XMM-Newton (Cross)-Calibration
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ESA Missions AO Analysis
ESA Announcements of Opportunity Outcome Analysis Arvind Parmar Head, Science Support Office ESA Directorate of Science With thanks to Kate Isaak, Erik Kuulkers, Göran Pilbratt and Norbert Schartel (Project Scientists) ESA UNCLASSIFIED - For Official Use The ESA Fleet for Astrophysics ESA UNCLASSIFIED - For Official Use Dual-Anonymous Proposal Reviews | STScI | 25/09/2019 | Slide 2 ESA Announcement of Observing Opportunities Ø Observing time AOs are normally only used for ESA’s observatory missions – the targets/observing strategies for the other missions are generally the responsibility of the Science Teams. Ø ESA does not provide funding to successful proposers. Ø Results for ESA-led missions with recent AOs presented: • XMM-Newton • INTEGRAL • Herschel Ø Gender information was not requested in the AOs. It has been ”manually” derived by the project scientists and SOC staff. ESA UNCLASSIFIED - For Official Use Dual-Anonymous Proposal Reviews | STScI | 25/09/2019 | Slide 3 XMM-Newton – ESA’s Large X-ray Observatory ESA UNCLASSIFIED - For Official Use Dual-Anonymous Proposal Reviews | STScI | 25/09/2019 | Slide 4 XMM-Newton Ø ESA’s second X-ray observatory. Launched in 1999 with annual calls for observing proposals. Operational. Ø Typically 500 proposals per XMM-Newton Call with an over-subscription in observing time of 5-7. Total of 9233 proposals. Ø The TAC typically consists of 70 scientists divided into 13 panels with an overall TAC chair. Ø Output is >6000 refereed papers in total, >300 per year ESA UNCLASSIFIED - For Official Use -
Two Fundamental Theorems About the Definite Integral
Two Fundamental Theorems about the Definite Integral These lecture notes develop the theorem Stewart calls The Fundamental Theorem of Calculus in section 5.3. The approach I use is slightly different than that used by Stewart, but is based on the same fundamental ideas. 1 The definite integral Recall that the expression b f(x) dx ∫a is called the definite integral of f(x) over the interval [a,b] and stands for the area underneath the curve y = f(x) over the interval [a,b] (with the understanding that areas above the x-axis are considered positive and the areas beneath the axis are considered negative). In today's lecture I am going to prove an important connection between the definite integral and the derivative and use that connection to compute the definite integral. The result that I am eventually going to prove sits at the end of a chain of earlier definitions and intermediate results. 2 Some important facts about continuous functions The first intermediate result we are going to have to prove along the way depends on some definitions and theorems concerning continuous functions. Here are those definitions and theorems. The definition of continuity A function f(x) is continuous at a point x = a if the following hold 1. f(a) exists 2. lim f(x) exists xœa 3. lim f(x) = f(a) xœa 1 A function f(x) is continuous in an interval [a,b] if it is continuous at every point in that interval. The extreme value theorem Let f(x) be a continuous function in an interval [a,b]. -
Herschel Space Observatory and the NASA Herschel Science Center at IPAC
Herschel Space Observatory and The NASA Herschel Science Center at IPAC u George Helou u Implementing “Portals to the Universe” Report April, 2012 Implementing “Portals to the Universe”, April 2012 Herschel/NHSC 1 [OIII] 88 µm Herschel: Cornerstone FIR/Submm Observatory z = 3.04 u Three instruments: imaging at {70, 100, 160}, {250, 350 and 500} µm; spectroscopy: grating [55-210]µm, FTS [194-672]µm, Heterodyne [157-625]µm; bolometers, Ge photoconductors, SIS mixers; 3.5m primary at ambient T u ESA mission with significant NASA contributions, May 2009 – February 2013 [+/-months] cold Implementing “Portals to the Universe”, April 2012 Herschel/NHSC 2 Herschel Mission Parameters u Userbase v International; most investigator teams are international u Program Model v Observatory with Guaranteed Time and competed Open Time v ESA “Corner Stone Mission” (>$1B) with significant