FINAL REPORT Senior Review of the Sun-Earth
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The Interstellar Transport of Galactic Cosmic Rays
Washington University in St. Louis Washington University Open Scholarship All Theses and Dissertations (ETDs) 5-24-2012 The nI terstellar Transport of Galactic Cosmic Rays Kelly Lave Washington University in St. Louis Follow this and additional works at: https://openscholarship.wustl.edu/etd Recommended Citation Lave, Kelly, "The nI terstellar Transport of Galactic Cosmic Rays" (2012). All Theses and Dissertations (ETDs). 707. https://openscholarship.wustl.edu/etd/707 This Dissertation is brought to you for free and open access by Washington University Open Scholarship. It has been accepted for inclusion in All Theses and Dissertations (ETDs) by an authorized administrator of Washington University Open Scholarship. For more information, please contact [email protected]. WASHINGTON UNIVERSITY IN ST. LOUIS Department of Physics Dissertation Examination Committee: Martin H. Israel, Chair W. Robert Binns James H. Buckley Ramanath Cowsik Bruce Fegley Jr. Henric Krawczynski Douglas A. Wiens The Interstellar Transport of Galactic Cosmic Rays by Kelly A. Lave A dissertation presented to the Graduate School of Arts and Sciences of Washington University in partial fulfillment of the requirements for the degree of Doctor of Philosophy August 2012 Saint Louis, Missouri c Copyright 2012 by Kelly A. Lave Abstract Using the Cosmic Ray Isotope Spectrometer (CRIS) onboard the Advanced Com- position Explorer (ACE) spacecraft, new and improved high-precision measurements of the elemental composition and energy spectra of galactic cosmic rays with energies from ∼50-550 MeV/nucleon and nuclear charge 5≤Z≤28 are reported here. These results cover observations during two solar minimum periods of the solar cycle, the most recent of which exhibited very low levels of solar activity and the highest galactic cosmic-ray intensities of the space era. -
The Early Explorers by Andrew J
The Early Explorers by Andrew J. LePage August 8, 1999 Among these programs were the next generation of Introduction Explorer satellites the ABMA was planning. In the chaos that swept the United States after the launching of the first Soviet Sputniks, a variety of The First New Explorers satellite programs was sponsored by the Department The first of the new series of larger Explorer satellites of Defense (DoD) to supplement (and in some cases was the 39.7 kilogram (87.5 pound) satellite NASA supplant) the country's flagging "official" satellite designated as S-1. Built by JPL, the spin stabilized program, Vanguard. One of the stronger programs S-1 consisted of a pair of fiberglass cones joined at was sponsored by the ABMA (Army Ballistic Missile their bases with a diameter and height of 76 Agency) with its engineering team lead by the centimeters each. The scientific payload consisted of German rocket expert, Wernher von Braun. Using instruments to study cosmic rays, solar X-ray and the Juno I launch vehicle, the ABMA team launched ultraviolet emissions, micrometeorites, as well as the America's first satellite, Explorer 1, which was built globe's heat balance. This was all powered by a bank by Caltech's Jet Propulsion Laboratory (JPL) (see of 15 nickel-cadmium batteries recharged by 3,000 Explorer: America's First Satellite in the February solar cells mounted on the satellite's exterior. This 1998 issue of SpaceViews). advanced payload was equipped with a timer to turn itself off after a year in orbit. While these first satellites returned a wealth of new data, they were limited by the tiny 11 kilogram (25 Explorer S-1 was launched from Cape Canaveral on pound) payload capability of the Juno I. -
XIII Publications, Presentations
