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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. -
Small Spacecraft Programs
Planetary Science Deep Space SmallSat Studies Small Spacecraft Programs Carolyn Mercer Program Officer, PSDS3 Program Executive, SIMPLEx NASA Glenn Research Center Briefing to the Mars Exploration Program Analysis Group (MEPAG) April 4, 2018 Crystal City, VA NOTE ADDED BY JPL WEBMASTER: This content has not been approved or adopted by NASA, JPL, or the California Institute of Technology. This document is being made available for information purposes only, and any views and opinions expressed herein do not necessarily state or reflect those of NASA, JPL, or the 1 California Institute of Technology. SMD CubeSat/SmallSat Approach Planetary Science Deep Space SmallSat Studies National Academies Report (2016) concluded that CubeSats have proven their ability to produce high- value science: • Useful as targeted investigations to augment the capabilities of larger missions • Useful to make highly-specific measurements • Constellations of 10-100 CubeSat/SmallSat spacecraft have the potential to enable transformational science SMD is developing a directorate-wide approach to: • Identify high-priority science objectives in each discipline that can be addressed with CubeSats/SmallSats • Manage program with appropriate cost and risk • Establish a multi-discipline approach and collaboration that helps science teams learn from experiences and grow capability, while avoiding unnecessary duplication • Leverage and partner with a growing commercial sector to collaboratively drive instrument and sensor innovation 2 PLANETARY SCIENCE DEEP SPACE SMALLSAT -
Sistema De Evaluación De Aprendizajes Para Alumnos En Situación De Extraedad
Estrategia Integral para la Mejora del Logro Educativo Alianza por la Calidad de la Educación Sistema de evaluación de aprendizajes para alumnos en situación de extraedad Colección Hacia el Logro Educativo Programa para el Fortalecimiento del Logro Educativo Sistema de evaluación de aprendizajes para alumnos en situación de extraedad Colección Hacia el Logro Educativo Sistema de evaluación de aprendizajes para alumnos en situación de extraedad,es una publicación de la Dirección General de Desarrollo de la Gestión e Innovación Educativa de la Subsecretaría de Educación Básica, realizada a través del Proyecto para Atender a la Población en Situación de Extraedad, por encargo a la Organización de Estados Iberoamericanos para la Educación, la Ciencia y la Cultura (OEI) y con la colaboración del Centro de Estudios Educativos (CEE). Alonso Lujambio Secretario de Educación Pública José Fernando González Sánchez Subsecretario de Educación Básica Coordinación general Alma Rosa Cuervo González Juan Martín Martínez Becerra Cuidado de la edición Director General de Desarrollo de la Gestión Esteban Manteca Aguirre e Innovación Educativa Jorge Humberto Miranda Vázquez Tonatiuh Arroyo Cerezo Ernesto Adolfo Ponce Rodríguez Coordinador General de Innovación Colaboradores de la Ofi cina de la Organización de Estados Iberoamericanos para la Educación, la Ciencia y la Cultura y autores de esta obra Lilia Dalila López Salmorán Coordinadora Nacional para el Fortalecimiento Coordinación del Logro Educativo Carlos Niembro Acosta Colaboradores Teresa Zamudio Gisela Santiago Benítez Maura Pompa Mancilla D.R. © Secretaría de Educación Pública, 2011 Diana Gómez Mayén Argentina 28 Col. Centro Histórico C.P. 06020, México, D.F. ISBN: 978-607-8017-53-9 Diseño y formación Constantine Editores, S. -
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. -
Explore Science
SMALL SATELLITE MISSIONS FOR PLANETARY SCIENCE Carolyn R. Mercer, Ph.D. Program Executive, Small Innovative Missions for Planetary Exploration (SIMPLEx) AIAA Small Spacecraft Missions Conference August 4, 2019 Logan, Utah Apollo 15 Particles and Fields Subsatellite (PFS-1) • 35 kg spacecraft flown with Apollo 15 in 1971 • Orbited the Moon for 6 months • Science mission: • Measured the strength and direction of interplanetary and terrestrial magnetic fields • Detected variations in the lunar gravity field • Measured proton and electron flux 2 NASA SCIENCE AN INTEGRATED PROGRAM Helio- Earth physics Science Planetary Astrophysics Science Joint Agency Satellite Division 4 Small Spacecraft for Planetary Science Astrobiology Science and Technology Instrument Development (ASTID) 2008 • O/OREOS (2010 