Lunar and Planetary Information Bulletin, Issue
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Shock Connectivity and the Late Cycle 24 Solar Energetic Particle Events in July and September 2017
Shock Connectivity and the Late Cycle 24 Solar Energetic Particle Events in July and September 2017 J.G. Luhmann1, M.L. Mays2, Yan Li1, C.O. Lee1, H. Bain3, D. Odstrcil4, R.A. Mewaldt5, C.M.S. Cohen5, D. Larson1, Gordon Petrie6 1Space Sciences Laboratory, University of California, Berkeley. 2CCMC, NASA Goddard Space Flight Center. 3NOAA Space Weather Prediction Center. 4George Mason University. 5California Institute of Technology. 6NSO. Corresponding author: Janet Luhmann ([email protected]) Key Points: Observer shock connectivity explains the SEP observations during the July and September 2017 events. The July and September 2017 solar and SEP events had similar characteristics due to similar source region and eruptions. The July and September 2017 events seemed to arise in conjunction with the appearance of a pseudostreamer, a possible alternate ICME source. This article has been accepted for publication and undergone full peer review but has not been through the copyediting, typesetting, pagination and proofreading process which may lead to differences between this version and the Version of Record. Please cite this article as doi: 10.1029/2018SW001860 © 2018 American Geophysical Union. All rights reserved. Abstract As solar activity steadily declined toward the cycle 24 minimum in the early months of 2017, the expectation for major Solar Energetic Particle (SEP) events diminished with the sunspot number. It was thus surprising (though not unprecedented) when a new, potentially significant active region rotated around the East limb in early July that by mid-month was producing a series of coronal eruptions, reaching a crescendo around July 23. This series, apparently associated with the birth of a growing pseudostreamer, produced the largest SEP event(s) seen since the solar maximum years. -
Glossary Glossary
Glossary Glossary Albedo A measure of an object’s reflectivity. A pure white reflecting surface has an albedo of 1.0 (100%). A pitch-black, nonreflecting surface has an albedo of 0.0. The Moon is a fairly dark object with a combined albedo of 0.07 (reflecting 7% of the sunlight that falls upon it). The albedo range of the lunar maria is between 0.05 and 0.08. The brighter highlands have an albedo range from 0.09 to 0.15. Anorthosite Rocks rich in the mineral feldspar, making up much of the Moon’s bright highland regions. Aperture The diameter of a telescope’s objective lens or primary mirror. Apogee The point in the Moon’s orbit where it is furthest from the Earth. At apogee, the Moon can reach a maximum distance of 406,700 km from the Earth. Apollo The manned lunar program of the United States. Between July 1969 and December 1972, six Apollo missions landed on the Moon, allowing a total of 12 astronauts to explore its surface. Asteroid A minor planet. A large solid body of rock in orbit around the Sun. Banded crater A crater that displays dusky linear tracts on its inner walls and/or floor. 250 Basalt A dark, fine-grained volcanic rock, low in silicon, with a low viscosity. Basaltic material fills many of the Moon’s major basins, especially on the near side. Glossary Basin A very large circular impact structure (usually comprising multiple concentric rings) that usually displays some degree of flooding with lava. The largest and most conspicuous lava- flooded basins on the Moon are found on the near side, and most are filled to their outer edges with mare basalts. -
The Van Allen Probes' Contribution to the Space Weather System
