Asteroid G-2 Experiments: New Fifth Force and Ultralight Dark Sector Tests
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Impact of Satellite Constellations on Optical Astronomy and Recommendations Toward Mitigations”
Appendices to “Impact of Satellite Constellations on Optical Astronomy and Recommendations Toward Mitigations” https://www.noirlab.edu/public/products/techdocs/techdoc004/ Table of Contents Introduction 4 Appendix A. Technical Report on Observations of Satellite Constellations 5 A. Summary and Recommendations 5 B. Introduction 6 C. Observations Details 7 D. Observations to Date 10 E. Data Analysis and Results 16 F. Lessons Learned 20 G. Future Observations 21 1. Goals and Expectations 21 2. Plans and Possible Observation Coordination/Networks 21 References 23 Appendix B. Technical Report on Simulations on Impacts of Satellite Constellations 24 A. Summary 24 B. Recommendations for Future Work 26 C. Simulations Working Group Report 26 D. Simulations of Starlinks on orbit 37 References 39 Appendix B.1: Technical Appendix: Simulation Details 40 References 48 Appendix C. Technical Report on Mitigations of Impacts of Satellite Constellations 49 A. Summary 49 B. The main recommendations of the Mitigations WG 49 C. Representative science cases 50 D. Mitigation categories 51 1. Laboratory investigations of sensor response to bright LEOsat trails, understanding this via device physics and camera models, and exploration of sensor clocking mitigations 51 2. Development of pixel processing algorithms for suppression of these effects, validation via simulation and lab data, culminating in a goal for satellite brightness 52 3. Measures to darken SpaceX Starlink LEOsats to meet this 7th mag brightness goal, including recent observations of DarkSat 53 4. Observation validation of these efforts, leading to further darkening experiments and some understanding of apparent brightness as a function of phase angle and other variables 55 2 5. -
Characterization of the June Epsilon Ophiuchids Meteoroid Stream And
Astronomy & Astrophysics manuscript no. aa37727-20 c ESO 2020 April 7, 2020 Characterization of the June epsilon Ophiuchids meteoroid stream and the comet 300P/Catalina Pavol Matlovicˇ1, Leonard Kornoš1, Martina Kovácovᡠ1, Juraj Tóth1, and Javier Licandro2;3 1 Faculty of Mathematics, Physics and Informatics, Comenius University, Bratislava, Slovakia e-mail: [email protected] 2 Instituto de Astrofísica de Canarias (IAC), C/Vía Láctea sn, 38205 La Laguna, Spain 3 Departamento de Astrofísica, Universidad de La Laguna, 38206 La Laguna, Tenerife, Spain Received 2020 ABSTRACT Aims. Prior to 2019, the June epsilon Ophiuchids (JEO) were known as a minor unconfirmed meteor shower with activity that was considered typically moderate for bright fireballs. An unexpected bout of enhanced activity was observed in June 2019, which even raised the possibility that it was linked to the impact of the small asteroid 2019 MO near Puerto Rico. Early reports also point out the similarity of the shower to the orbit of the comet 300P/Catalina. We aim to analyze the orbits, emission spectra, and material strengths of JEO meteoroids to provide a characterization of this stream, identify its parent object, and evaluate its link to the impacting asteroid 2019 MO. Methods. Our analysis is based on a sample of 22 JEO meteor orbits and four emission spectra observed by the AMOS network at the Canary Islands and in Chile. The meteoroid composition was studied by spectral classification based on relative intensity ratios of Na, Mg, and Fe. Heliocentric orbits, trajectory parameters, and material strengths were determined for each meteor and the mean orbit and radiant of the stream were calculated. -
A New Approach to Stellar Occultations in the Gaia Era Joao Ferreira
