In Situ Studies of the Solar Corona After Parker Solar Probe and Solar Orbiter
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Arxiv:2006.00776V1 [Physics.Space-Ph] 1 Jun 2020
manuscript submitted to Geophysical Research Letters Dust impact voltage signatures on Parker Solar Probe: influence of spacecraft floating potential S. D. Bale1,2, K. Goetz3, J. W. Bonnell1, A. W. Case4, C. H. K. Chen5,T. Dudok de Wit6, L. C. Gasque1,2, P. R. Harvey1, J. C. Kasper 7,4, P. J. Kellogg3, R. J. MacDowall8, M. Maksimovic9, D. M. Malaspina10, B. F. Page1,2, M. Pulupa1, M. L. Stevens4, J. R. Szalay11, A. Zaslavsky9 1Space Sciences Laboratory, University of California, Berkeley, CA 94720-7450, USA 2Physics Department, University of California, Berkeley, CA 94720-7300, USA 3School of Physics and Astronomy, University of Minnesota, Minneapolis, 55455, USA 4Smithsonian Astrophysical Observatory, Cambridge, MA 02138 USA 5School of Physics and Astronomy, Queen Mary University of London, London E1 4NS, UK 6LPC2E, CNRS and University of Orleans,´ Orleans,´ France 7Climate and Space Sciences and Engineering, University of Michigan, Ann Arbor, MI 48109, USA 8Solar System Exploration Division, NASA/Goddard Space Flight Center, Greenbelt, MD, 20771 9LESIA, Observatoire de Paris, Universit PSL, CNRS, Sorbonne Universit, Universit de Paris, 5 place Jules Janssen, 92195 Meudon, France 10Laboratory for Atmospheric and Space Physics, University of Colorado, Boulder, CO, 80303, USA 11Department of Astrophysical Sciences, Princeton University, Princeton, NJ, 08544, USA Key Points: • The Parker Solar Probe (PSP) FIELDS instrument measures millisecond volt- ages impulses associated with dust impacts • The sign of the largest monopole voltage response is a function of the spacecraft floating potential • These measurements are consistent with models of dynamic charge balance following dust impacts Submitted : June 2, 2020 arXiv:2006.00776v1 [physics.space-ph] 1 Jun 2020 Corresponding author: Stuart D. -
General Disclaimer One Or More of the Following Statements May Affect
General Disclaimer One or more of the Following Statements may affect this Document This document has been reproduced from the best copy furnished by the organizational source. It is being released in the interest of making available as much information as possible. This document may contain data, which exceeds the sheet parameters. It was furnished in this condition by the organizational source and is the best copy available. This document may contain tone-on-tone or color graphs, charts and/or pictures, which have been reproduced in black and white. This document is paginated as submitted by the original source. Portions of this document are not fully legible due to the historical nature of some of the material. However, it is the best reproduction available from the original submission. Produced by the NASA Center for Aerospace Information (CASI) NASA Technical Memorandum 85094 SOLAR RADIO BURST AND IN SITU DETERMINATION OF INTERPLANETARY ELECTRON DENSITY (NASA-^'M-85094) SOLAR RADIO BUFST AND IN N83-35989 SITU DETERMINATION OF INTEFPIAKETARY ELECTRON DENSITY SNASA) 26 p EC A03/MF A01 CSCL 03B Unclas G3/9.3 492134 J. L. Bougeret, J. H. King and R. Schwenn OCT Y'183 RECEIVED NASA Sri FACIUTY ACCESS DEPT. September 1883 I 3 National Aeronautics and Space Administration Goddard Spne Flight Center Greenbelt, Maryland 20771 k it R ^ f A SOLAR RADIO BURST AND IN SITU DETERMINATION OF INTERPLANETARY ELECTRON DENSITY J.-L. Bou eret * J.H. Kinr ^i Laboratory for Extraterrestrial Physics, NASA/Goddard Space Flight. Center, Greenbelt, Maryland 20771, U.S.A. and R. Schwenn Max-Planck-Institut fOr Aeronomie, Postfach 20, D-3411 Katlenburg-Lindau, Federal Republic of Germany - 2 - °t i t: ABSTRACT i • We review and discuss a few interplanetary electron density scales which have been derived from the analysis of interplanetary solar radio bursts, and we compare them to a model derived from 1974-1980 Helioi 1 and 2 in situ i i density observations made in the 0.3-1.0 AU range. -
Science: Planetary Science Outyears Are Notional