L. J. Zanetti et al. The Van Allen Probes’ Contribution to the Space Weather System Lawrence J. Zanetti, Ramona L. Kessel, Barry H. Mauk, Aleksandr Y. Ukhorskiy, Nicola J. Fox, Robin J. Barnes, Michele Weiss, Thomas S. Sotirelis, and NourEddine Raouafi ABSTRACT The Van Allen Probes mission, formerly the Radiation Belt Storm Probes mission, was renamed soon after launch to honor the late James Van Allen, who discovered Earth’s radiation belts at the beginning of the space age. While most of the science data are telemetered to the ground using a store-and-then-dump schedule, some of the space weather data are broadcast continu- ously when the Probes are not sending down the science data (approximately 90% of the time). This space weather data set is captured by contributed ground stations around the world (pres- ently Korea Astronomy and Space Science Institute and the Institute of Atmospheric Physics, Czech Republic), automatically sent to the ground facility at the Johns Hopkins University Applied Phys- ics Laboratory, converted to scientific units, and published online in the form of digital data and plots—all within less than 15 minutes from the time that the data are accumulated onboard the Probes. The real-time Van Allen Probes space weather information is publicly accessible via the Van Allen Probes Gateway web interface. INTRODUCTION The overarching goal of the study of space weather ing radiation, were the impetus for implementing a space is to understand and address the issues caused by solar weather broadcast capability on NASA’s Van Allen disturbances and the effects of those issues on humans Probes’ twin pair of satellites, which were launched in and technological systems. -
CEAS Quarterly Bulletin Talented Engineers Are Needed
The Quarterly Bulletin of the COUNCIL OF EUROPEAN AEROSPACE SOCIETIES 3AF– AIAE– AIDAA– DGLR– FSAE– FTF– HAES– NVvL– RAeS– SVFW–TsAGI • GENERAL • AERONAUTICS • SPACE • Issue 2 – 2009 • June • Editorial INVESTING IN YOUTH The future of Europe is in the hands of its youth: this is a basic truth. However, surprisingly, while we are full in course of the election campaign for the renewal of the European Parliament, we hear almost nothing about education and culture, and we see no proposals from the candidates on how to prepare the students and young professionals to live in an increasingly integrated Europe. The question is a very broad and difficult one, due to the large number of Member States and the diversity of languages and cultures; but this is all the more reason to concentrate great efforts on it. In the aerospace sector, the projects, more and more complex, are developed across several national borders and include the highest technologies. So, to overcome the Jean-Pierre Sanfourche numerous challenges which confront us in a fierce world-wide aerospace market, Editor-in-Chief, CEAS Quarterly Bulletin talented engineers are needed. Unfortunately, in the past two or three decades within Europe, there have been clear indications that the most brilliant students pre- fer careers in business and finance to those in science, technology and engineering. Action is clearly necessary to reverse this trend by taking the measures that will CONTENTS allow us to attract and then retain the best talent in the air and space activities. The GENERAL Pages organising Committee of the upcoming CEAS2009 Air & Space Conference in Manchester has taken an important step in this direction by including in the • The ASD President’s message 2 Conference agenda the launch of a new European Young Aerospace Professional • The life of the CEAS 4 (EYAP) forum. -
(50000) Quaoar, See Quaoar (90377) Sedna, See Sedna 1992 QB1 267
Index (50000) Quaoar, see Quaoar Apollo Mission Science Reports 114 (90377) Sedna, see Sedna Apollo samples 114, 115, 122, 1992 QB1 267, 268 ap-value, 3-hour, conversion from Kp 10 1996 TL66 268 arcade, post-eruptive 24–26 1998 WW31 274 Archimedian spiral 11 2000 CR105 269 Arecibo observatory 63 2000 OO67 277 Ariel, carbon dioxide ice 256–257 2003 EL61 270, 271, 273, 274, 275, 286, astrometric detection, of extrasolar planets – mass 273 190 – satellites 273 Atlas 230, 242, 244 – water ice 273 Bartels, Julius 4, 8 2003 UB313 269, 270, 271–272, 274, 286 – methane 271–272 Becquerel, Antoine Henry 3 – orbital parameters 271 Biermann, Ludwig 5 – satellite 272 biomass, from chemolithoautotrophs, on Earth 169 – spectroscopic studies 271 –, – on Mars 169 2005 FY 269, 270, 272–273, 286 9 bombardment, late heavy 68, 70, 71, 77, 78 – atmosphere 273 Borealis basin 68, 71, 72 – methane 272–273 ‘Brown Dwarf Desert’ 181, 188 – orbital parameters 272 brown dwarfs, deuterium-burning limit 181 51 Pegasi b 179, 185 – formation 181 Alfvén, Hannes 11 Callisto 197, 198, 199, 200, 204, 205, 206, ALH84001 (martian meteorite) 160 207, 211, 213 Amalthea 198, 199, 200, 204–205, 206, 207 – accretion 206, 207 – bright crater 199 – compared with Ganymede 204, 207 – density 205 – composition 204 – discovery by Barnard 205 – geology 213 – discovery of icy nature 200 – ice thickness 204 – evidence for icy composition 205 – internal structure 197, 198, 204 – internal structure 198 – multi-ringed impact basins 205, 211 – orbit 205 – partial differentiation 200, 204, 206, -
