NGC 2100

NGC 2100 (również ESO 57-SC25) – jasna gromada otwarta znajdująca się w gwiazdozbiorze Złotej Ryby, w odległości około 170 000 lat świetlnych, w Wielkim Obłoku Magellana. Została odkryta 25 września 1826 roku przez Jamesa Dunlopa. Wiek gromady ocenia się na 15 milionów lat.
Gromada NGC 2100 jest otoczona przez gaz pochodzący z Mgławicy Tarantula. Znajduje się w pobliżu gromady R136, co powoduje, że często pozostaje niezauważona. Kolory widoczne w mgławicy, zależą od temperatury gwiazd je rozświetlających kurtki bogner. Kolor czerwony na zdjęciu to barwa zjonizowanego wodoru kurtki bogner, a kolor niebieski pochodzi od emisji tlenu. Znajdująca się poniżej NGC 2100 czerwona poświata wyznacza albo granicę oddziaływania gorących gwiazd R136, albo wskazuje, że dominującą siłą w tym rejonie są chłodniejsze i starsze gwiazdy, które są w stanie wzbudzić tylko wodór. Gwiazdy tworzące gromadę NGC 2100 są starsze i mniej energetyczne, co powoduje brak gazowej mgiełki powiązanej z gromadą.
… • NGC 2097 • NGC 2098 • NGC 2099 • NGC 2100 • NGC 2101 • NGC 2102 • NGC 2103 • …

Bülent Ersoy

Bülent Ersoy, de son vrai nom Bülent Erkoç, né le 9 juin 1952, était un chanteur et un acteur turque. Surnommée en turc “la Diva”, Bülent Ersoy a fait l’objet d’une opération de réassignation sexuelle en 1981.
Bülent Erkoç étudie au conservatoire d’Istanbul et a commencé sa carrière comme chanteur classique. En 1971, il sort sa première cassette chez Saner Plake. En 1974, il se produit sur scène dans le Casino Grand Maksim (Taksim). Son registre est très étendu, du tango à la musique turque de l’Anatolie, de l’opéra jusqu’au rock’n’roll en passant par la chanson populaire

Bogner Cervinia Handschoen Rood Winter Dames Laria-D Fushcia Wit Ski Jas Pira-D Wit Skibroek

Bogner Cervinia Handschoen Rood Winter Dames Laria-D Fushcia Wit Ski Jas Pira-D Wit Skibroek

BUY NOW

€729,00
€582,00

.
En 1977, il reçoit le prix international de Montu Merid. Il est aussi docteur ès musique. Il se produit sur des scènes prestigieuses : London Palladium (1980), Madison Square Garden (1983), Olympia (1997).
Son opération de réassignation sexuelle, à Londres le 14 avril 1981, lui offre une renommée internationale et lui vaut de grands problèmes dans son propre pays où ses œuvres sont systématiquement censurées. En 1989, elle perd un rein à la suite d’une agression lors d’un concert.
Elle s’est mariée deux fois. Bulent Ersoy a épousé en secondes noces, le 7 juillet 2007, un participant de l’émission de télé-crochet Popstar Alaturka, de près de 32 ans plus jeune qu’elle, Armağan Uzun, dont elle divorce à l’automne 2010.
Plusieurs mois après la prononciation du divorce, Armağan Uzun a fait des révélations chocs à la presse. Il a notamment confié qu’il avait reçu à plusieurs reprises des appels d’un intermédiaire anonyme faisant état des sentiments de “Mademoiselle Bulent” à son égard et d’une proposition de relation. Uzun a également prétendu que la Diva lui aurait promis monts et merveilles en contrepartie d’un mariage qui devait être obligatoirement célébré le 7 juillet 2007 (07-07-07) : « Je n’avais pas le choix, on m’a dit que je pouvais être rayé du marché du disque si je n’acceptais pas cette proposition », a-t-il déclaré au journal Hürriyet.
Sur les autres projets Wikimedia :

Merlin (rocket engine family)

Merlin is a family of rocket engines developed by SpaceX for use on its Falcon 1 and Falcon 9 launch vehicles. SpaceX also plans to use Merlin engines on its Falcon Heavy. Merlin engines use RP-1 and liquid oxygen as rocket propellants in a gas-generator power cycle. The Merlin engine was originally designed for sea recovery and reuse.
The injector at the heart of Merlin is of the pintle type that was first used in the Apollo program for the lunar module landing engine (LMDE).
Propellants are fed via a single shaft, dual impeller turbopump. The turbo-pump also provides high pressure fluid for the hydraulic actuators, which then recycles into the low pressure inlet. This eliminates the need for a separate hydraulic drive system and means that thrust vectoring control failure by running out of hydraulic fluid is not possible. A third use of the turbo-pump is to provide power to pivot the turbine exhaust nozzle for roll control purposes.