A new approach to stellar occultations in the Gaia era Joao Ferreira To cite this version: Joao Ferreira. A new approach to stellar occultations in the Gaia era. Astrophysics [astro-ph]. Université Côte d’Azur; Universidade de Lisboa. Faculdade de ciências (Lisboa, Portugal), 2020. English. NNT : 2020COAZ4084. tel-03185433 HAL Id: tel-03185433 https://tel.archives-ouvertes.fr/tel-03185433 Submitted on 30 Mar 2021 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. THÈSE DE DOCTORAT Occultations stellaires: une nouvelle approche grâce à la mission Gaia João FERREIRA Laboratoire J-L. Lagrange – Observatoire de la Côte d’Azur ; Instituto de Astrofísica e Ciências do Espaço, Lisboa Présentée en vue de l’obtention Devant le jury, composé de : du grade de docteur en Sciences de la Planète Felipe BRAGA-RIBAS (Universidade Tecnológica Federal do et de l’Univers Paraná) d’Université Côte d’Azur René DUFFARD (Instituto de Astrofisica de Andalucía) et de Faculdade de Ciências da Universidade de Guy LIBOUREL (Université Côte d’Azur) Lisboa Pedro MACHADO (Instituto -
Non-Principal Axis Rotation in Binary Asteroid Systems and How It Weakens the BYORP Effect
Non-principal axis rotation in binary asteroid systems and how it weakens the BYORP effect Alice C. Quillena,∗, Anthony LaBarcaa, YuanYuan Chenb aDepartment of Physics and Astronomy, University of Rochester, Rochester, NY 14627, USA bKey Laboratory of Planetary Sciences, Purple Mountain Observatory, Chinese Academy of Sciences, Nanjing 210008, China Abstract Using viscoelastic mass/spring model simulations, we explore tidal evolution and migration of compact binary asteroid systems. We find that after the secondary is captured into a spin-synchronous state, non-principal axis rotation in the secondary can be long-lived. The secondary's long axis can remain approximately aligned along the vector connecting secondary to primary while the secondary rocks back and forth about its long axis. Inward orbital semi-major axis migration can also resonantly excite non-principal axis rotation. By estimating solar radiation forces on triangular surface meshes, we show that the magnitude of the BYORP effect induced torque is sensitive to the secondary's spin state. Non-principal axis rotation within the 1:1 spin-orbit resonance can reduce the BYORP torque or cause frequent reversals in its direction. 1. Introduction Orbital eccentricity could cause an elongated secondary to tumble, delaying BYORP drift-induced evolution and ex- The field of research on binary asteroids currently has tending the lifetime of NEA binaries (Naidu and Margot, two dynamical conundrums. Light curve based estimates 2015). of viscoelastic behavior in single asteroids based on tum- -
Joan Coronado Escudero Enunciat TFG
Titulació: Màster Universitari en Enginyeria Aeronàutica Alumne (nom i cognoms): Joan Coronado Escudero Enunciat TFG / TFM: Economics of the exploitation of the resources in celestial bodies Director/a del TFG / TFM: Stéphanie Lizy-Destrez Codirector/a del TFG / TFM: José de Sousa Convocatòria de lliurament del TFG / TFM: 2n Quadrimestre curs 2018-2019 PROJET DE FIN D’ETUDES Joan CORONADO ESCUDERO 2018 - 2019 Economics of the exploitation of the resources in celestial bodies Internship tutor Name and address of the José DE SOUSA organisation Internship and University manager RITM Stéphanie LIZY-DESTREZ Faculté Jean Monnet Internship duration April - October 2019 54, Boulevard Desgranges 92330 SCEAUX Table of contents 1 Introduction . .1 2 The economic value of asteroids . .2 2.1 Asteroid composition . .2 2.2 Asteroid mass estimation . .7 2.3 Market price . .7 3 The economic distance of asteroids . .8 3.1 Tsiolkovsky’s rocket equation . .8 3.2 The Earth-Moon Circular Restricted Three Body Problem . .9 3.3 ∆v optimisation algorithm . 17 4 The gravity trade model . 33 5 Conclusions . 34 Appendices 42 A Economic value . 42 A.1 Meteorite elemental mass fractions . 42 A.2 Elemental market price . 43 A.3 Asteroid total economic sizes . 45 B Economic distance . 46 B.1 Optimal total ∆v values . 46 B.2 Most optimal trajectories . 67 C Gravity model . 87 C.1 Favourability factor values . 87 D Matlab code . 88 D.1 Asteroid_deltav_calculator . 88 D.2 Lagrange_solver_adim . 94 D.3 preliminary_solver . 94 D.4 odezero_EARTHSOI . 96 D.5 syn2scECLIPJ2000 . 97 D.6 load_kernels . 99 D.7 load_kernels_alt . 99 D.8 unload_kernels_alt . -
July 2019 BRAS Newsletter