Navigation Challenges During Exomars Trace Gas Orbiter Aerobraking Campaign
NON-PEER REVIEW Please select category below: Normal Paper Student Paper Young Engineer Paper Navigation Challenges during ExoMars Trace Gas Orbiter Aerobraking Campaign Gabriele Bellei 1, Francesco Castellini 2, Frank Budnik 3 and Robert Guilanyà Jané 4 1 DEIMOS Space located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 2 Telespazio VEGA located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 3 ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany 4 GMV INSYEN located at ESA/ESOC, Robert-Bosch-Str. 5, Darmstadt, 64293, Germany Abstract The ExoMars Trace Gas Orbiter satellite spent one year in aerobraking operations at Mars, lowering its orbit period from one sol to about two hours. This delicate phase challenged the operations team and in particular the navigation system due to the highly unpredictable Mars atmosphere, which imposed almost continuous monitoring, navigation and re-planning activities. An aerobraking navigation concept was, for the first time at ESA, designed, implemented and validated on-ground and in-flight, based on radiometric tracking data and complemented by information extracted from spacecraft telemetry. The aerobraking operations were successfully completed, on time and without major difficulties, thanks to the simplicity and robustness of the selected approach. This paper describes the navigation concept, presents a recollection of the main in-flight results and gives a retrospective of the main lessons learnt during this activity. Keywords: ExoMars, Trace Gas Orbiter, aerobraking, navigation, orbit determination, Mars atmosphere, accelerometer Introduction The ExoMars program is a cooperation between the European Space Agency (ESA) and Roscosmos for the robotic exploration of the red planet. -
A Clearer Final Frontier of the Sentinel Family of Earth-Monitoring Satellites
COMMENT BOOKS & ARTS Station. His examination of other astro- nomical and exploration cooperation efforts is somewhat cursory, and there are small errors. The Rosetta mission of the Euro- pean Space Agency (ESA), for instance, is ROGER HARRIS/SPL not a solar mission, but instead will rendez- vous with and observe a comet. The lunar probe Chandrayaan-1 was a collaboration between India, ESA, NASA and Bulgaria; and unmentioned is the ground-breaking Double Star Sino-European joint mission. Failures in cooperation offer many lessons, and Moltz looks at the International Solar Polar Mission almost 25 years ago, as well as the United States’ 2012 pull-out from collaboration with ESA on Mars explora- tion. However, he misses the pivotal case of the International Gamma-Ray Laboratory (INTEGRAL), launched in 2002, the absence of expected levels of US support for which led to the first close ESA Science Programme cooperation with Russia. The distinction between cooperation and competition had, however, emerged decades before, with US refusal to launch the Franco-German com- munications satellite Symphonie. Europe learnt that it had to go it alone in using space for commercial or near-to-market purposes. Satellite deployment must be regulated to keep space usable and safe. Moltz accepts that space is important to commerce, but readers might query whether SPACE POLICY he sees how this may drive regulation. The European Union, the largest economic grouping in the world, is this year launching multiple spacecraft; these include members A clearer final frontier of the Sentinel family of Earth-monitoring satellites. The move is economic, and the use David Southwood finds that a study on safeguarding of space is evolving and increasingly focused space is shorter on cooperation than conflict. -
"I Think You Need a Pioneering Spirit in Society, a Frontier Spirit."
