Volcanic History of the Imbrium Basin: a Close-Up View from the Lunar Rover Yutu
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A Summary of the Unified Lunar Control Network 2005 and Lunar Topographic Model B. A. Archinal, M. R. Rosiek, R. L. Kirk, and B
A Summary of the Unified Lunar Control Network 2005 and Lunar Topographic Model B. A. Archinal, M. R. Rosiek, R. L. Kirk, and B. L. Redding U. S. Geological Survey, 2255 N. Gemini Drive, Flagstaff, AZ 86001, USA, [email protected] Introduction: We have completed a new general unified lunar control network and lunar topographic model based on Clementine images. This photogrammetric network solution is the largest planetary control network ever completed. It includes the determination of the 3-D positions of 272,931 points on the lunar surface and the correction of the camera angles for 43,866 Clementine images, using 546,126 tie point measurements. The solution RMS is 20 µm (= 0.9 pixels) in the image plane, with the largest residual of 6.4 pixels. We are now documenting our solution [1] and plan to release the solution results soon [2]. Previous Networks: In recent years there have been two generally accepted lunar control networks. These are the Unified Lunar Control Network (ULCN) and the Clementine Lunar Control Network (CLCN), both derived by M. Davies and T. Colvin at RAND. The original ULCN was described in the last major publication about a lunar control network [3]. Images for this network are from the Apollo, Mariner 10, and Galileo missions, and Earth-based photographs. The CLCN was derived from Clementine images and measurements on Clementine 750-nm images. The purpose of this network was to determine the geometry for the Clementine Base Map [4]. The geometry of that mosaic was used to produce the Clementine UVVIS digital image model [5] and the Near-Infrared Global Multispectral Map of the Moon from Clementine [6]. -
Modeling and Adjustment of THEMIS IR Line Scanner Camera Image Measurements
Modeling and Adjustment of THEMIS IR Line Scanner Camera Image Measurements by Brent Archinal USGS Astrogeology Team 2255 N. Gemini Drive Flagstaff, AZ 86001 [email protected] As of 2004 December 9 Version 1.0 Table of Contents 1. Introduction 1.1. General 1.2. Conventions 2. Observations Equations and Their Partials 2.1. Line Scanner Camera Specific Modeling 2.2. Partials for New Parameters 2.2.1. Orientation Partials 2.2.2. Spatial Partials 2.2.3. Partials of the observations with respect to the parameters 2.2.4. Parameter Weighting 3. Adjustment Model 4. Implementation 4.1. Input/Output Changes 4.1.1. Image Measurements 4.1.2. SPICE Data 4.1.3. Program Control (Parameters) Information 4.2. Computational Changes 4.2.1. Generation of A priori Information 4.2.2. Partial derivatives 4.2.3. Solution Output 5. Testing and Near Term Work 6. Future Work Acknowledgements References Useful web sites Appendix I - Partial Transcription of Colvin (1992) Documentation Appendix II - HiRISE Sensor Model Information 1. Introduction 1.1 General The overall problem we’re solving is that we want to be able to set up the relationships between the coordinates of arbitrary physical points in space (e.g. ground points) and their coordinates on line scanner (or “pushbroom”) camera images. We then want to do a least squares solution in order to come up with consistent camera orientation and position information that represents these relationships accurately. For now, supported by funding from the NASA Critical Data Products initiative (for 2003 September to 2005 August), we will concentrate on handling the THEMIS IR camera system (Christensen et al., 2003). -
EPSC2013-167, 2013 European Planetary Science Congress 2013 Eeuropeapn Planetarsy Science Ccongress C Author(S) 2013