XIII Publications, Presentations 1. Refereed Publications E., Kawamura, A., Nguyen Luong, Q., Sanhueza, P., Kurono, Y.: 2015, The 2014 ALMA Long Baseline Campaign: First Results from Aasi, J., et al. including Fujimoto, M.-K., Hayama, K., Kawamura, High Angular Resolution Observations toward the HL Tau Region, S., Mori, T., Nishida, E., Nishizawa, A.: 2015, Characterization of ApJ, 808, L3. the LIGO detectors during their sixth science run, Classical Quantum ALMA Partnership, et al. including Asaki, Y., Hirota, A., Nakanishi, Gravity, 32, 115012. K., Espada, D., Kameno, S., Sawada, T., Takahashi, S., Ao, Y., Abbott, B. P., et al. including Flaminio, R., LIGO Scientific Hatsukade, B., Matsuda, Y., Iono, D., Kurono, Y.: 2015, The 2014 Collaboration, Virgo Collaboration: 2016, Astrophysical Implications ALMA Long Baseline Campaign: Observations of the Strongly of the Binary Black Hole Merger GW150914, ApJ, 818, L22. Lensed Submillimeter Galaxy HATLAS J090311.6+003906 at z = Abbott, B. P., et al. including Flaminio, R., LIGO Scientific 3.042, ApJ, 808, L4. Collaboration, Virgo Collaboration: 2016, Observation of ALMA Partnership, et al. including Asaki, Y., Hirota, A., Nakanishi, Gravitational Waves from a Binary Black Hole Merger, Phys. Rev. K., Espada, D., Kameno, S., Sawada, T., Takahashi, S., Kurono, Lett., 116, 061102. Y., Tatematsu, K.: 2015, The 2014 ALMA Long Baseline Campaign: Abbott, B. P., et al. including Flaminio, R., LIGO Scientific Observations of Asteroid 3 Juno at 60 Kilometer Resolution, ApJ, Collaboration, Virgo Collaboration: 2016, GW150914: Implications 808, L2. for the Stochastic Gravitational-Wave Background from Binary Black Alonso-Herrero, A., et al. including Imanishi, M.: 2016, A mid-infrared Holes, Phys. -
Windows 7 Operating Guide
Welcome to Windows 7 1 1 You told us what you wanted. We listened. This Windows® 7 Product Guide highlights the new and improved features that will help deliver the one thing you said you wanted the most: Your PC, simplified. 3 3 Contents INTRODUCTION TO WINDOWS 7 6 DESIGNING WINDOWS 7 8 Market Trends that Inspired Windows 7 9 WINDOWS 7 EDITIONS 10 Windows 7 Starter 11 Windows 7 Home Basic 11 Windows 7 Home Premium 12 Windows 7 Professional 12 Windows 7 Enterprise / Windows 7 Ultimate 13 Windows Anytime Upgrade 14 Microsoft Desktop Optimization Pack 14 Windows 7 Editions Comparison 15 GETTING STARTED WITH WINDOWS 7 16 Upgrading a PC to Windows 7 16 WHAT’S NEW IN WINDOWS 7 20 Top Features for You 20 Top Features for IT Professionals 22 Application and Device Compatibility 23 WINDOWS 7 FOR YOU 24 WINDOWS 7 FOR YOU: SIMPLIFIES EVERYDAY TASKS 28 Simple to Navigate 28 Easier to Find Things 35 Easy to Browse the Web 38 Easy to Connect PCs and Manage Devices 41 Easy to Communicate and Share 47 WINDOWS 7 FOR YOU: WORKS THE WAY YOU WANT 50 Speed, Reliability, and Responsiveness 50 More Secure 55 Compatible with You 62 Better Troubleshooting and Problem Solving 66 WINDOWS 7 FOR YOU: MAKES NEW THINGS POSSIBLE 70 Media the Way You Want It 70 Work Anywhere 81 New Ways to Engage 84 INTRODUCTION TO WINDOWS 7 6 WINDOWS 7 FOR IT PROFESSIONALS 88 DESIGNING WINDOWS 7 8 WINDOWS 7 FOR IT PROFESSIONALS: Market Trends that Inspired Windows 7 9 MAKE PEOPLE PRODUCTIVE ANYWHERE 92 WINDOWS 7 EDITIONS 10 Remove Barriers to Information 92 Windows 7 Starter 11 Access -
Information Summaries
TIROS 8 12/21/63 Delta-22 TIROS-H (A-53) 17B S National Aeronautics and TIROS 9 1/22/65 Delta-28 TIROS-I (A-54) 17A S Space Administration TIROS Operational 2TIROS 10 7/1/65 Delta-32 OT-1 17B S John F. Kennedy Space Center 2ESSA 1 2/3/66 Delta-36 OT-3 (TOS) 17A S Information Summaries 2 2 ESSA 2 2/28/66 Delta-37 OT-2 (TOS) 17B S 2ESSA 3 10/2/66 2Delta-41 TOS-A 1SLC-2E S PMS 031 (KSC) OSO (Orbiting Solar Observatories) Lunar and Planetary 2ESSA 4 1/26/67 2Delta-45 TOS-B 1SLC-2E S June 1999 OSO 1 3/7/62 Delta-8 OSO-A (S-16) 17A S 2ESSA 5 4/20/67 2Delta-48 TOS-C 1SLC-2E S OSO 2 2/3/65 Delta-29 OSO-B2 (S-17) 17B S Mission Launch Launch Payload Launch 2ESSA 6 11/10/67 2Delta-54 TOS-D 1SLC-2E S OSO 8/25/65 Delta-33 OSO-C 17B U Name Date Vehicle Code Pad Results 2ESSA 7 8/16/68 2Delta-58 TOS-E 1SLC-2E S OSO 3 3/8/67 Delta-46 OSO-E1 17A S 2ESSA 8 12/15/68 2Delta-62 TOS-F 1SLC-2E S OSO 4 10/18/67 Delta-53 OSO-D 17B S PIONEER (Lunar) 2ESSA 9 2/26/69 2Delta-67 TOS-G 17B S OSO 5 1/22/69 Delta-64 OSO-F 17B S Pioneer 1 10/11/58 Thor-Able-1 –– 17A U Major NASA 2 1 OSO 6/PAC 8/9/69 Delta-72 OSO-G/PAC 17A S Pioneer 2 11/8/58 Thor-Able-2 –– 17A U IMPROVED TIROS OPERATIONAL 2 1 OSO 7/TETR 3 9/29/71 Delta-85 OSO-H/TETR-D 17A S Pioneer 3 12/6/58 Juno II AM-11 –– 5 U 3ITOS 1/OSCAR 5 1/23/70 2Delta-76 1TIROS-M/OSCAR 1SLC-2W S 2 OSO 8 6/21/75 Delta-112 OSO-1 17B S Pioneer 4 3/3/59 Juno II AM-14 –– 5 S 3NOAA 1 12/11/70 2Delta-81 ITOS-A 1SLC-2W S Launches Pioneer 11/26/59 Atlas-Able-1 –– 14 U 3ITOS 10/21/71 2Delta-86 ITOS-B 1SLC-2E U OGO (Orbiting Geophysical -