NASA contributions v NASA Herschel Science Center (NHSC) supports US community u Proposals/cycle (2 Regular Open Time cycles) v Submissions run 500 to 600 total, with >200 with US-based PI (~x3.5 over- subscription) u Users/cycle v US-based co-Investigators >500/cycle on >100 proposals u Funding Model v NASA funds US data analysis based on ESA time allocation u Default Proprietary Data Period v 6 months now, 1 year at start of mission Implementing “Portals to the Universe”, April 2012 Herschel/NHSC 3 Best Practices: International Collaboration u Approach to projects led elsewhere needs to be designed carefully v NHSC Charter remains firstly to support US community v But ultimately success of THE mission helps everyone v Need to express “dual allegiance” well and early to lead/other centers u NHSC became integral part of the larger team, worked for Herschel success, though focused on US community participation v Working closely with US community reveals needs and gaps for all users v Anything developed by NHSC is available to all users of Herschel v Trust follows from good teaming: E.g. -
MATH 1512: Calculus – Spring 2020 (Dual Credit) Instructor: Ariel
MATH 1512: Calculus – Spring 2020 (Dual Credit) Instructor: Ariel Ramirez, Ph.D. Email: [email protected] Office: LRC 172 Phone: 505-925-8912 OFFICE HOURS: In the Math Center/LRC or by Appointment COURSE DESCRIPTION: Limits. Continuity. Derivative: definition, rules, geometric and rate-of- change interpretations, applications to graphing, linearization and optimization. Integral: definition, fundamental theorem of calculus, substitution, applications to areas, volumes, work, average. Meets New Mexico Lower Division General Education Common Core Curriculum Area II: Mathematics (NMCCN 1614). (4 Credit Hours). Prerequisites: ((123 or ACCUPLACER College-Level Math =100-120) and (150 or ACT Math =28- 31 or SAT Math Section =660-729)) or (153 or ACT Math =>32 or SAT Math Section =>730). COURSE OBJECTIVES: 1. State, motivate and interpret the definitions of continuity, the derivative, and the definite integral of a function, including an illustrative figure, and apply the definition to test for continuity and differentiability. In all cases, limits are computed using correct and clear notation. Student is able to interpret the derivative as an instantaneous rate of change, and the definite integral as an averaging process. 2. Use the derivative to graph functions, approximate functions, and solve optimization problems. In all cases, the work, including all necessary algebra, is shown clearly, concisely, in a well-organized fashion. Graphs are neat and well-annotated, clearly indicating limiting behavior. English sentences summarize the main results and appropriate units are used for all dimensional applications. 3. Graph, differentiate, optimize, approximate and integrate functions containing parameters, and functions defined piecewise. Differentiate and approximate functions defined implicitly. 4. Apply tools from pre-calculus and trigonometry correctly in multi-step problems, such as basic geometric formulas, graphs of basic functions, and algebra to solve equations and inequalities. -
The X-Ray Imaging Polarimetry Explorer
Call for a Medium-size mission opportunity in ESA‟s Science Programme for a launch in 2025 (M4) XXIIPPEE The X-ray Imaging Polarimetry Explorer Lead Proposer: Paolo Soffitta (INAF-IAPS, Italy) Contents 1. Executive summary ................................................................................................................................................ 3 2. Science case ........................................................................................................................................................... 5 3. Scientific requirements ........................................................................................................................................ 15 4. Proposed scientific instruments............................................................................................................................ 