EPSC-DPS2011-1095, 2011 EPSC-DPS Joint Meeting 2011 C Author(S) 2011
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Geologic Structure of Shallow Maria
NASA CR. Photo Data Analysis S-221 NASA Contract NAS 9-13196 GEOLOGIC STRUCTURE OF SHALLOW MARIA Rene' A. De Hon, Principal Investigator John A. Waskom, Co-Investigator (NASA-CR-lq7qoo GEOLOGIC STahJCTUnF OF N76-17001 ISBALOW M1BIA-'(Arkansas Uni.v., mHiticelio.) 96 p BC $5.00' CSCL O3B Unclas G3/91, 09970- University of Arkansas at Monticello Monticello, Arkansas December 1975 Photo Data Analysis S-221 NASA Contract NAS 9-13196 GEOLOGIC STRUCTURE OF SHALLOW MARIA Rene' A. De Hon, Principal Investigator I John A. Waskom, Co-Investigator Un-iversity-of Arkansas-:at-.Monticl o Monticello, Arkansas December 1975 ABSTRACT Isopach maps and structural contour maps of the 0 0 eastern mare basins (30 N to 30 OS; 00 to 100 E) are constructed from measurements of partially buried craters. The data, which are sufficiently scattered to yield gross thickness variations, are restricted to shallow maria with less than 1500-2000 m of mare basalts. The average thickness of b-asalt in the irregular maria is between 200 and 400 m. Multiringed mascon basins are filled to various levels. The Serenitatis and Crisium basins have deeply flooded interiors and extensively flooded shelves. Mare basalts in the Nectaris basin fill only the innermost basin, and mare basalts in the Smythii basin occupy a small portion of the basin floor. Sinus Amoris, Mare Spumans, and Mare Undarum are partially filled troughs concentric to large circular basins. The Tranquillitatis and Fecunditatis are composite depressions containing basalts which flood degraded circular basins and adjacent terrain modified by the formation of nearby cir cular basins. -
TRANSIENT LUNAR PHENOMENA: REGULARITY and REALITY Arlin P
The Astrophysical Journal, 697:1–15, 2009 May 20 doi:10.1088/0004-637X/697/1/1 C 2009. The American Astronomical Society. All rights reserved. Printed in the U.S.A. TRANSIENT LUNAR PHENOMENA: REGULARITY AND REALITY Arlin P. S. Crotts Department of Astronomy, Columbia University, Columbia Astrophysics Laboratory, 550 West 120th Street, New York, NY 10027, USA Received 2007 June 27; accepted 2009 February 20; published 2009 April 30 ABSTRACT Transient lunar phenomena (TLPs) have been reported for centuries, but their nature is largely unsettled, and even their existence as a coherent phenomenon is controversial. Nonetheless, TLP data show regularities in the observations; a key question is whether this structure is imposed by processes tied to the lunar surface, or by terrestrial atmospheric or human observer effects. I interrogate an extensive catalog of TLPs to gauge how human factors determine the distribution of TLP reports. The sample is grouped according to variables which should produce differing results if determining factors involve humans, and not reflecting phenomena tied to the lunar surface. Features dependent on human factors can then be excluded. Regardless of how the sample is split, the results are similar: ∼50% of reports originate from near Aristarchus, ∼16% from Plato, ∼6% from recent, major impacts (Copernicus, Kepler, Tycho, and Aristarchus), plus several at Grimaldi. Mare Crisium produces a robust signal in some cases (however, Crisium is too large for a “feature” as defined). TLP count consistency for these features indicates that ∼80% of these may be real. Some commonly reported sites disappear from the robust averages, including Alphonsus, Ross D, and Gassendi. -
DMAAC – February 1973
