Interstellar Heliospheric Probe/Heliospheric Boundary Explorer Mission—A Mission to the Outermost Boundaries of the Solar System
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Program Book Update
15th Annual International Astrophysics Conference Cape Coral, FL – April 3-8, 2016 AGENDA SUNDAY, APRIL 3 5:00 PM – 8:00 PM Registration – Tarpon Terrace 6:00 PM – 9:00 PM Welcome Reception - Tarpon Terrace MONDAY, APRIL 4 7:00 AM - 5:00 PM Registration – Grandville Ballroom 8:00 AM – 6:00 PM GENERAL SESSION – Grandville Ballroom CHAIR: Zank 7:45 AM - 8:00 AM GARY ZANK WELCOME 8:00 AM - 8:25 AM Chen, Bin Particle Acceleration by a Solar Flare Termination Shock 8:25 AM - 8:50 AM Bucik, Radoslav Large-scale Coronal Waves in 3He-rich Solar Energetic Particle Events Element Abundances and Source Plasma Temperatures of 8:50 AM - 9:15 AM Reames, Donald Solar Energetic Particles 9:15 AM - 9:40 AM Manchester, Ward Simulating CME-Driven Shocks and Implications for SEPs STEREO and ACE SEP Science- Transforming Space Weather 9:40 AM - 10:05 AM Luhmann, Janet Prospects 10:05 AM - 10:30 AM Morning Break - Ballroom Foyer CHAIR: Zirnstein 11 years of ENA imaging with Cassini/INCA and in-situ ion Voyager1 & 10:30 AM - 10:55 AM Krimigis, Stamatios 2/LECP measurements Investigating the Heliospheric Boundary at Energies down to 10eV with 10:55 AM - 11:20 AM Wurz, Peter Neutral Atom Imaging by IBEX. In-situ and Remote Sensing Studies of Solar Wind Origin and 11:20 AM - 11:45 AM Landi, Enrico Acceleration The Sun’s Dynamic Influence on the Outer Heliosphere, the Heliosheath, 11:45 AM - 12:10 PM Intriligator, Devrie and the Local Interstellar Medium 12:10 PM – 1:30 PM Lunch Break – Ballroom Foyer CHAIR: Fichtner 1:30 PM - 1:55 PM McNutt, Ralph Making Interstellar -
Space Weathering of Itokawa Particles: Implications for Regolith Evolution
46th Lunar and Planetary Science Conference (2015) 2351.pdf SPACE WEATHERING OF ITOKAWA PARTICLES: IMPLICATIONS FOR REGOLITH EVOLUTION. Eve L. Berger1 and Lindsay P. Keller2, 1Geocontrol Systems – Jacobs JETS contract – NASA Johnson Space Center, Houston TX 77058, [email protected], 2NASA Johnson Space Center Introduction: Space weathering processes such as tion rate of 4.1 ±1.2 × 104 tracks/cm2/year at 1AU [6] solar wind irradiation and micrometeorite impacts are are: ~80,000 years for 0211, ~70,000 years for 0192, known to alter the the properties of regolith materials and ~24,000 years for 0125. exposed on airless bodies [1]. The rates of space Discussion: Cosmic-ray exposure: Measurements weathering processes however, are poorly constrained of cosmic-ray exposure (CRE) ages of Itokawa parti- for asteroid regoliths, with recent estimates ranging cles [6-8] reveal that these grains are relatively young, over many orders of magnitude [e.g., 2, 3]. The return of surface samples by JAXA’s Hayabusa mission to ≤1−1.5 Ma, when compared to the distribution of ex- asteroid 25143 Itokawa, and their laboratory analysis posure ages for LL chondrite meteorites (8−50Ma) [9]. provides “ground truth” to anchor the timescales for The CRE ages for Itokawa grains are consistent with a space weathering processes on airless bodies. Here, we stable regolith at meter-depths for ~106 years. use the effects of solar wind irradiation and the Solar flare particle tracks: Based on the solar flare accumulation of solar flare tracks recorded in Itokawa particle track production rate in olivine at 1AU [6], the grains to constrain the rates of space weathering and Itokawa grains recorded solar flare tracks over time- yield information about regolith dynamics on these scales of <105 years. -
And Type Ii Solar Outbursts
X-641-65-68 / , RADIO EMISSION FROM SHOCK WAVES - AND TYPE II SOLAR OUTBURSTS FEBRUARY 1965 \ -1 , GREENBELT, MARYLAND , X-641-65- 68 RADIO EMISSION FROM SHOCK WAVES AND TYPE II SOLAR OUTBURSTS bY Derek A. Tidman February 1965 NASA-Goddard Space Flight Center Greenbelt, Maryland * RADIO EMISSION FROM SHOCK WAVES AND TYPE 11 SOLAR OUTBURSTS Derek A. Tidman* NASA-Goddard Space Flight Center Greenbelt, Maryland ABSTRACT A model for Type 11 solar radio outbursts is discussed. The radiation is hypothesized to originate in the process of collective bremsstrahlung emitted by non-thermal electron and ion density fluctuations in a plasma containing a flux of energetic electrons. The source of radiation is assumed to be a collisionless plasma shock wave rising through the solar corona. It is also suggested that the collisionless bow shocks of the earth