EPSC Abstracts Vol. 8, EPSC2013-167, 2013 European Planetary Science Congress 2013 EEuropeaPn PlanetarSy Science CCongress c Author(s) 2013 Scientific Characterization of Mare Moscoviense Region of Interest A. Calzada (1) and S.C. Mest (2,3) (1) Department of Earth and Planetary Sciences Birkbeck, University of London, Malet Street, Bloomsbury, London WC1E 7HX (2) Planetary Science Institute, 1700 E. Ft. Lowell, Suite 106, Tucson, AZ 85719-2395 and (3) Planetary Geodynamics Laboratory, Code 698, NASA GSFC, Greenbelt, MD 20771 Abstract NASA´s Constellation Program has identified 50 Regions of Interest (ROI) with high scientific value in preparation for an eventual return to the Moon [1]. These 50 locations are geological diverse and geographically distributed to achieve a variety of goals and objectives and described by LEAG [2]. In order to evaluate its scientific interest, Mare Moscoviense (MMos) ROI was characterized using digital images and data provided by NASA´s Clementine and Lunar Reconnaissance (LRO) Missions as well as ArcGISTM v.10.1 software to create a geomorphologic and geologic map. The cartography and the input were analyzed to propose a set of three hypothetical traverses for future human or robotic expeditions within an area up to distances of 5, 10 and 20 km from the ROI location. The traverses has no constrains regarding Figure 1 LRO WAC Image from Mare Moscoviense basin. Red schedule, distances or topography. Experiments box indicates the studied area. Credits: NASA/JPL/MSSS proposed vary from petrologic and geochemical characterization such as samples and drill cores to 2. Cartography geophysical experiments using gravimetry, magnetometry and seismicity methods. -
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. -
Warren and Taylor-2014-In Tog-The Moon-'Author's Personal Copy'.Pdf
This article was originally published in Treatise on Geochemistry, Second Edition published by Elsevier, and the attached copy is provided by Elsevier for the author's benefit and for the benefit of the author's institution, for non- commercial research and educational use including without limitation use in instruction at your institution, sending it to specific colleagues who you know, and providing a copy to your institution’s administrator. All other uses, reproduction and distribution, including without limitation commercial reprints, selling or licensing copies or access, or posting on open internet sites, your personal or institution’s website or repository, are prohibited. For exceptions, permission may be sought for such use through Elsevier's permissions site at: http://www.elsevier.com/locate/permissionusematerial Warren P.H., and Taylor G.J. (2014) The Moon. In: Holland H.D. and Turekian K.K. (eds.) Treatise on Geochemistry, Second Edition, vol. 2, pp. 213-250. Oxford: Elsevier. © 2014 Elsevier Ltd. All rights reserved. Author's personal copy 2.9 The Moon PH Warren, University of California, Los Angeles, CA, USA GJ Taylor, University of Hawai‘i, Honolulu, HI, USA ã 2014 Elsevier Ltd. All rights reserved. This article is a revision of the previous edition article by P. H. Warren, volume 1, pp. 559–599, © 2003, Elsevier Ltd. 2.9.1 Introduction: The Lunar Context 213 2.9.2 The Lunar Geochemical Database 214 2.9.2.1 Artificially Acquired Samples 214 2.9.2.2 Lunar Meteorites 214 2.9.2.3 Remote-Sensing Data 215 2.9.3 Mare Volcanism -
Rare Earth Elements in Planetary Crusts: Insights from Chemically Evolved Igneous Suites on Earth and the Moon