In-Flight PSF Calibration of the Nustar Hard X-Ray Optics
In-flight PSF calibration of the NuSTAR hard X-ray optics Hongjun Ana, Kristin K. Madsenb, Niels J. Westergaardc, Steven E. Boggsd, Finn E. Christensenc, William W. Craigd,e, Charles J. Haileyf, Fiona A. Harrisonb, Daniel K. Sterng, William W. Zhangh aDepartment of Physics, McGill University, Montreal, Quebec, H3A 2T8, Canada; bCahill Center for Astronomy and Astrophysics, California Institute of Technology, Pasadena, CA 91125, USA; cDTU Space, National Space Institute, Technical University of Denmark, Elektrovej 327, DK-2800 Lyngby, Denmark; dSpace Sciences Laboratory, University of California, Berkeley, CA 94720, USA; eLawrence Livermore National Laboratory, Livermore, CA 94550, USA; fColumbia Astrophysics Laboratory, Columbia University, New York NY 10027, USA; gJet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USA; hGoddard Space Flight Center, Greenbelt, MD 20771, USA ABSTRACT We present results of the point spread function (PSF) calibration of the hard X-ray optics of the Nuclear Spectroscopic Telescope Array (NuSTAR). Immediately post-launch, NuSTAR has observed bright point sources such as Cyg X-1, Vela X-1, and Her X-1 for the PSF calibration. We use the point source observations taken at several off-axis angles together with a ray-trace model to characterize the in-orbit angular response, and find that the ray-trace model alone does not fit the observed event distributions and applying empirical corrections to the ray-trace model improves the fit significantly. We describe the corrections applied to the ray-trace model and show that the uncertainties in the enclosed energy fraction (EEF) of the new PSF model is ∼<3% for extraction ′′ apertures of R ∼> 60 with no significant energy dependence. -
Nustar Observatory Guide
NuSTAR Guest Observer Program NuSTAR Observatory Guide Version 3.2 (June 2016) NuSTAR Science Operations Center, California Institute of Technology, Pasadena, CA NASA Goddard Spaceflight Center, Greenbelt, MD nustar.caltech.edu heasarc.gsfc.nasa.gov/docs/nustar/index.html i Revision History Revision Date Editor Comments D1,2,3 2014-08-01 NuSTAR SOC Initial draft 1.0 2014-08-15 NuSTAR GOF Release for AO-1 Addition of more information about CZT 2.0 2014-10-30 NuSTAR SOC detectors in section 3. 3.0 2015-09-24 NuSTAR SOC Update to section 4 for release of AO-2 Update for NuSTARDAS v1.6.0 release 3.1 2016-05-10 NuSTAR SOC (nusplitsc, Section 5) 3.2 2016-06-15 NuSTAR SOC Adjustment to section 9 ii Table of Contents Revision History ......................................................................................................................................................... ii 1. INTRODUCTION ................................................................................................................................................... 1 1.1 NuSTAR Program Organization ..................................................................................................................................................................................... 1 2. The NuSTAR observatory .................................................................................................................................... 2 2.1 NuSTAR Performance ........................................................................................................................................................................................................ -
Building the Coolest X-Ray Satellite