and planets in the solar wind might be similar but weaker sources of low frequency emission with a similar two- harmonic structure to Type 11 emission. * Permanent address: Institute for Fluid Dynamics and Applied Mathematics, University of Maryland, College Park, Maryland. iii RADIO EMISSION FROM SHOCK WAVES AND TYPE II SOLAR OUTBURSTS by Derek A. Tidman NASA-Goddard Space Flight Center Greenbelt, Maryland INTRODUCTION In a previous paper' we calculated the bremsstrahlung emitted from thermal plasmas which co-exist with a flux of energetic (suprathermal) electrons. It was found that under some circumstances the radiation emitted from such plasmas can be greatly increased compared to the emission from a Maxwellian plasma with no energetic particles present. The enhanced emission occurs at the funda- mental and second harmonic of the electron plasma frequency. -
Radio Emissions Associated with Shock Waves and a Brief Model of Type Ii Solar Radio Bursts
RADIO EMISSIONS ASSOCIATED WITH SHOCK WAVES AND A BRIEF MODEL OF TYPE II SOLAR RADIO BURSTS C. S. Wu¤ Abstract In this paper, we discuss the generation of radio waves at shock waves. Two cases are considered. One is associated with a quasi{perpendicular shock and the other is with a quasi{parallel shock. In the former case, it is stressed that a nearly perpendicular shock can lead to a fast Fermi acceleration. Looking at these energized electrons either in the deHo®mann{Teller frame or the plasma frame, one concludes that the accelerated electrons should inherently possess a loss{cone distribution after the mirror reflection at the shock. Consequently, these electrons can lead to induced emission of radio waves via a maser instability. In the latter case, we assume that a quasi{parallel shock is propagating in an environment which has already been populated with energetic electrons. In this case, the shock wave can also lead to induced radiation via a maser instability. Based on this notion, we describe briefly a model to explain the Type II solar radio bursts which is a very intriguing phenomenon and has a long history. 1 Introduction An interesting theoretical issue is how radio emission processes can be induced or triggered by shock waves under various physical conditions. In this article, we present a discussion which comprises two parts. The ¯rst part is concerned with a nearly perpendicular shock. In this case, the shock can energize a fraction of the thermal electrons or suprathermal electrons to much higher energies by means of a fast Fermi process. -
Arxiv:1712.09051V1 [Astro-Ph.SR] 25 Dec 2017
Solar Physics DOI: 10.1007/•••••-•••-•••-••••-• Origin of a CME-related shock within the LASCO C3 field-of-view V.G.Fainshtein1 · Ya.I.Egorov1 c Springer •••• Abstract We study the origin of a CME-related shock within the LASCO C3 field-of-view (FOV). A shock originates, when a CME body velocity on its axis surpasses the total velocity VA + VSW , where VA is the Alfv´envelocity, VSW is the slow solar wind velocity. The formed shock appears collisionless, because its front width is manifold less, than the free path of coronal plasma charged particles. The Alfv´envelocity dependence on the distance was found by using characteristic values of the magnetic induction radial component and of the proton concentration in the Earth orbit, and by using the known regularities of the variations in these solar wind characteristics with distance. A peculiarity of the analyzed CME is its formation at a relatively large height, and the CME body slow acceleration with distance. We arrived at a conclusion that the formed shock is a bow one relative to the CME body moving at a super Alfv´envelocity. At the same time, the shock formation involves a steeping of the front edge of the coronal plasma disturbed region ahead of the CME body, which is characteristic of a piston shock. Keywords: Sun, Coronal Mass Ejection, Shock 1. Introduction The assumption that, ahead of solar material bunches that were earlier thought to be emitted during solar flares, a shock may emerge in the interplanetary space was already stated in 1950s (Gold, 1962). Based on observations of coronal mass ejections (CMEs) in 1973-1974 (Skylab era), Gosling et al., 1976 supposed that a bow shock should emerge ahead of sufficiently fast CEs. -
Introduction to Astronomy from Darkness to Blazing Glory