minerals Article Rare Earth Elements in Planetary Crusts: Insights from Chemically Evolved Igneous Suites on Earth and the Moon Claire L. McLeod 1,* and Barry J. Shaulis 2 1 Department of Geology and Environmental Earth Sciences, 203 Shideler Hall, Miami University, Oxford, OH 45056, USA 2 Department of Geosciences, Trace Element and Radiogenic Isotope Lab (TRaIL), University of Arkansas, Fayetteville, AR 72701, USA; [email protected] * Correspondence: [email protected]; Tel.: +1-513-529-9662 Received: 5 July 2018; Accepted: 8 October 2018; Published: 16 October 2018 Abstract: The abundance of the rare earth elements (REEs) in Earth’s crust has become the intense focus of study in recent years due to the increasing societal demand for REEs, their increasing utilization in modern-day technology, and the geopolitics associated with their global distribution. Within the context of chemically evolved igneous suites, 122 REE deposits have been identified as being associated with intrusive dike, granitic pegmatites, carbonatites, and alkaline igneous rocks, including A-type granites and undersaturated rocks. These REE resource minerals are not unlimited and with a 5–10% growth in global demand for REEs per annum, consideration of other potential REE sources and their geological and chemical associations is warranted. The Earth’s moon is a planetary object that underwent silicate-metal differentiation early during its history. Following ~99% solidification of a primordial lunar magma ocean, residual liquids were enriched in potassium, REE, and phosphorus (KREEP). While this reservoir has not been directly sampled, its chemical signature has been identified in several lunar lithologies and the Procellarum KREEP Terrane (PKT) on the lunar nearside has an estimated volume of KREEP-rich lithologies at depth of 2.2 × 108 km3. -
Science Concept 5: Lunar Volcanism Provides a Window Into the Thermal and Compositional Evolution of the Moon
Science Concept 5: Lunar Volcanism Provides a Window into the Thermal and Compositional Evolution of the Moon Science Concept 5: Lunar volcanism provides a window into the thermal and compositional evolution of the Moon Science Goals: a. Determine the origin and variability of lunar basalts. b. Determine the age of the youngest and oldest mare basalts. c. Determine the compositional range and extent of lunar pyroclastic deposits. d. Determine the flux of lunar volcanism and its evolution through space and time. INTRODUCTION Features of Lunar Volcanism The most prominent volcanic features on the lunar surface are the low albedo mare regions, which cover approximately 17% of the lunar surface (Fig. 5.1). Mare regions are generally considered to be made up of flood basalts, which are the product of highly voluminous basaltic volcanism. On the Moon, such flood basalts typically fill topographically-low impact basins up to 2000 m below the global mean elevation (Wilhelms, 1987). The mare regions are asymmetrically distributed on the lunar surface and cover about 33% of the nearside and only ~3% of the far-side (Wilhelms, 1987). Other volcanic surface features include pyroclastic deposits, domes, and rilles. These features occur on a much smaller scale than the mare flood basalts, but are no less important in understanding lunar volcanism and the internal evolution of the Moon. Table 5.1 outlines different types of volcanic features and their interpreted formational processes. TABLE 5.1 Lunar Volcanic Features Volcanic Feature Interpreted Process -
Actual Problems Актуальные Проблемы
АКАДЕМИЯ НАУК АВИАЦИИ И ВОЗДУХОПЛАВАНИЯ РОССИЙСКАЯ АКАДЕМИЯ КОСМОНАВТИКИ ИМ. К.Э.ЦИОЛКОВСКОГО ACADEMY OF AVIATION AND AERONAUTICS SCIENCES RUSSIAN ASTRONAUTICS ACADEMY OF K.E.TSIOLKOVSKY'S NAME СССР 7 195 ISSN 1727-6853 12.04.1961 АКТУАЛЬНЫЕ ПРОБЛЕМЫ АВИАЦИОННЫХ И АЭРОКОСМИЧЕСКИХ СИСТЕМ процессы, модели, эксперимент 2(39) 2014 RUSSIAN-AMERICAN SCIENTIFIC JOURNAL ACTUAL PROBLEMS OF AVIATION AND AEROSPACE SYSTEMS processes, models, experiment УРНАЛ УЧНЫЙ Ж О-АМЕРИКАНСКИЙ НА ОССИЙСК Р Казань Daytona Beach А К Т УА Л Ь Н Ы Е П Р О Б Л Е М Ы А В И А Ц И О Н Н Ы Х И А Э Р О К О С М И Ч Е С К И Х С И С Т Е М Казань, Дайтона Бич Вып. 2 (39), том 19, 1-206, 2014 СОДЕРЖАНИЕ CONTENTS Г.В.