Science: Planetary Science Outyears are notional ($M) 2019 2020 2021 2022 2023 Planetary Science $2,235 $2,200 $2,181 $2,162 $2,143 Ø Creates a robotic Lunar Discovery and Exploration program, that supports commercial partnerships and innovative approaches to achieving human and science exploration goals. Ø Continues development of Mars 2020 and Europa Clipper. Ø Establishes a Planetary Defense program, including the Double Asteroid Redirection Test (DART) and Near-Earth Object Observations. Ø Studies a potential Mars Sample Return mission incorporating commercial partnerships. Ø Formulates the Lucy and Psyche missions. Ø Selects the next New Frontiers mission. Ø Invests in CubeSats/SmallSats that can achieve entirely new science at lower cost. Ø Operates 10 Planetary missions. § OSIRIS-REx will map asteroid Bennu. § New Horizons will fly by its Kuiper belt target. Dawn Image of Ceres on January 13, 2015 20 Science: Astrophysics Outyears are notional ($M) 2019 2020 2021 2022 2023 Astrophysics $1,185 $1,185 $1,185 $1,185 $1,185 Ø Launches the James Webb Space Telescope. Ø Moves Webb into the Cosmic Origins Program within the Astrophysics Account. Ø Terminates WFIRST due to its significant cost and higher priorities elsewhere within NASA. Increases funding for future competed missions and research. Ø Supports the TESS exoplanet mission following launch by June 2018. Ø Formulates or develops, IXPE, GUSTO, XARM, Euclid, and a new MIDEX mission to be selected in FY 2019. Ø Operates ten missions and the balloon project. Ø Invests in CubeSats/SmallSats that can achieve entirely new science at lower cost. Ø All Astrophysics missions beyond prime operations (including SOFIA) will be subject to senior review in 2019. -
Astronomy & Astrophysics a Hipparcos Study of the Hyades
A&A 367, 111–147 (2001) Astronomy DOI: 10.1051/0004-6361:20000410 & c ESO 2001 Astrophysics A Hipparcos study of the Hyades open cluster Improved colour-absolute magnitude and Hertzsprung{Russell diagrams J. H. J. de Bruijne, R. Hoogerwerf, and P. T. de Zeeuw Sterrewacht Leiden, Postbus 9513, 2300 RA Leiden, The Netherlands Received 13 June 2000 / Accepted 24 November 2000 Abstract. Hipparcos parallaxes fix distances to individual stars in the Hyades cluster with an accuracy of ∼6per- cent. We use the Hipparcos proper motions, which have a larger relative precision than the trigonometric paral- laxes, to derive ∼3 times more precise distance estimates, by assuming that all members share the same space motion. An investigation of the available kinematic data confirms that the Hyades velocity field does not contain significant structure in the form of rotation and/or shear, but is fully consistent with a common space motion plus a (one-dimensional) internal velocity dispersion of ∼0.30 km s−1. The improved parallaxes as a set are statistically consistent with the Hipparcos parallaxes. The maximum expected systematic error in the proper motion-based parallaxes for stars in the outer regions of the cluster (i.e., beyond ∼2 tidal radii ∼20 pc) is ∼<0.30 mas. The new parallaxes confirm that the Hipparcos measurements are correlated on small angular scales, consistent with the limits specified in the Hipparcos Catalogue, though with significantly smaller “amplitudes” than claimed by Narayanan & Gould. We use the Tycho–2 long time-baseline astrometric catalogue to derive a set of independent proper motion-based parallaxes for the Hipparcos members. -
A New Vla–Hipparcos Distance to Betelgeuse and Its Implications
The Astronomical Journal, 135:1430–1440, 2008 April doi:10.1088/0004-6256/135/4/1430 c 2008. The American Astronomical Society. All rights reserved. Printed in the U.S.A. A NEW VLA–HIPPARCOS DISTANCE TO BETELGEUSE AND ITS IMPLICATIONS Graham M. Harper1, Alexander Brown1, and Edward F. Guinan2 1 Center for Astrophysics and Space Astronomy, University of Colorado, Boulder, CO 80309, USA; [email protected], [email protected] 2 Department of Astronomy and Astrophysics, Villanova University, PA 19085, USA; [email protected] Received 2007 November 2; accepted 2008 February 8; published 2008 March 10 ABSTRACT The distance to the M supergiant Betelgeuse is poorly known, with the Hipparcos parallax having a significant uncertainty. For detailed numerical studies of M supergiant atmospheres and winds, accurate distances are a pre- requisite to obtaining reliable estimates for many stellar parameters. New high spatial resolution, multiwavelength, NRAO3 Very Large