National Aeronautics and Space Administration Building the Coolest X-ray Satellite 朱雀 Suzaku A Video Guide for Teachers Grades 9-12 Probing the Structure & Evolution of the Cosmos http://suzaku-epo.gsfc.nasa.gov/ www.nasa.gov The Suzaku Learning Center Presents “Building the Coolest X-ray Satellite” Video Guide for Teachers Written by Dr. James Lochner USRA & NASA/GSFC Greenbelt, MD Ms. Sara Mitchell Mr. Patrick Keeney SP Systems & NASA/GSFC Coudersport High School Greenbelt, MD Coudersport, PA This booklet is designed to be used with the “Building the Coolest X-ray Satellite” DVD, available from the Suzaku Learning Center. http://suzaku-epo.gsfc.nasa.gov/ Table of Contents I. Introduction 1. What is Astro-E2 (Suzaku)?....................................................................................... 2 2. “Building the Coolest X-ray Satellite” ....................................................................... 2 3. How to Use This Guide.............................................................................................. 2 4. Contents of the DVD ................................................................................................. 3 5. Post-Launch Information ........................................................................................... 3 6. Pre-requisites............................................................................................................. 4 7. Standards Met by Video and Activities ...................................................................... 4 II. Video Chapter 1 -
Software Error Doomed Japanese Hitomi Spacecraft!
Software error doomed Japanese Hitomi spacecraft! ! Space agency declares the astronomy satellite a loss.! ! Japan’s flagship Hitomi astronomical satellite, which launched successfully on 17 February but tumbled out of control five weeks later, may have been doomed by a basic engineering error. Confused about how it was oriented in space and trying to stop itself from spinning, Hitomi's software apparently fired a thruster jet in the wrong direction — accelerating rather than slowing the craft's rotation.! ! http://www.nature.com/news/software-error-doomed-japanese-hitomi- spacecraft-1.19835! 1! Gamma-Ray Bursts- Longair 22.7! • Are bright flashes of γ-rays- for a short period of time (<100 sec )! • fluxes of ~0.1-100 photon/cm2/sec/keV emitted primarily in the 20-500 keV band.! – Distribution is isotropic on the sky! • Because of these properties it took ~30 years from their discovery (1967) to their identification! – They are at very large distances (z up to 8 (!)) with apparent luminosities of 3x1054 erg/sec! – Rate is ~10-7/yr/galaxy ! • What are they??- short timescales imply compact object ; what could the 2 33 energy reservoir be- Mc implies M~10 gms~ Msun if total conversion of mass into energy How does all this energy end up as γ-rays ?! – Location of long γRBs is in and near star forming regions in smallish galaxies- associated with star formation! – a few γRBs have been associated with a type Ic supernova! 2! 3! Gamma-Ray Bursts ! • Cosmic γ-ray bursts (GRBs) were first reported in 1973 by Klebesadel et al (l973) but were first seen -
Calibration Method and Uncertainty for the Primordial Inflation Explorer
Prepared for submission to JCAP Calibration Method and Uncertainty for the Primordial Inflation Explorer (PIXIE) A. Kogut1 and D.J. Fixsen1;2 1Code 665, Goddard Space Flight Center, Greenbelt, MD 20771 USA 2University of Maryland, College Park, MD 20742 USA E-mail: [email protected], [email protected] Abstract. The Primordial Inflation Explorer (PIXIE) is an Explorer-class mission con- cept to measure cosmological signals from both linear polarization of the cosmic microwave background and spectral distortions from a perfect blackbody. The targeted measurement arXiv:2002.00976v2 [astro-ph.IM] 4 Mar 2021 sensitivity is 2{4 orders of magnitude below competing astrophysical foregrounds, placing stringent requirements on instrument calibration. An on-board blackbody calibrator presents a polarizing Fourier transform spectrometer with a known signal to enable conversion of the sampled interference fringe patterns from telemetry units to physical units. We describe the instrumentation and operations needed to calibrate PIXIE, derive the expected uncertainty for the intensity, polarization, and frequency scales, and show the effect of calibration uncer- tainty in the derived cosmological signals. In-flight calibration is expected to be accurate to a few parts in 106 at frequencies dominated by the CMB, and a few parts in 104 at higher frequencies dominated by the diffuse dust foreground. Keywords: CMBR experiments, CMBR polarisation 1 Introduction The cosmic microwave background (CMB) provides a unique window to the early universe. Its blackbody spectrum points to a hot, dense phase in the early universe, while spatial maps of small temperature perturbations about the blackbody mean provide detailed information on the geometry, constituents, and evolution of the universe. -