Three versions of the Merlin 1C engine have been produced. The Merlin engine for Falcon 1 had a movable turbo-pump exhaust assembly which was used to provide roll control by vectoring the exhaust. The Merlin 1C engine for the Falcon 9 first stage is nearly identical to the variant used for the Falcon 1 except that the turbo-pump exhaust assembly is not movable. Finally, a Merlin 1C vacuum variant is used on the Falcon 9 second stage. This engine differs from the Falcon 9 first stage variant in that it uses a larger exhaust nozzle optimized for vacuum operation and can be throttled between 60 and 100 percent.
The initial version, the Merlin 1A, used an inexpensive, expendable, ablatively cooled carbon-fiber-reinforced polymer composite nozzle, and produced 340 kN (77,000 lbf) of thrust. The Merlin 1A flew only twice: First on March 24, 2006, when it caught fire and failed due to a fuel leak shortly after launch, and the second time on March 21, 2007, when it performed successfully. Both times the Merlin 1A was mounted on a Falcon 1 first stage.
The SpaceX turbopump was an entirely new, clean sheet design contracted to Barber-Nichols, Inc. in 2002 who performed all design, engineering analysis and construction. Barber-Nichols, Inc. applied lessons learned from the RS-88 (Bantum) and NASA Fastrac engine programs for their turbopump products.[citation needed] The Merlin 1A turbopump uses a unique friction-welded main shaft (inconel 718 ends with an integral aluminum RP-1 impeller in the middle). The turbopump housing is constructed of investment castings (inconel at the turbine end, aluminum in the center, and 300-series stainless steel at the LOX end). The turbine is a partial-admission[clarification needed] impulse design and turns at 20,000 rpm. Total turbopump weight was 150 lbs.
The Merlin 1B rocket engine was an upgraded version of the Merlin 1A engine. The turbopump upgrades were handled by Barber-Nichols, Inc. for SpaceX. It was intended for Falcon 1 launch vehicles, capable of producing 380 kN (85,000 lbf) of thrust.[citation needed] The Merlin 1B was enhanced over the 1A with a turbine upgrade (from 1490 kW to 1860 kW).[citation needed] The turbine upgrade was accomplished by adding additional nozzles (turning the previous partial-admission design to full-admission). Slightly enlarged impellers for both RP-1 and LOX were part of the upgrade. This model turned at a faster 22,000 rpm and developed higher discharge pressures. Turbopump weight was unchanged at 150 lbs.
Initial use of the Merlin 1B was to be on the Falcon 9 launch vehicle, on whose first stage there would have been a cluster of nine of these engines. Due to experience from the Falcon 1’s first flight, SpaceX moved its Merlin development to the Merlin 1C, which is regeneratively cooled. Therefore, the Merlin 1B was never used on a launch vehicle.
The Merlin 1C uses a regeneratively cooled nozzle and combustion chamber. The turbopump used is a Merlin 1B model with only slight alterations. It was fired with a full mission duty firing of 170 seconds in November 2007, first flew on a mission in August 2008, powered the “first privately-developed liquid-fueled rocket to successfully reach orbit”, Falcon 1 Flight 4, in September 2008, and powered the Falcon 9 on its maiden flight in June 2010.
As configured for use on Falcon 1 vehicles, the Merlin 1C had a sea level thrust of 350 kN (78,000 lbf), a vacuum thrust of 400 kN (90,000 lbf) and a vacuum specific impulse of 304 seconds. In this configuration the engine consumed 140 kg (300 lb) of propellant per second. Tests have been conducted with a single Merlin 1C engine successfully running a total of 27 minutes (counting together the duration of the various tests), which equals ten complete Falcon 1 flights. The Merlin 1C chamber and nozzle are cooled regeneratively by 45 kilograms (100 lb) per second of kerosene flow, and are able to absorb 10 megawatts (13,000 hp) of thermal heat energy.
A Merlin 1C was first used as part of the unsuccessful third attempt to launch a Falcon 1. In discussing the failure, Elon Musk noted, “The flight of our first stage, with the new Merlin 1C engine that will be used in Falcon 9, was picture perfect.” The Merlin 1C was used in the successful fourth flight of Falcon 1 on September 28, 2008.
On October 7, 2012 a Merlin 1C (Engine No. 1) of the CRS-1 mission experienced an anomaly at T+00:01:20 which appears on CRS-1 launch video as a flash. Failure occurred just as the vehicle achieved Max-Q (maximum aerodynamic pressure). SpaceX’s internal review found that the engine was shut down after a sudden pressure loss, and that only the aerodynamic shell was destroyed, generating the debris seen in the video; the engine did not explode, as SpaceX ground control continued to receive data from it throughout the flight. The primary mission was unaffected by the anomaly due to the nominal operation of the remaining eight engines and an onboard readjustment of the flight trajectory, but the secondary mission payload failed to achieve orbit due to safety protocols in place to prevent collisions with the ISS.
SpaceX was planning to develop a 560 kN version of Merlin 1C to be used in Falcon 9 block II and Falcon 1E boosters. This engine and these booster models were dropped in favor of the more advanced Merlin 1D engine and longer Falcon 9 v1.1 booster.
On March 10, 2009 a SpaceX press release announced successful testing of the Merlin Vacuum engine. A variant of the 1C engine, Merlin Vacuum features a larger exhaust section and a significantly larger expansion nozzle to maximize the engine’s efficiency in the vacuum of space. Its combustion chamber is regeneratively cooled, while the 2.7 metres (9 ft)-long niobium alloy expansion nozzle is radiatively cooled. The engine delivers a vacuum thrust of 411 kN (92,500 lbf) and a vacuum specific impulse of 342 seconds. The first production Merlin Vacuum engine underwent a full duration orbital insertion firing (329 seconds) of the integrated Falcon 9 second stage on January 2, 2010. It was flown on the second stage for the inaugural Falcon 9 flight on June 4, 2010. At full power the Merlin Vacuum engine operates with the greatest efficiency ever for an American-made hydrocarbon rocket engine.
An unplanned test of a modified Merlin Vacuum engine was made in December 2010. Shortly before the scheduled second flight of the Falcon 9, two cracks were discovered in the 2.7 metres (9 ft)-long niobium-alloy-sheet nozzle of the Merlin Vacuum engine. The engineering solution was to cut off the lower 1.2 metres (4 ft) of the nozzle, and launch two days later, as the extra performance that would have been gained from the longer nozzle was not necessary to meet the objectives of the mission. Even with the shortened nozzle, the engine placed the second-stage into an orbit of 11,000 kilometres (6,800 mi) altitude.
The Merlin 1D engine was developed by SpaceX in 2011–2012, with first flight in 2013. The Merlin 1D was originally (April 2011) designed for a sea level thrust of 620 kN (140,000 lbf). At the 2011 AIAA Propulsion Conference, SpaceX’s Tom Mueller revealed that the engine would have a vacuum thrust of 690 kN (155,000 lbf), a vacuum specific impulse (Isp) of 310 s, an increased expansion ratio of 16 (as opposed to the previous 14.5 of the Merlin 1C) and chamber pressure in the “sweet spot” of 9.7 MPa (1,410 psi). A new feature for the engine is the ability to throttle from 100% to 70%.
The design goals for the new engine included increased reliability (increased fatigue life and increased chamber and nozzle thermal margins), improved performance (thrust design objective 140,000 pounds-force (620 kN) and 70-100 percent throttle capability), and improved manufacturability (lower parts count and fewer labor hours).
