Mineralogical and Chemical Properties Inversed from 21-Lunar-Day VNIS
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Aitken Basin
Geological and geochemical analysis of units in the South Pole – Aitken Basin A.M. Borst¹,², F.S. Bexkens¹,², B. H. Foing², D. Koschny² ¹ Department of Petrology, VU University Amsterdam ² SCI-S. Research and Scientific Support Department, ESA – ESTEC Student Planetary Workshop 10-10-2008 ESA/ESTEC The Netherlands The South Pole – Aitken Basin Largest and oldest Lunar impact basin - Diameter > 2500 km - Depth > 12 km - Age 4.2 - 3.9 Ga Formed during Late heavy bombardment? Window into the interior and evolution of the Moon Priority target for future sample return missions Digital Elevation Model from Clementine altimetry data. Produced in ENVI, 50x vertical exaggeration, orthographic projection centered on the far side. Red +10 km, purple/black -10km. (A.M.Borst et.al. 2008) 1 The Moon and the SPA Basin Geochemistry Iron map South Pole – Aitken Basin mafic anomaly • High Fe, Th, Ti and Mg abundances • Excavation of mafic deep crustal / upper mantle material Thorium map Clementine 750 nm albedo map from USGS From Paul Lucey, J. Geophys. Res., 2000 Map-a-Planet What can we learn from the SPA Basin? • Large impacts; Implications and processes • Volcanism; Origin, age and difference with near side mare basalts • Cratering record; Age, frequency and size distribution • Late Heavy Bombardment; Intensity, duration and origin • Composition of the deeper crust and possibly upper mantle 2 Topics of SPA Basin study 1) Global structure of the basin (F.S. Bexkens et al, 2008) • Rims, rings, ejecta distribution, subsequent craters modifications, reconstructive -
Project Selene: AIAA Lunar Base Camp
Project Selene: AIAA Lunar Base Camp AIAA Space Mission System 2019-2020 Virginia Tech Aerospace Engineering Faculty Advisor : Dr. Kevin Shinpaugh Team Members : Olivia Arthur, Bobby Aselford, Michel Becker, Patrick Crandall, Heidi Engebreth, Maedini Jayaprakash, Logan Lark, Nico Ortiz, Matthew Pieczynski, Brendan Ventura Member AIAA Number Member AIAA Number And Signature And Signature Faculty Advisor 25807 Dr. Kevin Shinpaugh Brendan Ventura 1109196 Matthew Pieczynski 936900 Team Lead/Operations Logan Lark 902106 Heidi Engebreth 1109232 Structures & Environment Patrick Crandall 1109193 Olivia Arthur 999589 Power & Thermal Maedini Jayaprakash 1085663 Robert Aselford 1109195 CCDH/Operations Michel Becker 1109194 Nico Ortiz 1109533 Attitude, Trajectory, Orbits and Launch Vehicles Contents 1 Symbols and Acronyms 8 2 Executive Summary 9 3 Preface and Introduction 13 3.1 Project Management . 13 3.2 Problem Definition . 14 3.2.1 Background and Motivation . 14 3.2.2 RFP and Description . 14 3.2.3 Project Scope . 15 3.2.4 Disciplines . 15 3.2.5 Societal Sectors . 15 3.2.6 Assumptions . 16 3.2.7 Relevant Capital and Resources . 16 4 Value System Design 17 4.1 Introduction . 17 4.2 Analytical Hierarchical Process . 17 4.2.1 Longevity . 18 4.2.2 Expandability . 19 4.2.3 Scientific Return . 19 4.2.4 Risk . 20 4.2.5 Cost . 21 5 Initial Concept of Operations 21 5.1 Orbital Analysis . 22 5.2 Launch Vehicles . 22 6 Habitat Location 25 6.1 Introduction . 25 6.2 Region Selection . 25 6.3 Locations of Interest . 26 6.4 Eliminated Locations . 26 6.5 Remaining Locations . 27 6.6 Chosen Location . -
Martian Crater Morphology
ANALYSIS OF THE DEPTH-DIAMETER RELATIONSHIP OF MARTIAN CRATERS A Capstone Experience Thesis Presented by Jared Howenstine Completion Date: May 2006 Approved By: Professor M. Darby Dyar, Astronomy Professor Christopher Condit, Geology Professor Judith Young, Astronomy Abstract Title: Analysis of the Depth-Diameter Relationship of Martian Craters Author: Jared Howenstine, Astronomy Approved By: Judith Young, Astronomy Approved By: M. Darby Dyar, Astronomy Approved By: Christopher Condit, Geology CE Type: Departmental Honors Project Using a gridded version of maritan topography with the computer program Gridview, this project studied