A th Monthly Meeting July 8 at 7PM at HRPO (Monthly meetings are on 2nd Mondays, Highland Road Park Observatory). Program: Viewing of NASA’s The Eagle Has Landed video, after which members can discuss and share personal memories of Apollo 11 (and other) missions. What's In This Issue? President’s Message Secretary's Summary Outreach Report Astrophotography Group Asteroid and Comet News Light Pollution Committee Report Globe at Night Member’s Corner – Conner Matherne’s Astral Visions Messages from the HRPO Science Academy Friday Night Lecture Series APOLLO EVENTS Observing Notes: OphiuchusThe Serpent Bearer or Handler & Mythology Like this newsletter? See PAST ISSUES online back to 2009 Visit us on Facebook – Baton Rouge Astronomical Society Newsletter of the Baton Rouge Astronomical Society Page 2 July 2019 © 2019 President’s Message July 20, 2019 will mark the 50th anniversary of the Apollo 11 Moon Landing, one of the great milestones of United States and World History. Our meeting on Monday, July 8th involves inviting members of B.R.A.S. to share any memories we have of this event. These memories don't necessarily have to be especially profound (though this is certainly encouraged), and they can be about any of the Apollo missions, not just Apollo 11. BRAS ZAZZLE SHOP We opened a shop on Zazzle We are working some the bugs (i.e. T- Shirt prices). The shop can be found at: https://www.zazzle.com/store/br_astronomical VOLUNTEER AT HRPO: If any of the members wish to volunteer at HRPO, please speak to Chris Kersey, BRAS Liaison for BREC, to fill out the paperwork. -
Astronomical Phenomena 2019
ASTRONOMICAL PHENOMENA FOR THE YEAR 2019 Prepared Jointly by The Nautical Almanac Office United States Naval Observatory and Her Majesty’s Nautical Almanac Office United Kingdom Hydrographic Office WASHINGTON U.S. Government Publishing Office 2016 UNITED STATES Printed in the United States of America by the U. S. Government Publishing Office by permission For sale by the U.S. Government Publishing Office Superintendent of Documents P. O. Box 979050 St. Louis, MO 63197-9000 phone: 1-202-512-1800 order online at https://bookstore.gpo.gov/ UNITED KINGDOM ✂c Crown Copyright 2016 This publication is protected by international copyright law. All rights reserved. These pages may be reproduced under the terms of the UK Open Government Licence http://www.nationalarchives.gov.uk/doc/open-government-licence/version/2/ acknowledging the source as Her Majesty’s Nautical Almanac Office, United Kingdom Hydrographic Office. The following United States government work is excepted from the above notice, and no copyright is claimed for it in the United States: cover, title page and reverse, pages 64-71, 73-76, 78-88. Available from HM Nautical Almanac Office UK Hydrographic Office Admiralty Way Taunton Somerset TA1 2DN [email protected] Further information: http://www.usno.navy.mil/USNO/ https://www.gov.uk/government/organisations/hm-nautical-almanac-office ASTRONOMICAL PHENOMENA FOR THE YEAR 2019 CONTENTS Page Phenomena: Perihelion Passages of Comets ... ... ... ... ... ... ... ... ... ... 3 Seasons, Moon Phases, Eclipses ... ... ... ... ... ... ... ... ... 4 Occultations, Perigee and Apogee of the Moon ... ... ... ... ... ... 5 Geocentric and Heliocentric Planetary Phenomena ... ... ... ... ... 6 Visibility of the Planets ... ... ... ... ... ... ... ... ... ... ... 7, 8 Times of Meridian Passages of the Planets .. -
Arxiv:2102.11399V2 [Astro-Ph.EP] 24 Apr 2021 Degeneracies
THE MANIFOLD OF VARIATIONS: IMPACT LOCATION OF SHORT-TERM IMPACTORS ALESSIO DEL VIGNA, LINDA DIMARE, AND DAVIDE BRACALI CIOCI Abstract. The interest in the problem of small asteroids observed shortly before a deep close approach or an impact with the Earth has grown a lot in recent years. Since the observational dataset of such objects is very limited, they deserve dedicated orbit determination and hazard assessment methods. The currently available systems are based on the systematic ranging, a technique providing a 2-dimensional manifold of orbits compatible with the observations, the so-called Manifold Of Variations. In this paper we first review the Manifold Of Variations method, to then show how this set of virtual asteroids can be used to predict the impact location of short-term impactors, and compare the results with those of already existent methods. 