launch) Small Innovative Missions for Planetary Exploration (SIMPLEx-1) 2014 • LunaH-Map, Q-PACE Directed and Partnered Secondary Payloads • MarCO (2018 launch) • LICIA Cube (2021) – potential ASI contribution Planetary Science Deep Space SmallSat Studies (PSDS3) 2017 • 19 Studies – Presented March 2018 at LPSC Small Innovative Missions for Planetary Exploration (SIMPLEx-2) 2018 • Janus, Escapade, Lunar Trailblazer • Next proposals due no earlier than June 2020 5 Planetary Science Deep Space SmallSat Studies Solicitation requested: • Concepts for planetary science missions • 180 kg total spacecraft mass limit • $100M cost cap • No constraints on rides, infrastructure, etc. Solicitation sought answers to: • Can deep space missions be credibly done -
PSRD | a Cosmosparks Report
PSRD | A CosmoSparks report Quick Views of Big Advances Solar Wind Interactions with a Lunar Paleo-magnetosphere How would an ancient, global magnetic field on the Moon and its associated paleo-magnetosphere interact with the incoming, charged particles in the solar wind plasma? Would a paleo-magnetosphere shield the lunar surface from solar wind bombardment? Answering these questions improves our understanding of processes that were influenced by the Moon's paleo-magnetosphere, such as the accumulation and space weathering of volatiles in the polar regions. This is the work being undertaken by Ian Garrick-Bethell (University of California, Santa Cruz/Kyung Hee University, South Korea), Andrew Poppe (University of California, Berkeley/SSERVI NASA Ames), and Shahab Fatemi (Swedish Institute of Space Physics, Kiruna). Using computer models of the plasma environment with solar wind parameters appropriate for ~2 billion years ago, Garrick-Bethell and coauthors simulated its interaction with a lunar paleo-magnetosphere. The researchers applied Amitis, a fast, 3D computer model of plasma (kinetic ions and fluid electrons). They modeled the solar wind as H+ and used lunar surface paleo-magnetic field strengths of 0.5µT, 2µT, and 5µT (microteslas) at different orientations. (Earth, by comparison, has a surface magnetic field strength ranging from ~20 to 60µT.) Shown on the left is a 2D plot of one of the Moon-modeling results of plasma density for the case of a spin-aligned 2µT equatorial surface magnetic field strength. The magnetic dipole moment is vertical, as indicated by the small black arrow. The solar wind flows from right to left. In addition to the bow shock showing where the solar wind is diverted around the lunar magnetosphere, the modeling results clearly indicate the two polar cusps (areas of focused field lines) where solar wind plasma funnels down to the lunar surface. -
Navy Space and Astronautics Orientation. INSTITUTION Bureau of Naval Personnel, Washington, D
DOCUMENT RESUME ED 070 566 SE 013 889 AUTHOR Herron, R. G. TITLE Navy Space and Astronautics Orientation. INSTITUTION Bureau of Naval Personnel, Washington, D. C.; Naval Personnel Program Support Activity, Washington, D. C. REPORT NO NAVPERS- 10488 PUB DATE 67 NOTE 235p. '2 EDRS PRICE MF-$0.65 HC-$9.87 DESCRIPTORS Aerospace Education; AerospaceTechnology; *Instructional Materials; Military Science; *Military Training; Navigatioti; *Post Secondary Education; *Space Sciences; *Supplementary Textbooks; Textbooks ABSTRACT Fundamental concepts of the spatial environment, technologies, and applications are presented in this manual prepared for senior officers and key civilian employees. Following basic information on the atmosphere, solar system, and intergalactic space, a detailed review is included of astrodynamics, rocket propulsion, bioastronautics, auxiliary spacecraft survival systems, and atmospheric entry.Subsequentlythere is an analysis of naval space facilities, and satellite applications, especially those of naval interests, are discussed with a background of launch techniques, spatial data gathering, communications programs ,of)servation techniques, measurements by geodetic and navigation systems. Included is a description of space defense and future developments of both national and international space programs. Moreover, commercial systems are mentioned, such as the 85-pound Early Bird (Intelsat I) Intelsat II series, global Intelsat III series, and Soviet-made elMolnlyan satellites. The total of 29 men and one woman orbiting the earth In-1961-67 are tabulated in terms of their names, flight series, launching dates, orbit designations, or biting periods,. stand-up periods, and extra vehicular activity records. Besides numerous illustrations, a list ofsignificantspace launches and a glossary of special terms are included in the manual appendices along with two tables of frequencybanddesignation. -