the depth-diameter relationship of martian impact craters. The work encompasses 361 profiles of impacts with diameters larger than 15 kilometers and is a continuation of work that was started at the Lunar and Planetary Institute in Houston, Texas under the guidance of Dr. Walter S. Keifer. Using the most ‘pristine,’ or deepest craters in the data a depth-diameter relationship was determined: d = 0.610D 0.327 , where d is the depth of the crater and D is the diameter of the crater, both in kilometers. This relationship can then be used to estimate the theoretical depth of any impact radius, and therefore can be used to estimate the pristine shape of the crater. With a depth-diameter ratio for a particular crater, the measured depth can then be compared to this theoretical value and an estimate of the amount of material within the crater, or fill, can then be calculated. The data includes 140 named impact craters, 3 basins, and 218 other impacts. The named data encompasses all named impact structures of greater than 100 kilometers in diameter. -
POLYGONAL IMPACT CRATERS on CHARON. C.B. Beddingfield1,2, R
51st Lunar and Planetary Science Conference (2020) 1241.pdf POLYGONAL IMPACT CRATERS ON CHARON. C.B. Beddingfield1,2, R. Beyer1,2, R.J. Cartwright1,2, K. Singer3, S. Robbins3, S.A. Stern3, V. Bray4, J.M. Moore2, K. Ennico2, C.B. Olkin3, J.R. Spencer3, H.A. Weaver5, L.A. Young3, A.Verbiscer6, J. Parker3, and the New Horizons Geology, Geophysics, and Imaging (GGI) Team; 1SETI In- stitute, Mountain View, CA, 2NASA Ames Research Center, Mountain View, CA ([email protected]), 3Southwest Research Institute, Boulder, CO, 4University of Arizona, Tucson, AZ, 5John Hopkins University Applied Physics Laboratory, Laurel, MD, 6University of Virginia, Charlottesville, VA. Introduction: Polygonal impact craters (PICs) re- flect pre-existing extensional and strike-slip faults and fractures in the target material [e.g. 1-9]. PIC straight rim segments therefore can provide important infor- mation for deciphering the tectonic histories of plane- tary bodies [e.g. 8]. The only known PIC formation mechanism is the presence of pre-existing sub-vertical structures within the target material [e.g. 5, 7, 11-13]. In contrast, circular impact craters (CICs) are in- ferred to result from impact events in non-tectonized target material. CICs can also form in pre-fractured tar- get material if the fractures are widely or closely spaced, if the fracture system is highly complex, or if the target material is covered by a thick layer of non-cohesive sed- iment that limits interactions between the impactor and the underlying bedrock/ice [e.g. 14]. Consequently, PICs and CICs are useful tools to distinguish between Fig. -
Mobile Lunar and Planetary Base Architectures
Space 2003 AIAA 2003-6280 23 - 25 September 2003, Long Beach, California Mobile Lunar and Planetary Bases Marc M. Cohen, Arch.D. Advanced Projects Branch, Mail Stop 244-14, NASA-Ames Research Center, Moffett Field, CA 94035-1000 TEL 650 604-0068 FAX 650 604-0673 [email protected] ABSTRACT This paper presents a review of design concepts over three decades for developing mobile lunar and planetary bases. The idea of the mobile base addresses several key challenges for extraterrestrial surface bases. These challenges include moving the landed assets a safe distance away from the landing zone; deploying and assembling the base remotely by automation and robotics; moving the base from one location of scientific or technical interest to another; and providing sufficient redundancy, reliability and safety for crew roving expeditions. The objective of the mobile base is to make the best use of the landed resources by moving them to where they will be most useful to support the crew, carry out exploration and conduct research. This review covers a range of surface mobility concepts that address the mobility issue in a variety of ways. These concepts include the Rockwell Lunar Sortie Vehicle (1971), Cintala’s Lunar Traverse caravan, 1984, First Lunar Outpost (1992), Frassanito’s Lunar Rover Base (1993), Thangavelu’s Nomad Explorer (1993), Kozlov and Shevchenko’s Mobile Lunar Base (1995), and the most recent evolution, John Mankins’ “Habot” (2000-present). The review compares the several mobile base approaches, then focuses on the Habot approach as the most germane to current and future exploration plans. -