Новожилов 1 G.V.Novozhilov К 120-летию авиаконструктора To the 120-th Anniversary of Сергея Владимировича Ильюшина Sergey Vladimirovich Ilyushin А.Болонкин 14 A.Bolonkin Использование энергии ветра Utilization of wind energy at high больших высот altitude Эмилио Спедикато 46 Emilio Spedicato О моделировании взаимодействия About modelling interaction of Earth Земли с крупным космическим with large space object: the script with объектом: сценарий взрыва Фаэтона explosion of Phaeton and the sub- и последующей эволюции sequent evolution of Mankind (part II) Человечества (часть II) М.В.Левский 76 M.V.Levskii Оптимальное по времени The time-optimal control of motion of a управление движением spacecraft with inertial executive космического аппарата с devices инерционными исполнительными органами В.А.Афанасьев, А.С.Мещанов, 99 V.A.Afanasyev, A.S.Meshchanov, Е.Ю.Самышева -
Application of Tetraether Membrane Lipids As Proxies for Continental Climate
Institut de Ciència i Tecnologia Ambientals Universitat Autònoma de Barcelona Application of tetraether membrane lipids as proxies for continental climate reconstruction in Iberian and Siberian lakes Marina Escala Pascual Tesi doctoral Institut de Ciència i Tecnologia Ambientals Universitat Autònoma de Barcelona Application of tetraether membrane lipids as proxies for continental climate reconstruction in Iberian and Siberian lakes Memòria presentada per Marina Escala Pascual per optar al títol de Doctor per la Universitat Autònoma de Barcelona, sota la direcció del doctor Antoni Rosell Melé. Marina Escala Pascual Abril 2009 Cover photograph: Lake Baikal (Jens Klump, Continent Project) Als meus pares i al meu germà. INDEX Acknowledgements .................................................................................i Abstract .................................................................................................iii Resum ....................................................................................................iv Chapter 1 Introduction 1.1. Paleoclimate and biomarker proxies ....................................................3 1.2. Distribution of Archaea in freshwater environments ........................5 1.3. Origin and significance of GDGTs .......................................................9 1.4. Calibration of GDGT-based proxies ..................................................14 1.5. Objective and outline of this thesis ....................................................19 Chapter 2 Methodology 2.1. -
Space Sector Brochure
SPACE SPACE REVOLUTIONIZING THE WAY TO SPACE SPACECRAFT TECHNOLOGIES PROPULSION Moog provides components and subsystems for cold gas, chemical, and electric Moog is a proven leader in components, subsystems, and systems propulsion and designs, develops, and manufactures complete chemical propulsion for spacecraft of all sizes, from smallsats to GEO spacecraft. systems, including tanks, to accelerate the spacecraft for orbit-insertion, station Moog has been successfully providing spacecraft controls, in- keeping, or attitude control. Moog makes thrusters from <1N to 500N to support the space propulsion, and major subsystems for science, military, propulsion requirements for small to large spacecraft. and commercial operations for more than 60 years. AVIONICS Moog is a proven provider of high performance and reliable space-rated avionics hardware and software for command and data handling, power distribution, payload processing, memory, GPS receivers, motor controllers, and onboard computing. POWER SYSTEMS Moog leverages its proven spacecraft avionics and high-power control systems to supply hardware for telemetry, as well as solar array and battery power management and switching. Applications include bus line power to valves, motors, torque rods, and other end effectors. Moog has developed products for Power Management and Distribution (PMAD) Systems, such as high power DC converters, switching, and power stabilization. MECHANISMS Moog has produced spacecraft motion control products for more than 50 years, dating back to the historic Apollo and Pioneer programs. Today, we offer rotary, linear, and specialized mechanisms for spacecraft motion control needs. Moog is a world-class manufacturer of solar array drives, propulsion positioning gimbals, electric propulsion gimbals, antenna positioner mechanisms, docking and release mechanisms, and specialty payload positioners. -