LUNAR T-Rex): IDENTIFYING RESOURCES on the MOON USING TETHERED SMALLSATS
Developing a New Space Economy (2019) 5049.pdf LUNAR TETHERED RESOURCE EXPLORER (LUNAR T-REx): IDENTIFYING RESOURCES ON THE MOON USING TETHERED SMALLSATS. T. J. Stubbs1, M. E. Purucker1, J. D. Hudeck2, R. P. Hoyt3, B. K. Malphrus4, M. A. Mesarch1, M. Bakhtiari-nejad1, G. E. Cruz-Ortiz1, E. T. Stoneking1, T. E. Johnson2, D. J. Chai1, D. C. Folta1, and R. R. Vondrak1, 1NASA Goddard Space Flight Center, 2NASA Wallops Flight Facility, 3Tethers Unlimited, Inc., 4Morehead State University. Point of contact: [email protected] Introduction: On Earth, economically viable mineralization associated With large impact craters can often be identified by its magnetic signatures [1,2]. The magnetic field from these features decays With the inverse of distance, such that identification requires low altitude measurements. On the Moon, many of the large Nectarian-aged impact features have prominent magnetic features associated With their central peak regions [3]. It is possible that the signatures of economic mineralization could be iden- tified at the Moon With low altitude (<20 km) in situ magnetic field measurements. Tethered Architecture: However, low altitude lunar orbits (<50 km) tend to be unstable, such that without regular orbit maintenance maneuvers they last only a feW Weeks before impacting the Moon [4]. A mission surveying lunar magnetic fields Would require at least a feW months, if not more than a year. The Figure 1: A tethered lunar CubeSat mission. fuel mass burden for maintaining a low altitude orbit swirls. BOLAS consisted of tWo EPSA-class Small- is prohibitive, especially for SmallSats. Sats connected by a 25 km tether With the formation The Lunar Tethered Resource Explorer (Lunar T- center-of-mass in a “frozen” orbit, Which Was stable REx) team is studying the possibility of using tWo for at least a year and had a 30° inclination. -
Disertaciones Astronómicas Boletín Número 47 De Efemérides Astronómicas 2 De Septiembre De 2020
Disertaciones astronómicas Boletín Número 47 de efemérides astronómicas 2 de septiembre de 2020 Realiza Luis Fernando Ocampo O. ([email protected]). Noticias de la semana. Meteoros y sus diferentes manifestaciones. Imagen 1: Las diferencias entre meteoroide, meteoro y meteorito. Imagen https://www.researchgate.net/ Los ‘bólidos’ son meteoros que parecen más brillantes de lo normal. Una gran mayoría del material que orbita en el espacio exterior son pequeños trozos de piedra, hielo o metal de tamaño submilimétrico, o una combinación de estos materiales. Estos se conocen como micrometeoroides o simplemente polvo espacial. Estos diminutos fragmentos no pueden producir suficiente luz para ser vistos cuando se encuentran con la atmósfera y, sin embargo, contribuyen con muchas toneladas de material al peso de la Tierra cada año. A medida que el tamaño de estos objetos se acerca a un milímetro, comienzan a producir suficiente luz para ser vistos al entrar a la atmósfera superior como meteoros ordinarios. Debido a la velocidad a la que golpean la atmósfera de la Tierra, los fragmentos de más de 1 milímetro tienen la capacidad de producir un destello brillante cuando atraviesan los cielos. Estos meteoritos brillantes son lo que llamamos bolas de fuego y, a menudo, infunden temor y asombro a quienes los presencian. Las bolas de fuego ocurren todos los días en toda la Tierra. Sin embargo, para el individuo, son un espectáculo raro que se presencia muy pocas veces en la vida. Debe recordarse que las bolas de fuego también ocurren durante el día o en una noche nublada. También ocurren sobre el océano o sobre porciones de tierra deshabitadas. -
Technology Development for Planetary Science Missions