1. Introduction Astronomers observe the sky every night to search for new asteroids or for already known objects. The Minor Planet Center (MPC) collects the observations coming from all over the world and then tries to compute orbits and to determine the nature of the observed objects. New discoveries which could be Near-Earth Asteroids (NEAs) are posted in the NEO Confirmation Page (NEOCP1), which thus contains observational data of unconfirmed objects. They could be real asteroids as well as non-real objects, and cannot be officially designated until additional observations are enough to compute a reliable orbit and confirm the discovery. Some asteroids with an Earth-crossing orbit may impact our planet and the goal of impact monitoring is to identify potentially hazardous cases and solicit follow-up observations. -
Characterization of the June Epsilon
A&A 636, A122 (2020) Astronomy https://doi.org/10.1051/0004-6361/202037727 & © ESO 2020 Astrophysics Characterization of the June epsilon Ophiuchids meteoroid stream and the comet 300P/Catalina Pavol Matlovicˇ1, Leonard Kornoš1, Martina Kovácovᡠ1, Juraj Tóth1, and Javier Licandro2,3 1 Faculty of Mathematics, Physics and Informatics, Comenius University, Bratislava, Slovakia e-mail: [email protected] 2 Instituto de Astrofísica de Canarias (IAC), C/Vía Láctea s/n, 38205 La Laguna, Spain 3 Departamento de Astrofísica, Universidad de La Laguna, 38206 La Laguna, Tenerife, Spain Received 13 February 2020 / Accepted 23 March 2020 ABSTRACT Aims. Prior to 2019, the June epsilon Ophiuchids (JEO) were known as a minor unconfirmed meteor shower with activity that was considered typically moderate for bright fireballs. An unexpected bout of enhanced activity was observed in June 2019, which even raised the possibility that it was linked to the impact of the small asteroid 2019 MO near Puerto Rico. Early reports also point out the similarity of the shower to the orbit of the comet 300P/Catalina. We aim to analyze the orbits, emission spectra, and material strengths of JEO meteoroids to provide a characterization of this stream, identify its parent object, and evaluate its link to the impacting asteroid 2019 MO. Methods. Our analysis is based on a sample of 22 JEO meteor orbits and four emission spectra observed by the AMOS network at the Canary Islands and in Chile. The meteoroid composition was studied by spectral classification based on relative intensity ratios of Na, Mg, and Fe. Heliocentric orbits, trajectory parameters, and material strengths were determined for each meteor and the mean orbit and radiant of the stream were calculated. -
Ice & Stone 2020
Ice & Stone 2020 WEEK 26: JUNE 21-27 Presented by The Earthrise Institute # 26 Authored by Alan Hale This week in history JUNE 21 22 23 24 25 26 27 JUNE 22, 1978: U.S. Naval Observatory astronomer James Christy discovers Charon, Pluto’s first-known moon. Charon, the discovery of which would be confirmed with a series of transit and occultation events between it and Pluto that began in 1995, provided a major step in our understanding of Pluto’s size and physical nature. Pluto, its system of moons, and the New Horizons flyby through this system are the topic of a future “Special Topics” presentation. JUNE 22, 2019: The ATLAS survey program based in Hawaii discovers a tiny asteroid, designated 2019 MO, that entered Earth’s atmosphere over the Caribbean Sea and disintegrated a little less than twelve hours later. This is the fourth, and thus far most recent, event of this nature that has been detected; these are discussed in a future “Special Topics” presentation. JUNE 21 22 23 24 25 26 27 JUNE 25, 2020: Comet 2P/Encke, the comet with the shortest-known orbital period, will pass through perihelion at a heliocentric distance of 0.337 AU. Around the beginning of July it becomes accessible from the southern hemisphere and may briefly be bright enough to detect with binoculars. It is this week’s “Comet of the Week.” COVER IMAGE CREDIT: Front and back cover: As part of the global effort to hunt out risky celestial objects such as asteroids and comets, ESA is developing an automated telescope, nicknamed ‘Flyeye’, for nightly sky surveys. -