LUNAR TOPOGRAPHIC ORTHOPHOTOMAP (LTO) AND LUNAR ORTHOPHOTMAP (LO) SERIES (Published by DMATC) Lunar Topographic Orthophotmaps and Lunar Orthophotomaps Scale: 1:250,000 Projection: Transverse Mercator Sheet Size: 25.5”x 26.5” The Lunar Topographic Orthophotmaps and Lunar Orthophotomaps Series are the first comprehensive and continuous mapping to be accomplished from Apollo Mission 15-17 mapping photographs. This series is also the first major effort to apply recent advances in orthophotography to lunar mapping. Presently developed maps of this series were designed to support initial lunar scientific investigations primarily employing results of Apollo Mission 15-17 data. Individual maps of this series cover 4 degrees of lunar latitude and 5 degrees of lunar longitude consisting of 1/16 of the area of a 1:1,000,000 scale Lunar Astronautical Chart (LAC) (Section 4.2.1). Their apha-numeric identification (example – LTO38B1) consists of the designator LTO for topographic orthophoto editions or LO for orthophoto editions followed by the LAC number in which they fall, followed by an A, B, C or D designator defining the pertinent LAC quadrant and a 1, 2, 3, or 4 designator defining the specific sub-quadrant actually covered. The following designation (250) identifies the sheets as being at 1:250,000 scale. The LTO editions display 100-meter contours, 50-meter supplemental contours and spot elevations in a red overprint to the base, which is lithographed in black and white. LO editions are identical except that all relief information is omitted and selenographic graticule is restricted to border ticks, presenting an umencumbered view of lunar features imaged by the photographic base. -
Cratering Flow Fields
Proc. Lunar Planet. Sci. Conj. !Ith (1980), p. 2347-2378. Printed in the United States of America 1980LPSC...11.2347C Cratering flow fields: Implications for the excavation and transient expansion stages of crater formation Steven Kent Croft Lunar and Planetary Institute, 3303 NASA Road I, Houston, Texas 77058 Abstract-A Maxwell Z-model cratering flow field originating at non-zero depths-of-burst has been used to calculate theoretical depths and volumes of excavation, hinge radii, ejection angles, and transient structural rim uplifts for comparison with experimental and field data from impact and explosion craters. The model flow fields match the observed data well for values of Z between 2.5 and 3.0 for both explosion and impact craters, and effective depths-of-burst near one projectile di- ameter for impacts. The model flow field is therefore inferred to be a reasonable first-order quantitative approximation for several important crater structures, and to embody the important qualitative fea- tures of impact and explosion cratering flows. Formation of a hinge about which the coherent ejecta flap rotates at the rim of the transient crater divides material in the flow field into ejected and down- ward and outward-driven portions. Ejected material originates from an excavation cavity which has a geometry distinct from the transient crater. The excavation cavity and transient crater have the same diameter, D1c, but the depth of the excavation cavity is -0. I D1c, or about one-third of the transient crater depth, and, in the case of simple bowl-shaped craters, about one-half the depth of the final apparent crater. -
SMART-1 Lunar Highlights Bernard H
SMART-1 lunar highlights Bernard H. Foing & SMART-1 Project & Operations team, SMART-1 Science Technology Working Team, SMART-1 Impact Campaign Team http://sci.esa.int/smart-1/, www.esa.int BHF 2007 Europe to the Moon: spacecraft, launch, operations (ESA+ industry) Instruments PIs + TIs from 5 countries Co-Is from 13 ESA + 6 non European countries BHF 2007 Solar Electric Primary Propulsion: 7 g thrust, 60 liters Xenon to the Moon BHF 2007 SMART-1: With Sun power to the Moon on 60 liters of fuel BHF 2007 Solar Electric Propulsion to the Moon – Launched 27 Sept 2003 as Auxiliary passenger on Ariane 5 into Geostationary Transfer Orbit – Spiral out cruise (13.5 month): – lunar capture 15 November 2004, spiral down – arrival 15 March 05 science(450 -2900 km): commissioned spacecraft/instruments at Moon, nominal science mission March-July 05 – reboosting 2 aug-15 Sept 05 to increase orbit lifetime for extension phase until Aug 2006 BHF 2007 AMIE /SMART-1 End August 2006 Earth set & rise from the Moon X AMIE /SMART-1 May 21st, 2004 Earth view from ~70’000 km BHF 2007 First European Far Side Image of The Moon by AMIE/SMART-1 North Pole 12 Nov. 2004 BHF 2007 Moon Phase & Mission Extension MISSION EXTENSION Apolune Perilune Moon Radius BHF 2007 Sun SMART-1 light Reflecte d Sun Triple junction solar cells Multicolor microcamera light KA-band antenna Laser Link Communication X-Ray Spectrometer On-board computer Lithium ion batteries Infrared Spectrometer OBAN Platform Autonomy Technologies Miniaturisation BHF 2007 SMART-1 Science and Exploration Themes -