20 5. Proposed mission configuration and profile ........................................................................................................ 35 6. Management scheme ............................................................................................................................................ 45 7. Costing ................................................................................................................................................................. 50 8. Annex ................................................................................................................................................................... 52 Page 1 XIPE is proposed -
Max-Planck-Institut Für Extraterrestrische
The X-ray Universe 2011, Berlin Max-Planck-Institut für extraterrestrische Physik Download this poster here: http://www.xray.mpe.mpg.de/~hbrunner/Berlin2011Poster.pdf eROSITA: all-sky survey data reduction, source characterization, and X-ray catalogue creation Hermann Brunner1, Thomas Boller1, Marcella Brusa1, Fabrizia Guglielmetti1, Georg Lamer2, Jan Robrade3, Christian Schmid4, Nico Cappelluti5, Francesco Pace6, Mauro Roncarelli7 1Max-Planck-Institut für extraterrestrische Physik, Garching, 2Leibniz-Institut für Astrophysik, Potsdam, 3Hamburger Sternwarte, 4Dr. Karl Remeis-Sternwarte und ECAP, 5INAF-Osservatorio Astronomico di Bologna, 6Zentrum für Astronomie der Universität Heidelberg, 7Dipartimento di Astronomico, Università di Bologna eROSITA on SRG All-sky survey sensitivity eROSITA (extended Roentgen Survey with an Imaging Telescope Array) is the primary instrument on the Russian Spektrum-Roentgen-Gamma (SRG) mission, scheduled for launch in 2013. eROSITA consists of Effective area on axis 15´Background off-axis 30´off-axis seven Wolter-I telescope modules, each of which is equipped with 54 mirror shells with an outer diameter of 36 cm and a fast frame-store pn-CCD, resulting in a field-of-view (1o diameter) averaged PSF of 25´´-30´´ 1 keV HEW (on-axis: 15´´ HEW) and an effective area of 1500 cm2 at 1.5 keV. eROSITA/SRG will perform a four year long all-sky survey, to be followed be several years of pointed observations (Predehl et al. 2010). More info on eROSITA: http://www.mpe.mpg.de/erosita/ 4 keV eROSITA orbit and scanning strategy 7 keV Orbit: eROSITA/SRG will be placed in an Averaged all-sky survey PSF (examples) L2 orbit with a semi-major axis of about 1 million km and an orbital period of about 6 months. -
Differentiating an Integral
Differentiating an Integral P. Haile, February 2020 b(t) Leibniz Rule. If (t) = a(t) f(z, t)dz, then R d b(t) @f(z, t) db da = dz + f (b(t), t) f (a(t), t) . dt @t dt dt Za(t) That’s the rule; now let’s see why this is so. We start by reviewing some things you already know. Let f be a smooth univariate function (i.e., a “nice” function of one variable). We know from the fundamental theorem of calculus that if the function is defined as x (x) = f(z) dz Zc (where c is a constant) then d (x) = f(x). (1) dx You can gain some really useful intuition for this by remembering that the x integral c f(z) dz is the area under the curve y = f(z), between z = a and z = x. Draw this picture to see that as x increases infinitessimally, the added contributionR to the area is f (x). Likewise, if c (x) = f(z) dz Zx then d (x) = f(x). (2) dx Here, an infinitessimal increase in x reduces the area under the curve by an amount equal to the height of the curve. Now suppose f is a function of two variables and define b (t) = f(z, t)dz (3) Za where a and b are constants. Then d (t) b @f(z, t) = dz (4) dt @t Za i.e., we can swap the order of the operations of integration and differentiation and “differentiate under the integral.” You’ve probably done this “swapping” 1 before. -
International Space Station Basics Components of The