The Profile "I think you need a pioneering spirit in society, a frontier spirit." “There is a limit to how far I should, Professor David Southwood is the personally, because I feel like I am a general Director of Science in ESA, a post he has advancing on a wide front, and there is nothing that tells me that I should advance first on one front. I had for almost two years. During these have got to advance on many fronts. As a result, the two years he has made his mark through organised way to do it, like a general, is to advance the Cosmic Vision, engaging in finding new your forces on one front, make sure they have got the resources and backup, and then advance on other ways to explore space within ESA. fronts, consolidating, and so on. In other words, we cannot advance on all fronts at the same time. But by Nordic Space Activities met David having a plan we can advance on all fronts in time. I think there is nothing that can tell me there is one Southwood at ESTEC early this April, branch of science in need of Europe’s attention and asked him: entirely. Europe is too big a collection of counties to simply say it does only one kind of space science. It Today you talked about the Cosmic Vision, the should cover the frontier.” new way to go for European space research. Are the large resources that have been used for space The space research budgets have steadily research necessary to secure the future development decreased the last few years. -
Living with a Star Targeted Research and Technology (TR&T) Steering
Living with a Star Targeted Research and Technology (TR&T) Steering Committee Steering Committee Members: Liaison Members: Co-Chair: Eftyhia Zesta (GSFC) Terry Onsager (NOAA) Co-Chair: Mark Linton (NRL) Rodney Vierick (NOAA) Yuri Shprits (MIT) Ilia Roussev (NSF) Scott McIntosh (NCAR / HAO) Vyacheslav Lukin (NSF) Nathan Schwadron (UNH ex-chair) Masha Kuznetsova (GSFC / Community Karel Schrijver (Lockheed Martin) Coordinated Modeling Center) Jim Slavin (U Michigan) Mona Kessel (NASA HQ / Chadi Salem (UC Berkeley) Van Allen Probes) Alexa Halford (GSFC) Dean Pesnell (GSFC / Pontus Brandt (APL) Solar Dynamics Observatory) Tim Bastian (NRAO) David Sibeck (GSFC / Van Allen Probes) Kent Tobiska Adam Szabo (GSFC / Solar Probe Plus) (Space Environment Tech.) Chris St. Cyr (GSFC / Solar Orbiter) LWS Program Ex Officio: Elsayed Talaat & Jeff Morrill (NASA HQ), Shing Fung (GSFC) 2003 Science Definition Team Report: Living with a Star Objectives LWS initiative: goal-oriented research program targeting those aspects of the Sun-Earth system that directly affect life and society. The objectives of LWS will advance research in Sun-Earth system science to new territory, producing knowledge and understanding that society can ultimately utilize. 2003 LWS Science Definition Team Report: TR&T Program The Targeted Research and Technology (TR&T) component of LWS provides the theory, modeling, and data analysis necessary to enable an integrated, system-wide picture of Sun-Earth connection science with societal relevance. Science Definition Team (SDT) … formed -
Initial Maven Observations of Ion Cyclotron Waves and Pickup Protons: a Measurement of Hydrogen Loss in the Upper Martian Exosphere F
46th Lunar and Planetary Science Conference (2015) 2628.pdf INITIAL MAVEN OBSERVATIONS OF ION CYCLOTRON WAVES AND PICKUP PROTONS: A MEASUREMENT OF HYDROGEN LOSS IN THE UPPER MARTIAN EXOSPHERE F. J. Crary1, J. E. P. Connerney2, J. R. Espley3 and J. P. McFadden4, 1Laboratory for Space and Atmospheric Physics, University of Col- orado, Boulder, 1234 Innovation Dr., Boulder, CO, 80303, [email protected] 2Goddard Space Flight Center, Mail Code 695, Greenbelt, MD, 20771, [email protected] 3Goddard Space Flight Center, Mail Code 695, Greenbelt, MD, 20771, [email protected], 4Space Science Laboratory, University of California, Berkeley, 7 Gauss Way, Berkeley, CA 94720-7450, [email protected]. Introduction: Observations by the Mars Global Surveyor, Mars Express and Phobos 2 spacecraft [1],[2],[3] have shown that Mars has a hydrogen exo- sphere which extends as much as ten Martian radii from the planet. These hydrogen atoms ionize and are “picked up” in the solar wind flow. Neither the associ- ated hydrogen loss rate nor the structure of this extend- ed exosphere, have previously