Water on the Moon, III. Volatiles & Activity
Water on The Moon, III. Volatiles & Activity Arlin Crotts (Columbia University) For centuries some scientists have argued that there is activity on the Moon (or water, as recounted in Parts I & II), while others have thought the Moon is simply a dead, inactive world. [1] The question comes in several forms: is there a detectable atmosphere? Does the surface of the Moon change? What causes interior seismic activity? From a more modern viewpoint, we now know that as much carbon monoxide as water was excavated during the LCROSS impact, as detailed in Part I, and a comparable amount of other volatiles were found. At one time the Moon outgassed prodigious amounts of water and hydrogen in volcanic fire fountains, but released similar amounts of volatile sulfur (or SO2), and presumably large amounts of carbon dioxide or monoxide, if theory is to be believed. So water on the Moon is associated with other gases. Astronomers have agreed for centuries that there is no firm evidence for “weather” on the Moon visible from Earth, and little evidence of thick atmosphere. [2] How would one detect the Moon’s atmosphere from Earth? An obvious means is atmospheric refraction. As you watch the Sun set, its image is displaced by Earth’s atmospheric refraction at the horizon from the position it would have if there were no atmosphere, by roughly 0.6 degree (a bit more than the Sun’s angular diameter). On the Moon, any atmosphere would cause an analogous effect for a star passing behind the Moon during an occultation (multiplied by two since the light travels both into and out of the lunar atmosphere). -
Apollo Over the Moon: a View from Orbit (Nasa Sp-362)
chl APOLLO OVER THE MOON: A VIEW FROM ORBIT (NASA SP-362) Chapter 1 - Introduction Harold Masursky, Farouk El-Baz, Frederick J. Doyle, and Leon J. Kosofsky [For a high resolution picture- click here] Objectives [1] Photography of the lunar surface was considered an important goal of the Apollo program by the National Aeronautics and Space Administration. The important objectives of Apollo photography were (1) to gather data pertaining to the topography and specific landmarks along the approach paths to the early Apollo landing sites; (2) to obtain high-resolution photographs of the landing sites and surrounding areas to plan lunar surface exploration, and to provide a basis for extrapolating the concentrated observations at the landing sites to nearby areas; and (3) to obtain photographs suitable for regional studies of the lunar geologic environment and the processes that act upon it. Through study of the photographs and all other arrays of information gathered by the Apollo and earlier lunar programs, we may develop an understanding of the evolution of the lunar crust. In this introductory chapter we describe how the Apollo photographic systems were selected and used; how the photographic mission plans were formulated and conducted; how part of the great mass of data is being analyzed and published; and, finally, we describe some of the scientific results. Historically most lunar atlases have used photointerpretive techniques to discuss the possible origins of the Moon's crust and its surface features. The ideas presented in this volume also rely on photointerpretation. However, many ideas are substantiated or expanded by information obtained from the huge arrays of supporting data gathered by Earth-based and orbital sensors, from experiments deployed on the lunar surface, and from studies made of the returned samples. -
APOLLO 15 OBSERVATIONS; Farouk El-Baz, Lunar Explora- Tion Department, Bellcomm, Washington, D.C