Technology Development for Planetary Science Missions James Green NASA, Planetary Science Division July 13, 2017 NAS Planetary Decadal Mid-Term 1 Outline • PSD Response to Technology Development in the Planetary Decadal • Specific Topics to be Addressed as Requested: – Electric Power – Electric Propulsion forecasted ISP Improvement timeline versus mission needs – Planetary Relay Optical Comm Concepts and Implementation timeline • Detector/Instrumentation Development • Planetary Data System 1/29/16 2 Visions and Voyages “The committee unequivocally recommends that a substantial program of planetary exploration technology development should be reconstituted and carefully protected against all incursions that would deplete its resources. This program should be consistently funded at approximately 6 to 8 percent of the total NASA Planetary Science Division budget.” “The committee recommends that the Planetary Science Division’s technology program should accept the responsibility, and assign the required funds, to continue the development of the most important technology items through TRL 6.” Technology Investment Categories Spacecraft: Broad and Mission-Specific Instruments: Broad and Mission-Specific Mission Support: o Tools(technology analysis, mission analysis, technology development) o Facilities (necessary for technology development) o Processes (necessary for technology utilization) Management: o Studies o Planning, Documentation and Communication 4 PSD Technology Funding by Category FY16 Total = $243M (All) (Technologies only = -
An Evolving Astrobiology Glossary
Bioastronomy 2007: Molecules, Microbes, and Extraterrestrial Life ASP Conference Series, Vol. 420, 2009 K. J. Meech, J. V. Keane, M. J. Mumma, J. L. Siefert, and D. J. Werthimer, eds. An Evolving Astrobiology Glossary K. J. Meech1 and W. W. Dolci2 1Institute for Astronomy, 2680 Woodlawn Drive, Honolulu, HI 96822 2NASA Astrobiology Institute, NASA Ames Research Center, MS 247-6, Moffett Field, CA 94035 Abstract. One of the resources that evolved from the Bioastronomy 2007 meeting was an online interdisciplinary glossary of terms that might not be uni- versally familiar to researchers in all sub-disciplines feeding into astrobiology. In order to facilitate comprehension of the presentations during the meeting, a database driven web tool for online glossary definitions was developed and participants were invited to contribute prior to the meeting. The glossary was downloaded and included in the conference registration materials for use at the meeting. The glossary web tool is has now been delivered to the NASA Astro- biology Institute so that it can continue to grow as an evolving resource for the astrobiology community. 1. Introduction Interdisciplinary research does not come about simply by facilitating occasions for scientists of various disciplines to come together at meetings, or work in close proximity. Interdisciplinarity is achieved when the total of the research expe- rience is greater than the sum of its parts, when new research insights evolve because of questions that are driven by new perspectives. Interdisciplinary re- search foci often attack broad, paradigm-changing questions that can only be answered with the combined approaches from a number of disciplines. -
Planetary Science Update
Planetary Science Division Status Report Jim Green NASA, Planetary Science Division October 11, 2017 Presentation at LEAG Planetary Science Missions Events 2016 March – Launch of ESA’s ExoMars Trace Gas Orbiter July 4 – Juno inserted in Jupiter orbit * Completed September 8 – Launch of Asteroid mission OSIRIS – REx to asteroid Bennu September 30 – Landing Rosetta on comet CG October 19 – ExoMars EDM landing and TGO orbit insertion 2017 January 4 – Discovery Mission selection announced February 9-20 - OSIRIS-REx began Earth-Trojan search April 22 – Cassini begins plane change maneuver for the “Grand Finale” August 22 – Solar Eclipse across America September 15 – Cassini end of mission at Saturn September 22 – OSIRIS-REx Earth flyby October 28 – International Observe the Moon night (1st quarter) 2018 May 5 - Launch InSight mission to Mars August – OSIRIS-REx arrival at Bennu October – Launch of ESA’s BepiColombo to Mercury November 26 – InSight landing on Mars 2019 January 1 – New Horizons flyby of Kuiper Belt object 2014MU69 Formulation Implementation Primary Ops BepiColombo Lunar Extended Ops (ESA) Reconnaissance Orbiter Lucy New Horizons Psyche Juno Dawn JUICE (ESA) ExoMars 2016 MMX MAVEN MRO (ESA) (JAXA) Mars Express Mars (ESA) Odyssey OSIRIS-REx ExoMars 2020 (ESA) Mars Rover Opportunity Curiosity InSight 2020 Rover Rover NEOWISE Europa Clipper Discovery Program Discovery Program NEO characteristics: Mars evolution: Lunar formation: Nature of dust/coma: Solar wind sampling: NEAR (1996-1999) Mars Pathfinder (1996-1997) Lunar Prospector