National Aeronautics and Space Administration International Space Station Basics The International Space Station (ISS) is the largest orbiting can see 16 sunrises and 16 sunsets each day! During the laboratory ever built. It is an international, technological, daylight periods, temperatures reach 200 ºC, while and political achievement. The five international partners temperatures during the night periods drop to -200 ºC. include the space agencies of the United States, Canada, The view of Earth from the ISS reveals part of the planet, Russia, Europe, and Japan. not the whole planet. In fact, astronauts can see much of the North American continent when they pass over the The first parts of the ISS were sent and assembled in orbit United States. To see pictures of Earth from the ISS, visit in 1998. Since the year 2000, the ISS has had crews living http://eol.jsc.nasa.gov/sseop/clickmap/. continuously on board. Building the ISS is like living in a house while constructing it at the same time. Building and sustaining the ISS requires 80 launches on several kinds of rockets over a 12-year period. The assembly of the ISS Components of the ISS will continue through 2010, when the Space Shuttle is retired from service. The components of the ISS include shapes like canisters, spheres, triangles, beams, and wide, flat panels. The When fully complete, the ISS will weigh about 420,000 modules are shaped like canisters and spheres. These are kilograms (925,000 pounds). This is equivalent to more areas where the astronauts live and work. On Earth, car- than 330 automobiles. -
The Definite Integral
Mathematics Learning Centre Introduction to Integration Part 2: The Definite Integral Mary Barnes c 1999 University of Sydney Contents 1Introduction 1 1.1 Objectives . ................................. 1 2 Finding Areas 2 3 Areas Under Curves 4 3.1 What is the point of all this? ......................... 6 3.2 Note about summation notation ........................ 6 4 The Definition of the Definite Integral 7 4.1 Notes . ..................................... 7 5 The Fundamental Theorem of the Calculus 8 6 Properties of the Definite Integral 12 7 Some Common Misunderstandings 14 7.1 Arbitrary constants . ............................. 14 7.2 Dummy variables . ............................. 14 8 Another Look at Areas 15 9 The Area Between Two Curves 19 10 Other Applications of the Definite Integral 21 11 Solutions to Exercises 23 Mathematics Learning Centre, University of Sydney 1 1Introduction This unit deals with the definite integral.Itexplains how it is defined, how it is calculated and some of the ways in which it is used. We shall assume that you are already familiar with the process of finding indefinite inte- grals or primitive functions (sometimes called anti-differentiation) and are able to ‘anti- differentiate’ a range of elementary functions. If you are not, you should work through Introduction to Integration Part I: Anti-Differentiation, and make sure you have mastered the ideas in it before you begin work on this unit. 1.1 Objectives By the time you have worked through this unit you should: • Be familiar with the definition of the definite integral as the limit of a sum; • Understand the rule for calculating definite integrals; • Know the statement of the Fundamental Theorem of the Calculus and understand what it means; • Be able to use definite integrals to find areas such as the area between a curve and the x-axis and the area between two curves; • Understand that definite integrals can also be used in other situations where the quantity required can be expressed as the limit of a sum. -
Herschel Space Observatory-An ESA Facility for Far-Infrared And
Astronomy & Astrophysics manuscript no. 14759glp c ESO 2018 October 22, 2018 Letter to the Editor Herschel Space Observatory? An ESA facility for far-infrared and submillimetre astronomy G.L. Pilbratt1;??, J.R. Riedinger2;???, T. Passvogel3, G. Crone3, D. Doyle3, U. Gageur3, A.M. Heras1, C. Jewell3, L. Metcalfe4, S. Ott2, and M. Schmidt5 1 ESA Research and Scientific Support Department, ESTEC/SRE-SA, Keplerlaan 1, NL-2201 AZ Noordwijk, The Netherlands e-mail: [email protected] 2 ESA Science Operations Department, ESTEC/SRE-OA, Keplerlaan 1, NL-2201 AZ Noordwijk, The Netherlands 3 ESA Scientific Projects Department, ESTEC/SRE-P, Keplerlaan 1, NL-2201 AZ Noordwijk, The Netherlands 4 ESA Science Operations Department, ESAC/SRE-OA, P.O. Box 78, E-28691 Villanueva de la Canada,˜ Madrid, Spain 5 ESA Mission Operations Department, ESOC/OPS-OAH, Robert-Bosch-Strasse 