APOLLO 15 OBSERVATIONS; Farouk El-Baz, Lunar Explora- tion Department, Bellcomm, Washington, D.C. 20024; A. M. Worden and V. D. Brand, Astronaut Office, Manned Spacecraft Center, Houston, Texas 77058 Visual observations from lunar orbit constitute a signif- icant complement to photography and other remote-sensed data. Utilization of the capabilities of a well-trained observer in lunar orbit is an illustration of the role of man in space flight. This is particularly significant when one considers the special characteristics of the human eye and the interpretive powers of the brain. The unaided eye resolves 20-30 m objects from 110 km orbit. It is also especially equipped, through its wide dynamic range, to distinguish subtle differences in bright- ness levels, color tones, topographic expressions and textural variations. Fifteen lunar surface areas were studied in detail from lunar orbit on Apollo 15. The wide field of view allowed in- vestigation of both the general and local settings at varying sun elevation angles and viewing directions. "On the scene" interpretations were made and later checked and confirmed on successive orbits. In certain cases, features and phenomena were compared to similar occurrences in other parts of the groundtracks. Results of the observation of eight targets are given and an example is provided of the geologic significance of observing cinder cones on the southeastern rim of Mare Serenitatis. The more significant observations were made of the following features starting with the most easterly target: 1) Swirls of light colored markings on the floor of Mare Inginii on the lunar farside. No topographic expressions are associated with these sinuous markings which appear to have been the result of a "bleaching" mechanism. -
Master's Thesis
2009:106 MASTER'S THESIS Design a Nano-Satellite for Observation of Transient Lunar Phenomena(TLP) Bao Han Luleå University of Technology Master Thesis, Continuation Courses Space Science and Technology Department of Space Science, Kiruna 2009:106 - ISSN: 1653-0187 - ISRN: LTU-PB-EX--09/106--SE Design a Nano-Satellite for Observation of Transient Lunar Phenomena (TLP) SpaceMaster Thesis I Students: Bao Han Supervisor: Prof. Dr. Hakan Kayal Date of Submission: 24 Sep 2009 II DECLARATION I hereby declare that this submission is my own work and that, to the best of my knowledge and belief, it contains no material previously published or written by other person or material which to a substantial extent has been accepted for the award of other degree or diploma of university or other institute of high learning, except due acknowledgment has been made in the text. Würzburg, the 20th, September, 2009 _______________________ (Bao Han) III ACKNOWLEGMENT I would like to express my gratitude to all those who gave me the possibility to complete this thesis. First I am deeply indebted to my supervisor Prof. Dr. Hakan Kayal for providing me the possibility to do a very interesting and changeling master thesis by contributing to the Nano-Satellite project and his stimulating suggestions and encouragement helped me in all the time of research for and writing of this thesis. This thesis work allowed me to have a good insight in the Nano-satellite project while gaining many satellite system design experience in many fields. I have furthermore to thank the Prof. Klaus Schilling, the chair of the computer science VII department, who encouraged me to go ahead with my thesis. -
Apollo 15 Index of 70Mm Photographs
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION APOLLO 15 INDEX OF 70 mm PHOTOGRAPHS JANUARY 12, 1972 MAPPING SCIENCES BRANCH EARTH OBSERVATIONS DIVISION SCIENCE AND APPLICATIONS DIRECTORATE MANNED SPACECRAFT CENTER HOUSTON,TEXAS APOLLO 15 INDEX OF 70mm PHOTOGRAPHS January 12, 1972 Prepared for: Mapping Sciences Branch Earth Observations Division National Aeronautics and Space Administration Manned Spacecraft Center Houston, Texas Scanned and converted to PDF format by Matthew Kay [email protected] May 2002 PREFACE This report was prepared by Lockheed Electronics Company, Inc., Houston Aerospace Systems Division, under Contract NAS 9-12200, Project Work Order 63-0117-5714, and issued at the Manned Spacecraft