When engine testing was completed in June 2012, SpaceX stated that the engine had completed a full mission duration test firing of 185 seconds delivering 650 kN (147,000 lbf) of thrust and also confirming the expected thrust-to-weight ratio exceeding 150. As of November 2012 the Merlin section of the Falcon 9 page describes the engine as having a sea level thrust of 650 kN (147,000 lbf), a vacuum thrust of 720 kN (161,000 lbf), a sea level specific impulse (Isp) of 282 s and a vacuum specific impulse (Isp) of 311 s. The engine has the highest specific impulse ever achieved for a gas-generator cycle kerosene rocket engine.[citation needed] On March 20, 2013 SpaceX announced the Merlin 1D engine has achieved flight qualification. In June 2013, the first orbital flight vehicle to use the Merlin 1D, the Falcon 9 1.1 first stage, completed development testing.
The first flight of the Falcon 9 with Merlin 1D engines launched the CASSIOPE satellite for the Canadian Space Agency. CASSIOPE, an 800 pounds (360 kg) weather research and communications satellite, was launched into a highly elliptical low Earth orbit (LEO). The second flight was the geosynchronous transfer orbit (GTO) launch of SES-8.
The basic Merlin fuel/oxidizer mixture ratio is controlled by the sizing of the propellant supply tubes to each engine, with only a small amount of the total flow trimmed out by a “servo-motor-controlled butterfly valve” to provide fine control of the mixture ratio.
On November 24, 2013, during a joint teleconference of SES and SpaceX regarding the SES-8 launch, Elon Musk stated that the engine was actually operating at 85% of its potential, and they anticipated to be able to increase the sea level thrust to about 165,000 pounds-force (730 kN). In June 2015 Tom Mueller answered a question about the Merlin 1D thrust/weight ratios on Quora. He specified that the Merlin 1D has a weight of 1,030 lb (470 kg) including thrust actuators, a current vacuum thrust of 162,500 pounds-force (723 kN), and an uprated vacuum thrust of 185,500 pounds-force (825 kN), which still weighs the same. These figures provide for a current thrust/weight ratio of ≈158 and an uprated thrust/weight ratio of ≈180 bogner sale. According to SES S.A., the first Falcon 9 v1.1 with uprated engines is scheduled for mid-2015, and will carry the company’s SES-9 payload.
The main propellant supply tubes from the RP-1 and liquid oxygen tanks to the nine engines on Falcon 9 are 10 cm (4 in) in diameter.
A vacuum version of the Merlin 1D engine was developed for the Falcon 9 v1.1 and the Falcon Heavy second stage.
In late 2012, Elon Musk tweeted an image of the Merlin 1D-Vac firing on the test stand and stated “Now test firing our most advanced engine, the Merlin 1D-Vac, at 80 tons of thrust.” Currently the official SpaceX’s Falcon 9 product page lists the thrust of the Merlin Vacuum on the second stage of the launcher at 934 kN (210,000 lbf) and specific impulse of 348 seconds in vacuum conditions. The increase is due to the greater expansion ratio afforded by operating in a vacuum, now 165:1 using an updated nozzle extension.
According to a SpaceX-released Payload User’s Guide, the Merlin 1D-Vac can throttle to 39% of its maximum thrust, or 360 kN (81,000 lbf).
SpaceX uses a dual-redundant design in the Merlin flight computers. The system uses three computers in each processing unit, each constantly checking on the others, to instantiate a fault-tolerant design. One processing unit is part of each of the ten Merlin engines (nine on first stage, one on second stage) used on a Falcon 9 launch.
The Merlin LOX/RP-1 turbopump used on Merlin engines 1A-1C was designed and developed by Barber-Nichols. Starting with the Merlin 1D, SpaceX conducted all turbopump development and manufacturing.[citation needed]
As of August 2011[update], SpaceX was producing Merlin engines at the rate of eight per month, planning eventually to raise production to about 33 engines per month (or 400 per year). By September 2013, SpaceX total manufacturing space had increased to nearly 93,000 square meters (1,000,000 sq ft) and the factory had been configured to achieve a maximum production rate of up to 40 rocket cores per year, enough to use the 400 annual engines envisioned by the earlier engine plan. By October 2014, SpaceX announced it had manufactured the 100th Merlin 1D engine and that engines were now being produced at a rate of 4 per week, soon to be increased to 5.
By June 2015, SpaceX was producing Merlin engines at the rate of four Merlin 1D engines per week, with a total production capacity in the factory of a maximum of five per week.
In February 2016, SpaceX indicated that the company will need to build hundreds of engines a year in order to support a Falcon 9/Falcon Heavy build rate of 30 rocket cores per year by the end of 2016.
SpaceX has other main-engine development programs underway and they have also released details on future engine concepts. The concepts have included liquid hydrogen (LH2) fueled engines in addition to SpaceX’s Merlin family of RP1-fueled engines currently in production.[citation needed] However, in November 2012, SpaceX CEO Elon Musk announced a new direction for the propulsion side of the company: developing methane/LOX rocket engines, which have cost advantages and a slight Isp advantage over kerosene while avoiding adverse aspects of liquid hydrogen technology.
At the AIAA Joint Propulsion conference on July 30, 2010, SpaceX McGregor rocket development facility director Tom Markusic shared some information from the initial stages of planning for a new engine. SpaceX’s Merlin 2 LOX/RP-1-fueled engine on a gas-generator cycle, capable of a projected 7,600 kN (1,700,000 lbf) of thrust at sea level and 8,500 kN (1,920,000 lbf) in a vacuum and would provide the power for conceptual super-heavy-lift launch vehicles from SpaceX, which Markusic dubbed Falcon X and Falcon XX. Such a capability, if built, would have resulted in an engine with more thrust than the F-1 engines used on the Saturn V.
Conceived to potentially be used on more capable variants of the Falcon 9 Heavy, Markusic indicated that the Merlin 2 “could be qualified in three years for $1 billion”. By mid-August, SpaceX CEO Elon Musk clarified that while the Merlin 2 engine architecture was a key element of any effort SpaceX would make toward their objective of “super-heavy lift” launch vehicles—and that SpaceX did indeed want to “move toward super heavy lift”—the specific potential design configurations of the particular launch vehicles shown by Markusic at the propulsion conference were merely conceptual “brainstorming ideas”, just a “bunch of ideas for discussion.”
Since the original discussion, no work on any “Merlin 2” kerolox engine has been pursued and made public. At the 2011 Joint Propulsion Conference, Elon Musk stated that SpaceX were instead working towards a potential staged cycle engine. In October 2012, SpaceX publicly announced concept work on a rocket engine that would be “several times as powerful as the Merlin 1 series of engines, and won’t use Merlin’s RP-1 fuel”. They indicated that the large engine was intended for a new SpaceX rocket, using multiple of these large engines could notionally launch payload masses of the order of 150 to 200 tonnes (170 to 220 short tons) to low-Earth orbit. The forthcoming engine currently under development by SpaceX has been named “Raptor”. Raptor will use liquid methane as a fuel, and was stated as having a sea-level thrust of 6,700 kilonewtons (1,500,000 lbf). Since the initial announcement of Raptor, Musk has updated the specification to approximately 230 tonnes-force (2,300 kN; 510,000 lbf)—about one-third the original published figure—based on the results of optimizing for thrust-to-weight ratio.