March 21–25, 2016
FORTY-SEVENTH LUNAR AND PLANETARY SCIENCE CONFERENCE PROGRAM OF TECHNICAL SESSIONS MARCH 21–25, 2016 The Woodlands Waterway Marriott Hotel and Convention Center The Woodlands, Texas INSTITUTIONAL SUPPORT Universities Space Research Association Lunar and Planetary Institute National Aeronautics and Space Administration CONFERENCE CO-CHAIRS Stephen Mackwell, Lunar and Planetary Institute Eileen Stansbery, NASA Johnson Space Center PROGRAM COMMITTEE CHAIRS David Draper, NASA Johnson Space Center Walter Kiefer, Lunar and Planetary Institute PROGRAM COMMITTEE P. Doug Archer, NASA Johnson Space Center Nicolas LeCorvec, Lunar and Planetary Institute Katherine Bermingham, University of Maryland Yo Matsubara, Smithsonian Institute Janice Bishop, SETI and NASA Ames Research Center Francis McCubbin, NASA Johnson Space Center Jeremy Boyce, University of California, Los Angeles Andrew Needham, Carnegie Institution of Washington Lisa Danielson, NASA Johnson Space Center Lan-Anh Nguyen, NASA Johnson Space Center Deepak Dhingra, University of Idaho Paul Niles, NASA Johnson Space Center Stephen Elardo, Carnegie Institution of Washington Dorothy Oehler, NASA Johnson Space Center Marc Fries, NASA Johnson Space Center D. Alex Patthoff, Jet Propulsion Laboratory Cyrena Goodrich, Lunar and Planetary Institute Elizabeth Rampe, Aerodyne Industries, Jacobs JETS at John Gruener, NASA Johnson Space Center NASA Johnson Space Center Justin Hagerty, U.S. Geological Survey Carol Raymond, Jet Propulsion Laboratory Lindsay Hays, Jet Propulsion Laboratory Paul Schenk, -
LUNAR REGOLITH PROPERTIES CONSTRAINED by LRO DIVINER and CHANG'e 2 MICROWAVE RADIOMETER DATA. J. Feng1, M. A. Siegler1, P. O
50th Lunar and Planetary Science Conference 2019 (LPI Contrib. No. 2132) 3176.pdf LUNAR REGOLITH PROPERTIES CONSTRAINED BY LRO DIVINER AND CHANG’E 2 MICROWAVE RADIOMETER DATA. J. Feng1, M. A. Siegler1, P. O. Hayne2, D. T. Blewett3, 1Planetary Sci- ence Institute (1700 East Fort Lowell, Suite 106 Tucson, AZ 85719-2395, [email protected]), 2University of Colorado, Boulder. 3Johns Hopkins Univ. Applied Physics Lab, Maryland. Introduction: The geophysical properties of the sults of the thermal model (which includes layer num- lunar regolith have been well-studied, but many uncer- bers, layer thickness, temperature profile and density tainties remain about their in-situ nature. Diviner Lunar profile) are input parameters for the microwave model. Radiometer Experiment onboard LRO [1] is an instru- In contrast to [2, 3], we update the thermal parame- ment measuring the surface bolometric temperature of ters to match the surface temperature at noon in the the regolith. It has been systematically mapping the equatorial region and diurnal temperature variation in Moon since July 5, 2009 at solar and infrared wave- high latitude (Fig. 1). The best fit of the data show that lengths covering a full range of latitudes, longitudes, for most highlands the regolith has a bond albedo of local times and seasons. The Microwave Radiometer 0.09 at normal solar incidence and bond albedo at arbi- (MRM) carried by Chang’e 2 (CE-2) was used to de- trary solar incidence θ is represented by A=0.09 rive the brightness temperature of the moon in frequen- +0.04×(4θ/π)3+0.05×(2θ/π)8.