Array (VLA) radio positions of Betelgeuse have been obtained and then combined with Hipparcos Catalogue Intermediate Astrometric Data to derive new astrometric solutions. These new solutions indicate a smaller parallax, and hence greater distance (197 ± 45 pc), than that given in the original Hipparcos Catalogue (131 ± 30 pc) and in the revised Hipparcos reduction. They also confirm smaller proper motions in both right ascension and declination, as found by previous radio observations. We examine the consequences of the revised astrometric solution on Betelgeuse’s interaction with its local environment, on its stellar properties, and its kinematics. We find that the most likely star-formation scenario for Betelgeuse is that it is a runaway star from the Ori OB1 association and was originally a member of a high-mass multiple system within Ori OB1a. -
On Parker Solar Probe, NASA Leaves the Driving to Aerojet Rocketdyne
On Parker Solar Probe, NASA Leaves the Driving to Aerojet Rocketdyne August 12, 2018 KENNEDY SPACE CENTER, Fla., Aug. 12, 2018 (GLOBE NEWSWIRE) -- With a big assist from Aerojet Rocketdyne, NASA’s Parker Solar Probe is now on its way to humankind’s closest encounter ever with a star – in this case our solar system’s sun. Parker Solar Probe NASA image Aerojet Rocketdyne provided the full propulsion system on NASA’s Parker Solar Probe, which will venture eight times closer to the Sun than the previous record holderCredit: NASA/Johns Hopkins APL In addition to the RS-68A main engines for the United Launch Alliance Delta IV Heavy rocket that launched the Parker Probe into space, Aerojet Rocketdyne also supplied the RL10B-2 second stage engine and 12 MR-106 reaction control thrusters on the Delta Cryogenic Second Stage, as well as the full propulsion system on the Parker Solar Probe. The nearly 7-year journey will bring the probe to within 6.2 million kilometers of the Sun’s surface. That’s well within the orbit of the Sun’s nearest planet, Mercury, and eight times closer than the previous record holder, the U.S.-German Helios B probe, which made its closest approach in 1976. “Surviving a years-long journey to the corona of the Sun while operating in autonomous mode requires an incredibly high level of reliability,” said Aerojet Rocketdyne CEO and President Eileen Drake. “Aerojet Rocketdyne propulsion plays a critical role in all aspects of the Parker Solar Probe mission, from launch on the Delta IV, to the probe’s safe cruise through space and approach of the Sun’s atmosphere.” The Parker Solar Probe ultimately will dip into the Sun’s corona, carrying instruments to observe and measure the movement and interaction of phenomena including electric and magnetic fields, energetic particles and solar wind. -
The Active Region Source of a Type III Radio Storm Observed by Parker Solar Probe During Encounter 2 Log-Spaced Chunks, Each of 2.56 Mhz Wide
Astronomy & Astrophysics manuscript no. ISSI_E2_Hinode-final ©ESO 2021 February 10, 2021 The active region source of a type III radio storm observed by Parker Solar Probe during Encounter 2 L. Harra1, 2, D. H. Brooks3, S. D. Bale4, C. H. Mandrini5, 6, K. Barczynski1, 2, R. Sharma7, S. T. Badman4, S. Vargas Domínguez8, and M. Pulupa4 1 PMOD/WRC, Dorfstrasse 33 CH-7260 Davos Dorf, Switzerland e-mail: [email protected] e-mail: [email protected] 2 ETH-Zurich, Hönggerberg campus, HIT building, Zürich, Switzerland 3 College of Science, George Mason University, 4400 University Drive, Fairfax, VA 22030 USA e-mail: [email protected] 4 Physics Department and Space Sciences Laboratory, University of California, Berkeley, USA. 94720-7450 e-mail: [email protected] 5 Instituto de Astronomía y Física del Espacio (IAFE), CONICET-UBA, Buenos Aires, Argentina 6 Facultad de Ciencias Exactas y Naturales (FCEN), UBA, Buenos Aires, Argentina e-mail: [email protected] 7 Fachhochschule Nordwestschweiz (FHNW), Bahnhofstrasse 6, 5210 Windisch, Switzerland e-mail: [email protected] 8 Universidad Nacional de Colombia, Observatorio Astronómico Nacional, Bogotá, Colombia e-mail: [email protected] Received September 2020 ABSTRACT Context. To investigate the source of a type III radio burst storm during encounter 2 of NASA’s Parker Solar Probe (PSP) mission. Aims. It was observed that in encounter 2 of NASA’s Parker Solar Probe mission there was a large amount of radio activity, and in particular a noise storm of frequent, small type III bursts from 31st March to 6th April 2019. Our aim is to investigate the source of these small and frequent bursts. -