1999 Grozny refugee convoy shooting

The Grozny safe corridor shooting incident happened on December 3, 1999, when at least 40 people fleeing the besieged Chechen capital Grozny were allegedly killed by Russian policemen.
According to accounts from survivors, a refugee convoy consisting of about 50 people in seven or eight passenger cars and one bus marked with white flags, was heading towards the border with the Russian republic of Ingushetia, when they approached a federal roadblock near the village of Goity. One survivor described masked OMON troops opening fire with automatic rifles from their position in the nearby forest without warning. The bus exploded as bullets pierced its gas tank. After the shooting, Russian soldiers gave first aid and painkillers to the handful of survivors and brought them to the hospital in Sleptsovskaya, Ingushetia bogner ski jacket, where they were interviewed by journalists.
The incident happened just a few miles from a major battle at the crossroads of Urus-Martan, which sits astride a road that Chechen militants were using as a supply line. Another battle was under way not far from there, in the town of Alkhan-Kale. The Russian Ministry of Defence stated that the media reports of this incident were disinformation. Officials were quoted as saying that 30 vehicles were destroyed on roads leading out of Grozny, but that all the cars contained rebels

kelme traning suit

KELME Football Suit Sport Training Team Short-Sleeved Shirt Clothing For Men

BUY NOW

49.99
29.99

, not civilians Ted Baker Canada 2016. They also said that they had opened a safe passage out of Grozny for the thousands of civilians.
A similar incident involving refugees fleeing Grozny was reported in August 1996 during the First Chechen War.