XVI Congresso Nazionale Di Scienze Planetarie Book of Abstracts
XVI Congresso Nazionale di Scienze Planetarie Book of Abstracts https://indico.ict.inaf.it/e/CongressoPlanetologia Scientific Organizing Committee • G.Cremonese, chair INAF-Padova - [email protected] • M.Lazzarin, chair, dip.Fisica e Astronomia, Universita’ di Padova - [email protected] • J.Brucato, INAF -Firenze • F.Capaccioni, INAF - IAPS, Roma • M.T.Capria, INAF - IAPS, Roma • A.Cellino, INAF - Torino • R.Claudi, INAF-Padova • S.Debei, CISAS, Universita’ di Padova • F.Esposito, INAF – Napoli • L.Iess, dip.Ingegneria Meccanica e Aerospaziale, Universita’ la Sapienza, Roma • F.Marzari, dip.Fisica e Astronomia, Universita’ di Padova • M.Massironi, dip.Geoscienze, Universita’ di Padova • E.Perozzi, ASI • G.Piccioni, INAF - IAPS, Roma • G.Piotto, dip.Fisica e Astronomia, Universita’ di Padova • G.Pratesi, dip.Scienze della Terra Universita’ di Firenze • R.Ragazzoni, INAF – Padova Local Organizing Committee • R. Spiga, chair, Università di Padova - [email protected] • G. Cremonese, INAF-Osservatorio Astronomico di Padova • M. Lazzarin, Università di Padova • F. La Forgia, Università di Padova • A. Lucchetti, INAF-Osservatorio Astronomico di Padova • G. Munaretto, INAF-Osservatorio Astronomico di Padova • M. Pajola, INAF-Osservatorio Astronomico di Padova • M. Di Martino, INAF-Osservatorio Astrofisico di Torino • R. Pozzobon, Geoscienze UNIPD • A.T. Bologna, Università di Padova • S. Cecconato, Università di Padova • S. Carraro, INAF-OAPD • L. Giacomini, INAF-IAPS • G. Mantovani, INAF-IAPS • V. Mezzalira, Universita di Padova i Programma 3 Febbraio 09.15 • welcome • 09.30 Inizio corso per giornalisti • 11.30 coffe break • 12.00 Saluto autorita’ • 12.30 relazioni programmatiche – Barbara Negri ASI – Francesca Esposito INAF – Luigi Colangeli ESA • 13.30 Pranzo 15.00 • Tavola Rotonda: le prospettive future per la nostra comunità • 16.30 Coffe break • 17.00 Piccoli Corpi: 5 presentazioni chair: Davide Perna – Alessandro Rossi, YORP-Yarkowski evolution of asteroid families – Giovanni Valsecchi, Collisions vs. -
Novel 3U Stand-Alone Cubesat Architecture for Autonomous Near Earth Asteroid Fly-By
aerospace Article Novel 3U Stand-Alone CubeSat Architecture for Autonomous Near Earth Asteroid Fly-By Stefano Casini 1,2,*, Iosto Fodde 3, Bert Monna 2, Angelo Cervone 1 and Eberhard Gill 1 1 Space Systems Engineering, Faculty of Aerospace Engineering, Delft University of Technology, Kluyverweg 1, 2629 HS Delft, The Netherlands; [email protected] (A.C.); [email protected] (E.G.) 2 Hyperion Technologies, Vlinderweg 2, 2623 AX Delft, The Netherlands; [email protected] 3 University of Strathclyde, 16 Richmond Street, Glasgow G1 1XJ, UK; [email protected] * Correspondence: [email protected]; Tel.: +31-15-27-89804 Abstract: The purpose of this work is to present a novel CubeSat architecture, aimed to explore Near Earth Asteroids. The fast growth in small satellite commercial-off-the-shelf technologies, which characterized the last decade of space industry, is exploited to design a 3U CubeSat able to provide a basic scientific return sufficient to improve the target asteroid dataset. An overview of the current available technologies for each subsystem is presented, followed by a component selection driven by the mission constraints. First a typical asteroid fly-by mission is introduced together with the system and performance requirements. Then each characterizing subsystem is critically analyzed, and the proposed configuration is presented, showing the mission feasibility within only 3.9 kg of wet mass and 385 m/s of total DV. Keywords: interplanetary CubeSat; commercial-off-the-shelf; Near Earth Asteroids; fly-by 1. Introduction Citation: Casini, S.; Fodde, I.; Monna, Near Earth Asteroids (NEAs) represent one of the most challenging and interesting B.; Cervone, A.; Gill, E.