Introduction to Astronomy From Darkness to Blazing Glory Published by JAS Educational Publications Copyright Pending 2010 JAS Educational Publications All rights reserved. Including the right of reproduction in whole or in part in any form. Second Edition Author: Jeffrey Wright Scott Photographs and Diagrams: Credit NASA, Jet Propulsion Laboratory, USGS, NOAA, Aames Research Center JAS Educational Publications 2601 Oakdale Road, H2 P.O. Box 197 Modesto California 95355 1-888-586-6252 Website: http://.Introastro.com Printing by Minuteman Press, Berkley, California ISBN 978-0-9827200-0-4 1 Introduction to Astronomy From Darkness to Blazing Glory The moon Titan is in the forefront with the moon Tethys behind it. These are two of many of Saturn’s moons Credit: Cassini Imaging Team, ISS, JPL, ESA, NASA 2 Introduction to Astronomy Contents in Brief Chapter 1: Astronomy Basics: Pages 1 – 6 Workbook Pages 1 - 2 Chapter 2: Time: Pages 7 - 10 Workbook Pages 3 - 4 Chapter 3: Solar System Overview: Pages 11 - 14 Workbook Pages 5 - 8 Chapter 4: Our Sun: Pages 15 - 20 Workbook Pages 9 - 16 Chapter 5: The Terrestrial Planets: Page 21 - 39 Workbook Pages 17 - 36 Mercury: Pages 22 - 23 Venus: Pages 24 - 25 Earth: Pages 25 - 34 Mars: Pages 34 - 39 Chapter 6: Outer, Dwarf and Exoplanets Pages: 41-54 Workbook Pages 37 - 48 Jupiter: Pages 41 - 42 Saturn: Pages 42 - 44 Uranus: Pages 44 - 45 Neptune: Pages 45 - 46 Dwarf Planets, Plutoids and Exoplanets: Pages 47 -54 3 Chapter 7: The Moons: Pages: 55 - 66 Workbook Pages 49 - 56 Chapter 8: Rocks and Ice: -
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. -
Abstract Observation Overview Nustar HXR Imaging Microflare
Imaging and Spectroscopy of Six NuSTAR MicroFlares SH11D-2898 Contact: J. Duncan1, L. Glesener1, I. Hannah2, D. Smith3, B. Grefenstette4 (1Univ, of Minnesota; 2Univ. of Glasgow; 3UC Santa Cruz; 4California Institute of Technology) [email protected] Abstract MicroFlare Time Evolution Hard X-ray (HXR) emission in solar flares originates from regions of high temperature plasma, as well as from non-thermal particle populations [1]. Both of these sources of HXR radiation make solar observation in this band important for study of • NuSTAR observed 6 MicroFlares during this observation. Time evolution is shown in both raw and normalized NuSTAR flare energetics. NuSTAR is the first HXR telescope with direct focusing optics, giving it a dramatic increase in sensitivity countsLivetime acrosscorrection several applied energy ranges for each flare. Counts are livetime-corrected (NuSTAR livetime ranged from 1-14%). Livetime correction applied over previous indirect imaging methods. Here we present NuSTAR observation of six microflares from one solar active Livetime correction applied 5 5 6 5×10 4×10 2.0 10 5 × 4×10 5 region during a period of several hours on May 29th, 2018. In conjunction with simultaneous data from SDO/AIA, data 3×10 5 2-4 keV 2-4 keV 6 3×10 1.5 10 Orbit1, Flare B 4-6 keV 2×105 4-6 keV × 5 counts 2 10 2-4 keV × Orbit1, Flare A 6-8 keV counts Orbit1, Flare C 6-8 keV from this observation has been used to create flare-time images showing the spatial extent of HXR emission. Additionally, 5 5 1 10 1×10 8-10 keV × 8-10 keV 6 4-6 keV 1.0×10 (Left) Estimated GOES A5 flare, with 0 0 1.2 1.2 16:07 16:08 16:09 16:10 16:11 16:46 16:48 16:50 16:52 16:54 NuSTAR lightcurves show time evolution in four different HXR energy ranges over the course of each flare. -
Build a Spacecraft Activity
UAMN Virtual Family Day: Amazing Earth Build a Spacecraft SMAP satellite. Image: NASA. Discover how scientists study Earth from above! Scientists use satellites and spacecraft to study the Earth from outer space. They take pictures of Earth's surface and measure cloud cover, sea levels, glacier movements, and more. Materials Needed: Paper, pencil, craft materials (small recycled boxes, cardboard pieces, paperclips, toothpicks, popsicle sticks, straws, cotton balls, yarn, etc. You can use whatever supplies you have!), fastening materials (glue, tape, rubber bands, string, etc.) Instructions: Step 1: Decide what you want your spacecraft to study. Will it take pictures of clouds? Track forest fires? Measure rainfall? Be creative! Step 2: Design your spacecraft. Draw a picture of what your spacecraft will look like. It will need these parts: Container: To hold everything together. Power Source: To create electricity; solar panels, batteries, etc. Scientific Instruments: This is the why you launched your satellite in the first place! Instruments could include cameras, particle collectors, or magnometers. Communication Device: To relay information back to Earth. Image: NASA SpacePlace. Orientation Finder: A sun or star tracker to show where the spacecraft is pointed. Step 3: Build your spacecraft! Use any craft materials you have available. Let your imagination go wild. Step 4: Your spacecraft will need to survive launching into orbit. Test your spacecraft by gently shaking or spinning it. How well did it hold together? Adjust your design and try again! Model spacecraft examples. Courtesy NASA SpacePlace. Activity adapted from NASA SpacePlace: spaceplace.nasa.gov/build-a-spacecraft/en/ UAMN Virtual Early Explorers: Amazing Earth Studying Earth From Above NASA is best known for exploring outer space, but it also conducts many missions to investigate Earth from above. -
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 ........................................................................................................................................................................................................ -
From the Heliosphere Into the Sun Programme Book Incuding All
511th WE-Heraeus-Seminar From the Heliosphere into the Sun –SailingagainsttheWind– Programme book incuding all abstracts Physikzentrum Bad Honnef, Germany January 31 – February 3, 2012 http://www.mps.mpg.de/meetings/heliocorona/ From the Heliosphere into the Sun A meeting dedicated to the progress of our understanding of the solar wind and the corona in the light of the upcoming Solar Orbiter mission This meeting is dedicated to the processes in the solar wind and corona in the light of the upcoming Solar Orbiter mission. Over the last three decades there has been astonishing progress in our understanding of the solar corona and the inner heliosphere driven by remote-sensing and in-situ observations. This period of time has seen the first high-resolution X-ray and EUV observations of the corona and the first detailed measurements of the ion and electron velocity distribution functions in the inner heliosphere. Today we know that we have to treat the corona and the wind as one single object, which calls for a mission that is fully designed to investigate the interwoven processes all the way from the solar surface to the heliosphere. The meeting will provide a forum to review the advances over the last decades, relate them to our current understanding and to discuss future directions. We will concentrate one day on in- situ observations and related models of the inner heliosphere, and spend another day on remote sensing observations and modeling of the corona – always with an eye on the symbiotic nature of the two. On the third day we will direct our view towards the future. -
Space Weathering on Mercury
Advances in Space Research 33 (2004) 2152–2155 www.elsevier.com/locate/asr Space weathering on Mercury S. Sasaki *, E. Kurahashi Department of Earth and Planetary Science, The University of Tokyo, Tokyo 113 0033, Japan Received 16 January 2003; received in revised form 15 April 2003; accepted 16 April 2003 Abstract Space weathering is a process where formation of nanophase iron particles causes darkening of overall reflectance, spectral reddening, and weakening of absorption bands on atmosphereless bodies such as the moon and asteroids. Using pulse laser irra- diation, formation of nanophase iron particles by micrometeorite impact heating is simulated. Although Mercurian surface is poor in iron and rich in anorthite, microscopic process of nanophase iron particle formation can take place on Mercury. On the other hand, growth of nanophase iron particles through Ostwald ripening or repetitive dust impacts would moderate the weathering degree. Future MESSENGER and BepiColombo mission will unveil space weathering on Mercury through multispectral imaging observations. Ó 2003 COSPAR. Published by Elsevier Ltd. All rights reserved. 1. Introduction irradiation should change the optical properties of the uppermost regolith surface of atmosphereless bodies. Space weathering is a proposed process to explain Although Hapke et al. (1975) proposed that formation spectral mismatch between lunar soils and rocks, and of iron particles with sizes from a few to tens nanome- between asteroids (S-type) and ordinary chondrites. ters should be responsible for the optical property Most of lunar surface and asteroidal surface exhibit changes, impact-induced formation of glassy materials darkening of overall reflectance, spectral reddening had been considered as a primary cause for space (darkening of UV–Vis relative to IR), and weakening of weathering.