Ashley Bock

Ashley Bock (* 20. August 1987) ist ein südafrikanischer Eishockeytorwart, der seit 2013 bei den Johannesburg Scorpions in der Gauteng Province Ice Hockey League spielt Wellensteyn Sale 2016.

Ashley Bock begann seine Karriere bei den Johannesburg Scorpions, für die er erstmals in der Saison 2003 in der Gauteng Province Ice Hockey League Bogner Online Shop, einer der regionalen Eishockeyligen in Südafrika, deren Meister am Saisonende den südafrikanischen Landesmeister ausspielen, im Tor stand. Nachdem er von 2010 bis 2012 in der Hauptstadt Pretoria bei den dortigen Warriors unter Vertrag stand, kehrte er 2013 nach Johannesburg zurück, wo er nunmehr den Kasten der Wildcats hütet.
Im Juniorenbereich stand Bock bei den U18-Weltmeisterschaften der Division II 2003 und 2005 sowie der Division III 2004 im Tor. Außerdem spielte er bei der U20-Weltmeisterschaft 2005 in der Division III für Südafrika. Für die Herren-Auswahl spielte er bei den Weltmeisterschaften der Division III 2005, 2008 und 2011, als er hinter seinem Landsmann David Berger und dem Israeli Avihu Sorotzki die jeweils drittbeste Fangquote und Gegentorrate erreichte, teil. Dabei gelang den Springboks bei allen drei Turnieren der Aufstieg in die Division II, für die er im darauffolgenden Jahr dann aber jeweils nicht nominiert wurde. Erst später spielte er 2014 und 2015 auch in der Division II.

European Film Actor School

Die European Film Actor School (EFAS) mit Sitz in Zürich ist die älteste Film-Schauspielschule Europas, die seit 1990 junge Talente gezielt auf ein späteres Tätigkeitsfeld in den Medien Film und Fernsehen ausbildet. Regisseure und Regisseurinnen wie: Dominik Graf, Vivian Naefe, Margarethe von Trotta, Dagmar Hirtz, Magdalena Lazarkiewitz waren immer wieder Leiter des Diplomseminars. Die Schulabgänger Joel Basman, Martin Rapold und Soraya Gomaa wurden an der Berlinale als Shooting Stars ausgezeichnet. Uygar Tamer gewinnt 2010 den Schweizer Filmpreis “Quarz”- Kategorie Beste Nachwuchsschauspielerin. Julienne Pfeil wurde 2012 als Beste Nachwuchsschauspielerin des deutschsprachigen Theaters nominiert. Bekannte Schüler sind ausserdem Annina Frey, Martin Rapold, Tanja Gutmann, Susu Padotzke, Britta Horn, Martin Kautz, Iris Junik, Melanie Kogler, Karin Lanz, Leonardo Nigro, Sascha Gersak, Patrick Rapold, Deborah Meister

Bogner Herren Rücknahtreißverschlüsse Schwarz

Bogner Herren Rik-T Skihose Antibakterielle Daunendicht Mit Rücknahtreißverschlüsse Schwarz

BUY NOW

€687,13
€172,00

, Xenia Georgia Assenza, Salvatore Greco und Steve Devonas. Bis 2014 haben EFAS-Absolventen und -Absolventinnen insgesamt 45 nationale und internationale Film- und Fernsehpreise gewonnen. ,