Michael Perryman
Michael Perryman Cavendish Laboratory, Cambridge (1977−79) European Space Agency, NL (1980−2009) (Hipparcos 1981−1997; Gaia 1995−2009) [Leiden University, NL,1993−2009] Max-Planck Institute for Astronomy & Heidelberg University (2010) Visiting Professor: University of Bristol (2011−12) University College Dublin (2012−13) Lecture program 1. Space Astrometry 1/3: History, rationale, and Hipparcos 2. Space Astrometry 2/3: Hipparcos science results (Tue 5 Nov) 3. Space Astrometry 3/3: Gaia (Thu 7 Nov) 4. Exoplanets: prospects for Gaia (Thu 14 Nov) 5. Some aspects of optical photon detection (Tue 19 Nov) M83 (David Malin) Hipparcos Text Our Sun Gaia Parallax measurement principle… Problematic from Earth: Sun (1) obtaining absolute parallaxes from relative measurements Earth (2) complicated by atmosphere [+ thermal/gravitational flexure] (3) no all-sky visibility Some history: the first 2000 years • 200 BC (ancient Greeks): • size and distance of Sun and Moon; motion of the planets • 900–1200: developing Islamic culture • 1500–1700: resurgence of scientific enquiry: • Earth moves around the Sun (Copernicus), better observations (Tycho) • motion of the planets (Kepler); laws of gravity and motion (Newton) • navigation at sea; understanding the Earth’s motion through space • 1718: Edmond Halley • first to measure the movement of the stars through space • 1725: James Bradley measured stellar aberration • Earth’s motion; finite speed of light; immensity of stellar distances • 1783: Herschel inferred Sun’s motion through space • 1838–39: Bessell/Henderson/Struve -
Cmes, Solar Wind and Sun-Earth Connections: Unresolved Issues
CMEs, solar wind and Sun-Earth connections: unresolved issues Rainer Schwenn Max-Planck-Institut für Sonnensystemforschung, Katlenburg-Lindau, Germany [email protected] In recent years, an unprecedented amount of high-quality data from various spaceprobes (Yohkoh, WIND, SOHO, ACE, TRACE, Ulysses) has been piled up that exhibit the enormous variety of CME properties and their effects on the whole heliosphere. Journals and books abound with new findings on this most exciting subject. However, major problems could still not be solved. In this Reporter Talk I will try to describe these unresolved issues in context with our present knowledge. My very personal Catalog of ignorance, Updated version (see SW8) IAGA Scientific Assembly in Toulouse, 18-29 July 2005 MPRS seminar on January 18, 2006 The definition of a CME "We define a coronal mass ejection (CME) to be an observable change in coronal structure that occurs on a time scale of a few minutes and several hours and involves the appearance (and outward motion, RS) of a new, discrete, bright, white-light feature in the coronagraph field of view." (Hundhausen et al., 1984, similar to the definition of "mass ejection events" by Munro et al., 1979). CME: coronal -------- mass ejection, not: coronal mass -------- ejection! In particular, a CME is NOT an Ejección de Masa Coronal (EMC), Ejectie de Maså Coronalå, Eiezione di Massa Coronale Éjection de Masse Coronale The community has chosen to keep the name “CME”, although the more precise term “solar mass ejection” appears to be more appropriate. An ICME is the interplanetry counterpart of a CME 1 1. -
Astrometry and Optics During the Past 2000 Years
1 Astrometry and optics during the past 2000 years Erik Høg Niels Bohr Institute, Copenhagen, Denmark 2011.05.03: Collection of reports from November 2008 ABSTRACT: The satellite missions Hipparcos and Gaia by the European Space Agency will together bring a decrease of astrometric errors by a factor 10000, four orders of magnitude, more than was achieved during the preceding 500 years. This modern development of astrometry was at first obtained by photoelectric astrometry. An experiment with this technique in 1925 led to the Hipparcos satellite mission in the years 1989-93 as described in the following reports Nos. 1 and 10. The report No. 11 is about the subsequent period of space astrometry with CCDs in a scanning satellite. This period began in 1992 with my proposal of a mission called Roemer, which led to the Gaia mission due for launch in 2013. My contributions to the history of astrometry and optics are based on 50 years of work in the field of astrometry but the reports cover spans of time within the past 2000 years, e.g., 400 years of astrometry, 650 years of optics, and the “miraculous” approval of the Hipparcos satellite mission during a few months of 1980. 