Photographs Written Historical and Descriptive
CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY HAER FL-8-B BUILDING AE HAER FL-8-B (John F. Kennedy Space Center, Hanger AE) Cape Canaveral Brevard County Florida PHOTOGRAPHS WRITTEN HISTORICAL AND DESCRIPTIVE DATA HISTORIC AMERICAN ENGINEERING RECORD SOUTHEAST REGIONAL OFFICE National Park Service U.S. Department of the Interior 100 Alabama St. NW Atlanta, GA 30303 HISTORIC AMERICAN ENGINEERING RECORD CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY BUILDING AE (Hangar AE) HAER NO. FL-8-B Location: Hangar Road, Cape Canaveral Air Force Station (CCAFS), Industrial Area, Brevard County, Florida. USGS Cape Canaveral, Florida, Quadrangle. Universal Transverse Mercator Coordinates: E 540610 N 3151547, Zone 17, NAD 1983. Date of Construction: 1959 Present Owner: National Aeronautics and Space Administration (NASA) Present Use: Home to NASA’s Launch Services Program (LSP) and the Launch Vehicle Data Center (LVDC). The LVDC allows engineers to monitor telemetry data during unmanned rocket launches. Significance: Missile Assembly Building AE, commonly called Hangar AE, is nationally significant as the telemetry station for NASA KSC’s unmanned Expendable Launch Vehicle (ELV) program. Since 1961, the building has been the principal facility for monitoring telemetry communications data during ELV launches and until 1995 it processed scientifically significant ELV satellite payloads. Still in operation, Hangar AE is essential to the continuing mission and success of NASA’s unmanned rocket launch program at KSC. It is eligible for listing on the National Register of Historic Places (NRHP) under Criterion A in the area of Space Exploration as Kennedy Space Center’s (KSC) original Mission Control Center for its program of unmanned launch missions and under Criterion C as a contributing resource in the CCAFS Industrial Area Historic District. -
Solar Flares
https://ntrs.nasa.gov/search.jsp?R=20150005791 2019-08-31T11:04:12+00:00Z Solar Flares Sabrina Savage (NASA/MSFC) Heliophysics System Observatory (HSO) • Fleet of solar, heliospheric, geospace, and planetary satellites designed to work independently while enabling large-scale collaborative investigations. http://www.nasa.gov/mission_pages/sunearth/missions/ Heliophysics System Observatory (HSO): http://www.nasa.gov/mission_pages/sunearth/missions/ The Sun in Layers Converts 4 million tons of matter into energy every second. Core is as dense as lead. Interplay between magnetic pressure and gas (plasma) pressure. 15 000 000 ∘C “Mysteries of the Sun”: NASA / Jenny Mottar Sun Facts: http://solarscience.msfc.nasa.gov/ The Sun in Layers 15 000 000 ∘C European Space Agency (ESA) Smithsonian Astrophysical Observatory (SAO) “Mysteries of the Sun”: NASA / Jenny Mottar Sun Facts: http://solarscience.msfc.nasa.gov/ Sunspots & Active Regions 1625 May: Christoph Scheiner 2014 April 14: SDO HMI 6173 A European Space Agency (ESA) / Royal Observatory Belgium (ROB) NOAA Active Regions: SolarMonitor.org PROBA2 Science Center (ROB): http://proba2.sidc.be/ Sunspots & Active Regions Formation 4500 A 193 A 131 A SDO / AIA 2014 Apr 13 - 15 JHelioviewer — Explore the Sun: http://jhelioviewer.org/ Sunspots & Active Regions Hinode SOT: NASA / JAXA / NAOJ Sunspot Magnetic fields ~ 3000-6000 times stronger than Earth’s field. Magnetic pressure dominates gas pressure in spot, thus inhibiting convective flow of heat. JHelioviewer SDO / AIA 2014 Apr 04 SOT (CN line 3883 A); 2007 May 2 SOHO animation gallery SOT Picture of the Day (POD): http://sot.lmsal.com/pod?cmd=view-gallery Sunspots & Active Regions Solar Dynamics Observatory (GSFC) Jewel Box: http://svs.gsfc.nasa.gov/vis/a000000/a004100/a004117/ Sunspots & Active Regions Courtesy of Milo Littenberg Sunspots & Active Regions “SDO Jewel Box” Solar features as seen with 10 different filters (i.e., plasma at different temperatures).