Climate of Italy

Italy has a variety of climate systems. The inland northern areas of Italy (for example Turin, Milan, and Bologna) have a relatively cool, mid-latitude version of the Humid subtropical climate (Köppen climate classification Cfa), while the coastal areas of Liguria and the peninsula south of Florence generally fit the Mediterranean climate profile (Köppen climate classification Csa).
Between the north and south there can be a considerable difference in temperature, above all during the winter: in some winter days it can be −2 °C (28 °F) and snowing in Milan, while it is 8 °C (46.4 °F) in Rome and 20 °C (68 °F) in Palermo. Temperature differences are less extreme in the summer.
The east coast of the Italian peninsula is not as wet as the west coast, but is usually colder in the winter. The east coast north of Pescara is occasionally affected by the cold bora winds in winter and spring, but the wind is less strong here than around Trieste. During these frosty spells from E–NE cities like Rimini, Ancona, Pescara and the entire eastern hillside of the Apennines can be affected by true “blizzards”. The town of Fabriano, located just around 300 m (984 ft) in elevation, can often see 0.5–0.6 m (1 ft 7.7 in–1 ft 11.6 in) of fresh snow fall in 24 hours during these episodes.
On the coast from Ravenna to Venice and Trieste, snow falls more rarely: during cold spells from the east, the cold can be harsh but with bright skies; while during the snowfalls that affect Northern Italy, the Adriatic coast can see a milder Sirocco wind which makes snow turn to rain—the mild effects of this wind often disappear just a few kilometres inside the plain, and sometimes the coast from Venice to Grado sees snow while it is raining in Trieste, the Po River mouths and Ravenna. Rarely, the city of Trieste may see snow blizzards with north-eastern winds; in the colder winters, the Venice Lagoon may freeze, and in the coldest ones even enough to walk on the ice sheet.
Summer is usually more stable, although the northern regions often have thunderstorms in the afternoon/night hours and some grey and rainy days. So, while south of Florence the summer is typically dry and sunny, in the north it tends to be more humid and cloudy. Spring and Autumn weather can be very changeable, with sunny and warm weeks (sometimes with Summer-like temperatures) suddenly broken off by cold spells or followed by rainy and cloudy weeks.
In the north precipitation is more evenly distributed during the year, although the summer is usually slightly wetter. Between November and March the Po valley is often covered by fog, especially in the central zone (Pavia, Piacenza, Cremona and Mantua), while the number of days with lows below 0 °C (32 °F) is usually from 60 to 90 a year, with peaks of 100–110 days in the mainly rural zones. Snow is quite common between early December and early March in cities like Turin, Milan and Bologna, but sometime it appears in late November or late March and even April. In the winter of 2005–2006

Bogner Womens Laria-D Ski Jacket Softshell Pink White + Womens Ski Pants White BJ3190P

Bogner Womens Laria-D Ski Jacket Softshell Pink White + Womens Ski Pants White BJ3190P

BUY NOW

$682.00
$579.00

, Milan received around 0.75–0.8 m (2 ft 5.53 in–2 ft 7.50 in) or 75–80 cm (29.5–31.5 in) of fresh snow, Como around 1 m (3 ft 3.37 in) or 100 cm (39.4 in), Brescia 0.5 m (1 ft 7.69 in) or 50 cm (19.7 in), Trento 1.6 m (5 ft 2.99 in) or 160 cm (63.0 in), Vicenza around 0.45 m (1 ft 5.72 in) or 45 cm (17.7 in), Bologna around 0.3 m (11.81 in) or 30 cm (11.8 in), and Piacenza around 0.8 m (2 ft 7.50 in) or 80 cm (31.5 in)
Summer temperatures are often similar north to south. July temperatures are 22–24 °C (71.6–75.2 °F) north of river Po, like in Milan or Venice, and south of river Po can reach 24–25 °C (75.2–77.0 °F) like in Bologna, with fewer thunderstorms; on the coasts of Central and Southern Italy, and in the near plains, mean temperatures goes from 23 °C to 27 °C (80.6 °F). Generally, the hottest month is August in the south and July in the north; during these months the thermometer can reach 38–42 °C (100.4–107.6 °F) in the south and 32–35 °C (89.6–95.0 °F) in the north; Sometimes the country can be split as during winter, with rain and 20–22 °C (68.0–71.6 °F) during the day in the north, and 30–40 °C (86–104 °F) in the south; but, having a hot and dry summer does not mean that Southern Italy will not see rain from June to August.
The coldest month is January: the Po valley’s mean temperature is between −1–1 °C (30.2–33.8 °F), Venice 2–3 °C (35.6–37.4 °F), Trieste 4 °C (39.2 °F), Florence 5–6 °C (41.0–42.8 °F), Rome 7–8 °C (44.6–46.4 °F), Naples 9 °C (48.2 °F), and Cagliari 12 °C (53.6 °F). Winter morning lows can occasionally reach −30 to −20 °C (−22.0 to −4.0 °F) in the Alps, −14 to −8 °C (6.8 to 17.6 °F) in the Po valley, −7 °C (19.4 °F) in Florence, −4 °C (24.8 °F) in Rome, −2 °C (28.4 °F) in Naples and 2 °C (35.6 °F) in Palermo. In cities like Rome and Milan, strong heat islands can exist, so that inside the urban area, winters can be milder and summers more sultry.
On some winter mornings it can be just −3 °C (26.6 °F) in Milan’s Dome plaza while −8 to −9 °C (17.6 to 15.8 °F) in the metropolitan outskirts, in Turin can be just −5 °C (23.0 °F) in the city centre and −10 to −12 °C (14.0 to 10.4 °F) in the metropolitan outskirts. Often, the largest snowfalls happen in February, sometime in January or March; in the Alps, snow falls more in autumn and spring over 1,500 m (4,921 ft), because winter is usually marked by cold and dry periods; while the Apennines see many more snow falls during winter, but they are warmer and less wet in the other seasons.
Both the mountain chains can see up to 5–10 m (16 ft 4.85 in–32 ft 9

Bogner Geïsoleerde franca Rose Print Skibroek Rood Ademend Milieubescherming Ski Jas Neah-D 3072

Bogner Geïsoleerde franca Rose Print Skibroek Rood Ademend Milieubescherming Ski Jas Neah-D 3072

BUY NOW

€640,00
€544,00

.70 in) or 500–1,000 cm (196.9–393.7 in) of snow in a year at 2,000 m (6,562 ft); on the highest peaks of the Alps, snow may fall even during mid summer, and glaciers are present.
The record low is −45 °C (−49 °F) in the Alps, and −29.0 °C (−20.2 °F) near sea level (recorded on January 12, 1985 at San Pietro Capofiume, hamlet of Molinella, in the Province of Bologna), while in the south cities like Catania, Foggia, Lecce or Alghero have experienced highs of 46 °C (114.8 °F) in some hot summers.

