 could lead to abnormal localization of the fusion protein, which could have consequences that include contribution to neoplastic transformation.