2011.05.03: Collection of reports from November 2008. The following contains overview with summary and link to the reports Nos. 1-9 from 2008 and Nos. 10-13 from 2011. The reports are collected in two big file, see details on p.8. CONTENTS of Nos. 1-9 from 2008 No. Title Overview with links to all reports 2 1 Bengt Strömgren and modern astrometry: 5 Development of photoelectric astrometry including the Hipparcos mission 1A Bengt Strömgren and modern astrometry .. -
Delta IV Parker Solar Probe Mission Booklet
A United Launch Alliance (ULA) Delta IV Heavy what is the source of high-energy solar particles. MISSION rocket will deliver NASA’s Parker Solar Probe to Parker Solar Probe will make 24 elliptical orbits an interplanetary trajectory to the sun. Liftoff of the sun and use seven flybys of Venus to will occur from Space Launch Complex-37 at shrink the orbit closer to the sun during the Cape Canaveral Air Force Station, Florida. NASA seven-year mission. selected ULA’s Delta IV Heavy for its unique MISSION ability to deliver the necessary energy to begin The probe will fly seven times closer to the the Parker Solar Probe’s journey to the sun. sun than any spacecraft before, a mere 3.9 million miles above the surface which is about 4 OVERVIEW The Parker percent the distance from the sun to the Earth. Solar Probe will At its closest approach, Parker Solar Probe will make repeated reach a top speed of 430,000 miles per hour journeys into the or 120 miles per second, making it the fastest sun’s corona and spacecraft in history. The incredible velocity trace the flow of is necessary so that the spacecraft does not energy to answer fall into the sun during the close approaches. fundamental Temperatures will climb to 2,500 degrees questions such Fahrenheit, but the science instruments will as why the solar remain at room temperature behind a 4.5-inch- atmosphere is thick carbon composite shield. dramatically Image courtesy of NASA hotter than the The mission was named in honor of Dr. -
Radial Variation of the Interplanetary Magnetic Field Between 0.3 AU and 1.0 AU
|00000575|| J. Geophys. 42, 591 - 598, 1977 Journal of Geophysics Radial Variation of the Interplanetary Magnetic Field between 0.3 AU and 1.0 AU Observations by the Helios-I Spacecraft G. Musmann, F.M. Neubauer and E. Lammers Institut for Geophysik and Meteorologie, Technische Universitiit Braunschweig, Mendelssohnstr. lA, D-3300 Braunschweig, Federal Republic of Germany Abstract. We have investigated the radial dependence of the radial and azimuthal components and the magnitude of the interplanetary magnetic field obtained by the Technical University of Braunschweig magnetometer experiment on-board of Helios-1 from December 10, 1974 to first perihelion on March 15, 1975. Absolute values of daily averages of each quantity have been employed. The regression analysis based on power laws leads to 2.55 y x r- 2 · 0 , 2.26 y x r- i.o and F = 5.53 y x r- i. 6 with standard deviations of 2.5 y, 2.0 y and 3.2 y for the radial and azimuthal components and magnitude, respectively. Here r is the radial distance from the sun in astronomical units. The results are compared with results obtained for Mariners 4, 5 and 10 and Pioneers 6 and 10. The differences are probably due to different epochs in the solar cycle and the different statistical techniques used. Key words: Interplanetary magnetic field - Helios-1 results. Introduction The study of the vanat10n of the components and magnitude of the in terplanetary magnetic field with heliocentric distance is very intersting at the present time. The mission of Mariner 10 to the inner solar system to a heliocentric distance of 0.46 AU and the missions of Pioneer 10 and Pioneer 11 to the outer solar system to heliocentric distances beyond 5 AU have provided new data over a wide range of heliocentric distance.