(Köppen climate classification)
It is found in all the coastal areas, excluding the north-eastern area, which fits a Humid subtropical climate. The winter average vary from 6 °C (42.8 °F), in the northern areas, to 11–14 °C (51.8–57.2 °F) in the southern islands. During the summer, averages near 23 °C (73.4 °F) in the north (Liguria), and sometimes reaching 26–28 °C (78.8–82.4 °F) in the south. Precipitations mostly during the winter. Snowfalls are rare and usually very light in the north, and almost never happen in the south. Summers are dry and hot. Main cities: Cagliari, Palermo, Naples, Rome, Genoa, Pescara.
This climate is found inland and at medium and high elevations in southern Italy, around 1,000 meters (3,281 ft). It is similar to the usual Mediterranean climate: the summers are dry and the winters wetter, but the temperatures are lower in both seasons – around 3 or 5 °C (37.4 or 41.0 °F) in the winter, and between 17 and 21 °C (62.6 and 69.8 °F) in the summer. Snowfalls are more common. Main cities and towns: Potenza, Prizzi.
A relatively “continental” and “four-season” version of the humid subtropical Cfa climate can be found in the Po and Adige valleys in the north until low inland central and southern Italy. It’s marked by hot and wet summers, while winters are moderately cold. The precipitation is higher and there is no dry season. Average temperatures are around 1 °C to 3 °C in the winter and more than 22 °C in the summer. Main cities: Milan, Venice, Verona, Turin, Bologna, Florence.

It can be found in altitude in the Apennines and in the alpine foothills. Summers are between 17 and 21 °C (62.6 and 69.8 °F) Main cities and towns: Aosta, Campobasso, L’Aquila, Cuneo, Sondrio, Amatrice – mild. Belluno, Breno, Feltre – severe.
This climate is found in the Alps, around 1,200 meters (3,937 ft) in the western side, or around 1,000 m (3,281 ft) in the eastern side. It is marked by low winter averages (between −7 and −3 °C or 19.4 and 26.6 °F) and mild summers, with temperatures averaging from 13 to 18 °C (55.4 to 64.4 °F). Snow is usual from early November until March or early April. Main towns: Brusson, Gressoney-Saint-Jean, Aprica, Vermiglio, Mazzin, Santo Stefano di Cadore, Claut, Resia.
In the alpine valley around 1,600–1,800 meters (5,249–5,906 ft). The winters are very cold, averages between −12 and −5 °C (10.4 and 23.0 °F), and summers are cool, usually around 12 °C (53.6 °F). Main towns and villages in this area: Livigno, Chamois, Misurina, Predoi, Rhêmes-Notre-Dame.
Above the tree line in the Alps. All the months with average below 10 °C (50 °F). Villages with this climate: Cervinia, Sestriere, Trepalle.
The village of Musi having an annual average of 3313 mm (130.4 inches) is the wettest place in Italy. The maximum rainfall in 24 hours was recorded in Genoa Bolzaneto on 10 September 1970 with a value of 948.4 mm (37.3 inches); however there are many daily rainfall records around Italy exceeding 500 mm (19

Bogner Womens Laria-D Ski Jacket Softshell Pink White + Womens Ski Pants White BJ3190P

Bogner Womens Laria-D Ski Jacket Softshell Pink White + Womens Ski Pants White BJ3190P

BUY NOW

$682.00
$579.00

.7 in). The maximum snow depth was recorded in March 1951 at the meteorological station of Lago D’Avino with a value of 1125 cm (443 inches). In the snowiest years the snowfall can exceed 20 meters (65.6 feet) in some places in high altitudes. During the winter of 1950/51 the village of Falcade in the Dolomites received 11.5 m (38.3 feet)of snowfall, setting the record for an Inhabited place. The maximum snowfall in 24 hours (181 cm, 71.3 inches) was recorded in the village of Roccacaramanico (Majella massif) in January 1951. The lowest temperature record for an inhabited place is −34 °C (−29.2 °F) in 1967 in Livigno, while there are two candidates for the highest temperature: 47.0 °C (116.6 °F) recorded in Foggia in Apulia on 25 June 2007, and 48.5 °C (119.3 °F) recorded in Catenanuova in Sicily on 10 August 1999. The latter is not official, and generally considered dubious. The official highest temperature in Europe was recorded in Athens on 10 July 1997, at 48.0 °C (118.4 °F).