Center, Houston, Texas. The major contributors to this document were R. G. Cook, R. A. Pinter and F. W. Solomon of the Image Analysis Section with the support of personnel of the Mapping Science Department. APOLLO 15 INDEX OF 70 MM PHOTOGRAPHS Prepared By: Lockheed Electronics Company, Inc., HASD Mapping Sciences Department For Mapping Sciences Branch of the Earth Observations Division National Aeronautics and Space Administration Manned Spacecraft Center Houston, Texas Dr. M. C. McEwen Approved By: Head, Lunar Screening & Indexing Group Mapping Sciences Branch/EOD January 12, 1972 Issue Date Apollo 15 Index of 70mm Photographs TABLE OF CONTENTS Page Introduction . 1 Sources of Information . 3 Index by NASA Photo Numbers Magazine QQ, AS15-81-10869 to 11046 . 10 Magazine SS, AS15-82-11047 to 11217 . 22 Magazine MM, AS15-84-11235 to 11352 . 34 Magazine LL, AS15-85-11353 to 11529 . 42 Magazine NN, AS15-86-11530 to 11694 . 54 Magazine KK, AS15-87-11695 to 11860 . -
Calibration Targets
EUROPE TO THE MOON: HIGHLIGHTS OF SMART-1 MISSION Bernard H. FOING, ESA SCI-S, SMART-1 Project Scientist J.L. Josset , M. Grande, J. Huovelin, U. Keller, A. Nathues, A. Malkki, P. McMannamon, L.Iess, C. Veillet, P.Ehrenfreund & SMART-1 Science & Technology Working Team STWT M. Almeida, D. Frew, D. Koschny, J. Volp, J. Zender, RSSD & STOC G. Racca & SMART-1 Project ESTEC , O. Camino-Ramos & S1 Operations team ESOC, [email protected], http://sci.esa.int/smart-1/, www.esa.int SMART-1 project team Science Technology Working Team & ESOC Flight Control Team EUROPE TO THE MOON: HIGHLIGHTS OF SMART-1 MISSION Bernard H. Foing & SMART-1 Project & Operations team, SMART-1 Science Technology Working Team, SMART-1 Impact Campaign Team http://sci.esa.int/smart-1/, www.esa.int ESA Science programme Mars Express Smart 1 Chandrayaan1 Beagle 2 Cassini- Huygens Solar System Venus Express 05 Solar Orbiter Rosetta 04 2017 BepiColombo 2013 SMART-1 Mission SMART-1 web page (http://sci.esa.int/smart-1/) • ESA SMART Programme: Small Missions for Advanced Research in Technology – Spacecraft & payload technology demonstration for future cornerstone missions – Management: faster, smarter, better (& harder) – Early opportunity for science SMART-1 Solar Electric Propulsion to the Moon – Test for Bepi Colombo/Solar Orbiter – Mission approved and payload selected 99 – 19 kg payload (delivered August 02) – 370 kg spacecraft – launched Ariane 5 on 27 Sept 03, Kourou Europe to the Moon Some of the Innovative Technologies on Smart-1 Sun SMART-1 light Reflecte d Sun -
Crater Size-Frequency Distribution Measurements of Mare Crisium
42nd Lunar and Planetary Science Conference (2011) 2179.pdf CRATER SIZE-FREQUENCY DISTRIBUTION MEASUREMENTS OF MARE CRISIUM. H. Hiesinger1, C. H. van der Bogert1, D. Reiss1, and M. S. Robinson2, 1Institut für Planetologie, Westfälische Wilhelms- Universität, Wilhelm-Klemm-Str. 10, 48149 Münster, Germany ([email protected]), 2Arizona State Uni- versity, Tempe, AZ, USA. Introduction: Mare Crisium is located between region of the basin was also mapped as Eratosthenian 10° and 30º N and 50° and 70º E on the lunar nearside. or Imbrian basalts (EIm). This unit roughly corre- Previous work [1] identified three major basalt groups sponds to the Group I basalts of [1]. The geologic map within the basin (Fig. 1). The soils formed from a Fe- of [3] also shows mostly Imbrian ages for the mare and Mg-rich high Ti basalt similar to Luna 16 samples basalts in southern Mare Crisium, except for two (Group I), a very low Ti ferrobasalt similar to Luna 24 small, isolated areas east of Picard X, which were samples (Group II), and a low Ti ferrobasalt similar to mapped as Eratosthenian or Imbrian basalts (EIm). Apollo 12 samples (Group III). Group I basalts appear Radiometric ages of the Luna 24 samples indicate ages to be the oldest deposits in the basin, as they are only of 3.34 to 3.44 Ga [4] or 2.52-3.45 Ga [5]. Crater deg- exposed in the topographically higher SE region of the radation ages of [6] show an age of 3.50 Ga for the basin and are excavated by major post-mare impact Luna 24 landing site (Fig.