5, D-64293 Darmstadt, Germany Received 9 April 2010; accepted 10 May 2010 ABSTRACT Herschel was launched on 14 May 2009, and is now an operational ESA space observatory offering unprecedented observational capabilities in the far-infrared and submillimetre spectral range 55−671 µm. Herschel carries a 3.5 metre diameter passively cooled Cassegrain telescope, which is the largest of its kind and utilises a novel silicon carbide technology. The science payload comprises three instruments: two direct detection cameras/medium resolution spectrometers, PACS and SPIRE, and a very high-resolution heterodyne spectrometer, HIFI, whose focal plane units are housed inside a superfluid helium cryostat. Herschel is an observatory facility operated in partnership among ESA, the instrument consortia, and NASA. The mission lifetime is determined by the cryostat hold time. -
Exploring the Sky with Erosita
Exploring the X-ray Sky with eROSITA for the eROSITA Team Observatories and mission timelines Basic Scientific Idea …. to extend the ROSAT all-sky survey up to 12 keV with an XMM type sensitivity Historical Development Spectrum-XG Jet-X, SODART, etc. ROSAT 1990-1998 First X-ray all-sky survey with an imaging telescope Negotiations between Roskosmos and ESA ABRIXAS 1999 on a "new" Spectrum-XG mission (2005) To extend the all-sky survey towards higher energies Agreement between Roskosmos and DLR (2007) ROSITA 2002 Spectrum-RG ABRIXAS science on the eROSITA International Space Station Dark Energy 105 Clusters of Galaxies extended ROentgen Survey with an Imaging Telescope Array Mission scenario & Instrument specification • 3 month calibration & science verification phase • 4 yrs all-sky survey (8 sky coverages) • 2.7 yrs pointed observations • Energy range 0.2 - 12 keV • FOV: 1 degree • All-sky survey sensitivity ~ 6 x10-14 erg cm-2 s-1 ~ (10 – 30) x ROSAT • Deep survey field(s) (~100 sqdeg) with 5×10-15 erg cm-2 s-1 • Temporal resolution ~ 50 ms • Energy resolution ~ 130 ev @ 6 keV / 80 ev @ 1.5 keV • Angular resolution ~ 15” (20” survey) eROSITA status: completely approved and funded Mr. Putin gets informed about Dark Energy... Signature of the "Detailed Agreement" (Reichle, Wörner, Perminov) 50:50 data share between Ru / Germany HERCULES BOOTES URSA MAIOR DRACO URSA MINOR LEO CEPHEUS VIRGO CASSIOPEIA CYGNUS AURIGA AQUILA GEMINI PERSEUS ANDROMEDA SCORPIUS PEGASUS SAGITTARIUS CENTAURUS TAURUS ORION VELA CRUX CANIS MAIOR AQUARIUS CARINA HEMISPHAERA ORIENTALIS HEMISPHAERA OCCIDENTALIS Actual definition depends on mission planning eROSITA: Launch date …. -
The X-Ray Background and the ROSAT Deep Surveys
THE X–RAY BACKGROUND AND THE ROSAT DEEP SURVEYS G. HASINGER Astrophysikalisches Institut Potsdam, An der Sternwarte 16, 14482 Potsdam, Germany E-mail : [email protected] G. ZAMORANI Osservatorio Astronomico, Via Zamboni 33, Bologna, 40126, Italy E-mail: [email protected] In this article we review the measurements and understanding of the X-ray back- ground (XRB), discovered by Giacconi and collaborators 35 years ago. We start from the early history and the debate whether the XRB is due to a single, homo- geneous physical process or to the summed emission of discrete sources, which was finally settled by COBE and ROSAT. We then describe in detail the progress from ROSAT deep surveys and optical identifications of the faint X-ray source popula- tion. In particular we discuss the role of active galactic nuclei (AGNs) as dominant contributors for the XRB, and argue that so far there is no need to postulate a hypothesized new population of X-ray sources. The recent advances in the under- standing of X-ray spectra of AGN is reviewed and a population synthesis model, based on the unified AGN schemes, is presented. This model is so far the most promising to explain all observational constraints. Future sensitive X-ray surveys in the harder X-ray band will be able to unambiguously test this picture. 1 Introduction It is a heavy responsibility for us, as it would be for everybody else, to write a paper on the X–ray Deep Surveys and the X–ray background (XRB) for this book, in honour of Riccardo Giacconi.