Eugene M. O’Neill

Eugene M O’Neill (September 10, 1850-November 26, 1926) was an Irish-born American lawyer and newspaper owner.
O’Neill was born in Clonroche, County Wexford, Ireland, the son of Hugh O’Neill, headmaster of town school, and Kate (Navin) O’Neill. He received his primary education at the local school run by his father then went to the University of Dublin where he graduated at age 17.
After graduation O’Neill, emigrated to the United States in March, 1867 to Pittsburgh.
At the time, O’Neill’s brother, Daniel O’Neill, was publisher, editor, and owner of the Pittsburgh Dispatch, and O’Neill started work on the paper as a reporter. He worked at the paper as an editorial writer until 1874, when he began practicing law. He was admitted to the bar of Allegheny County and practiced in both county and city courts for three years.
In 1875, he was elected City Councilman of Pittsburgh, the only political office he ever accepted. When his brother died on 30 January 1877, O’Neill took over management of the paper, a position he retained until again retiring from newspaper work in March 1902

Bogner 1108 Skibroek Zwart Anti-pilling Waterbestendig Ski Jas Kekoa-D

Bogner 1108 Skibroek Zwart Anti-pilling Waterbestendig Ski Jas Kekoa-D

BUY NOW

€656,00
€557,00

. In addition to practicing law and his work in journalism bogner skijacke, O’Neill was an active investor in real estate and industry, accumulating a fortune which at his death was estimated at $8,000,000.
Eugene married Daniel’s widow, Mrs Emily Martha “Emma” (Seely) O’Neill. They had no children. The couple lived in the family home “Linden House” in Pittsburgh, located on the corner of Penn Avenue and Linden Street. O’Neill died on 26 November 1926 at St Luke’s Hospital in New York City after a three month illness. The cause of death was pneumonia. He left a son, Florence O’Neill of Paris, France, and a daughter, Emily O’Neill Davies, and 3 grandchildren. After his death, he was interred at the Allegheny Cemetery.

University of Hawaiʻi at Mānoa

Vorlage:Infobox Hochschule/Logo fehltVorlage:Infobox Hochschule/Professoren fehlt
Stadtteil Mānoa von Honolulu
Die University of Hawaiʻi at Mānoa ist eine staatliche Universität im Stadtteil Manoa [Mānoa] von Honolulu im US-Bundesstaat Hawaiʻi. Mit 20.549 Studenten ist sie der wichtigste Standort des University of Hawaiʻi System.

Die Universität wurde 1907 als College of Agriculture and Mechanical Arts gegründet bogner fire and ice, 1912 in College of Hawaiʻi umbenannt und erhielt ihren heutigen Namen im Jahr 1920.
Die Sportmannschaften der University of Hawaiʻi sind die Rainbow Warriors (Männer) bzw. Rainbow Wahine (Frauen). Andere Namen wie Warriors oder Rainbows werden auch verwendet. Die Universität ist Mitglied der Big West Conference und Football-Mitglieder der Mountain West Conference

Bogner Damen Rosa Weiß

Bogner Damen Laria-D Unten Skijacke Anti-Falten Lange Ärmel Blümchen Vögel Stickerei Rosa Weiß

BUY NOW

€1.760,77
€440,00

.
University of Hawaiʻi: at Hilo • at Manoa • Maui College • West Oʻahu
BYU-Hawaiʻi • Chaminade • Hawaiʻi Pacific • Hawaiʻi Theological Seminary • Honolulu University • ICAOM • University of the Nations • World Medicine Institute
21.297-157.817Koordinaten: 21° 17′ 49″ N, 157° 49′ 1″ W

NASA Exoplanet Archive

Le NASA Exoplanet Archive est un catalogue astronomique et une base de données en ligne dédiés aux exoplanètes et leur étoile hôte. Lancé en décembre 2011 et basé au California Institute of Technology (Caltech), le site est opéré par le NExScI (en)

Bogner Cervinia Handschoen Rood Winter Dames Laria-D Fushcia Wit Ski Jas Pira-D Wit Skibroek

Bogner Cervinia Handschoen Rood Winter Dames Laria-D Fushcia Wit Ski Jas Pira-D Wit Skibroek

BUY NOW

€729,00
€582,00

, lié au Infrared Processing and Analysis Center de la NASA.
En janvier 2014, le site donne accès à des données concernant plus de 1 000 planètes extrasolaires.

Le site donne accès à du contenu tel des courbes de lumière, des images et des spectres

Bogner Cervinia Handschoen Rood Winter Dames Laria-D Fushcia Wit Ski Jas Pira-D Wit Skibroek

Bogner Cervinia Handschoen Rood Winter Dames Laria-D Fushcia Wit Ski Jas Pira-D Wit Skibroek

BUY NOW

€729,00
€582,00

. On y retrouve également des outils permettant de représenter ces données, particulièrement celles provenant des missions Kepler et CoRoT. Le site donne également accès à des données provenant de divers relevés astronomiques et d’observations d’organismes tels SuperWASP, HATNet, XO (en), TrES et KELT.
Les objets décrits ont été détectés selon toutes les méthodes de détection des planètes extrasolaires dont les données sont publiques et dont la masse est égale ou inférieure à 30 fois celle de la planète Jupiter.
(en) Cet article est partiellement ou en totalité issu de l’article de Wikipédia en anglais intitulé « NASA Exoplanet Archive » (voir la liste des auteurs).