been well determined. The resulting pickup protons have a distinctive veloci- ty distribution and generate low frequency electromag- netic waves near the ion cyclotron frequency. Proton pickup ions have been observed by Mars Express [4] and proton cyclotron waves have been observed by Mars Global Surveyor [2]. The MAVEN spacecraft is the first Mars orbiter able to simultane- ously measure both ion cyclotron waves. Data from the spacecraft’s magnetometer [5], providing the vector magnetic field at a rate of 32 samples per second, is Fourier transformed to produce dynamic spectra of right-circularly polarized (whistler mode) and left- circularly polarized (ion cyclotron mode) ultralow fre- quency electromagnetic waves. -
OVERVIEW of the PHOENIX MARS LANDER MISSION. P. H. Smith1, 1Lunar and Planetary Lab, University of Arizona, Tucson, AZ 85721, [email protected]
Martian Sulfates as Recorders of Atmospheric-Fluid-Rock Interactions (2006) 7069.pdf OVERVIEW OF THE PHOENIX MARS LANDER MISSION. P. H. Smith1, 1Lunar and Planetary Lab, University of Arizona, Tucson, AZ 85721, [email protected]. Introduction: The Phoenix lander is ples of this biological paydirt and test for the next mission to study the surface of signatures related to biology. Mars in situ. By studying the active water Baseline Mission: After the initial as- cycles in the polar region, it complements sessment of the landing site by the science the Mars Exploration Rovers that look at team, the primary science phase of the the ancient history of Mars contained in mission begins with the collection of sur- the solid rocks. Lacking mobility, Phoenix face samples. Two major science instru- explores the subsurface to the north of the ments receive and analyze the samples. lander, studying the mineralogy and The first is the thermal evolved gas ana- chemistry of the soils and ice. lyzer (TEGA). A sample is delivered to a Scientific Objectives, Phoenix Follows hopper that feeds a small amount of soil the Water: The Phoenix mission targets into a tiny oven, which is sealed and the northern plains between 65 and 72 N. heated slowly to temperatures approaching High-resolution images from the Mars Or- 1000 C. The heater power profile neces- biter Camera on the Mars Global Surveyor sary to maintain a constant temperature spacecraft show a “basketball-like” texture gradient contains peaks and valleys that on the surface with low hummocks spaced indicate phase transitions. For instance, 10’s of meters apart; polygonal terrain, or ice will show a feature at its melting point patterned ground, is also common. -
Sentinelssentinels
SentinelsSentinels This LWS program element includes the Inner Heliospheric Sentinels (IHS) and the Far Side Sentinel (FSS) missions, each with its own distinct concept. And post o’er land and ocean without rest, They also serve who only stand and wait. On His Blindness Goddard Space Flight Center John Milton SentinelsSentinels StudyStudy ChronologyChronology Date Event Concept 1/13/00 Sentinels Briefing By A. Szabo Far Side Observer, L1 Cluster, NG STEREO 1/20/00 Preformulation Team Meeting Imaging/In-Situ Libration Point Measurements 2/2/00 Preformulation Team Meeting Emphasis On Heliospheric Elements 2/3/00 to 3/31/00 Libration Point Orbit Studies Orbit Trajectory Options 3/31/00 Preformulation Team Meeting Far Side Sentinel/4 Inner Heliospheric Sentinels 4/6/00 Sentinels Workshop 4 Satellite Constellation/Far Side Options 4/7/00 JPL Preliminary FSS Concept 3-Axis Spacecraft/5 Instruments/1 Launch 4/10/00 IMDC IHS Briefing 4 Spinning Satellites/4 Instruments/1 Launch 4/17/00 to 4/20/00 IMDC IHS Study 4 Spinning Satellites/4 Instruments/1 Launch 4/20/00 to 4/27/00 JPL FSS Concept/Cost Update Custom Spacecraft/5 Instruments/1 Launch 4/21/00 to 5/5/00 GSFC Mission Costing Far Side Sentinel/4 Inner Heliospheric Sentinels 5/25/00 FSS Mission Concept Summary Defined In Attached System/Subsystem Charts 5/31/00 Program Operating Plan Costed As Two Separate Missions Goddard Space Flight Center SentinelsSentinels ConceptConcept EvolutionEvolution LWS scientists initially considered a complement of spacecraft for the Sentinels mission that included a spacecraft observing the far side of the Sun, a cluster of satellites at L1, and two next-generation STEREO spacecraft.