Secondary Craters on Europa and Implications for Cratered Surfaces
Vol 437|20 October 2005|doi:10.1038/nature04069 LETTERS Secondary craters on Europa and implications for cratered surfaces Edward B. Bierhaus1, Clark R. Chapman2 & William J. Merline2 For several decades, most planetary researchers have regarded the craters were typically not spatially random, but instead appeared in impact crater populations on solid-surfaced planets and smaller clumps and clusters16 even at distances far (several hundred kilo- bodies as predominantly reflecting the direct (‘primary’) impacts metres) from the nearest large primary crater. This clustered spatial of asteroids and comets1. Estimates of the relative and absolute distribution contrasts with primary impacts, which are spatially ages of geological units on these objects have been based on this random. The low spatial density and unusual non-random spatial assumption2. Here we present an analysis of the comparatively distribution of Europa’s small craters enabled us to achieve what has sparse crater population on Jupiter’s icy moon Europa and suggest been previously difficult, namely unambiguous identification and that this assumption is incorrect for small craters. We find that quantification of the contribution of distant secondary craters to the ‘secondaries’ (craters formed by material ejected from large total crater SFD. This, in turn, allows us to re-examine the overall primary impact craters) comprise about 95 per cent of the small crater age-dating methodology. We discuss the specifics of the craters (diameters less than 1 km) on Europa. We therefore con- Europa data first. clude that large primary impacts into a solid surface (for example, We measured more than 17,000 craters in 87 low-compression, ice or rock) produce far more secondaries than previously low-sun, high-resolution Europa images (scales ,60 m pixel21), believed, implying that the small crater populations on the which cover nine regions totalling 0.2% of Europa’s surface (a much Moon, Mars and other large bodies must be dominated by larger percentage of Europa has been imaged at lower resolutions), secondaries. -
Salubrious Living
Salubrious Living 00. Salubrious Living - Introduction 01. The Search for Youth 02. The Myth of Medical Progress 03. The Hygienic System 04. The Nature of Disease 05. The Foods of Civilization 06. The Foods of Primitive Man 07. Don't Cook Your Foods 08. The Fruitarian Diet 09. How to Plan Your Meals 10. The Best Sources of Minerals and Vitamins 11. Soil and Food 12. Nature's Supreme Healing Agency 13. The Value of Heliotherapy 14. Building Strength and Health Through Exercise 15. Some Common Ailments 16. Why Lose Your Teeth? 17. Better Vision Without Glasses 18. Building Strong Feet 19. Keep Your Hair 20. The Needs of Infants and Growing Children 21. To Build Beauty You Must Build Health 22. Eugenics and the Survival of the White Race Author: Ben Klassen Format: Paperback Creativity Book Publisher Pub. Date: 1982 Food Chart Copyright © 2003 by World Church of Creativity Salubrious Living - Introduction The term "Salubrious Living" is a nomenclature I have coined as part and parcel of a very important facet of our religious creed and program set forth by the CHURCH OF THE CREATOR. The word "salubrious" comes from the Latin word "salubris" meaning "healthy; wholesome; sound; useful; vigorous". Webster's dictionary defines the English derivative "salubrious" as: 1. favorable to, or promoting health or well being; invigorating; 2. spiritually wholesome; conducive to good results". It is in this context of fully promoting the health and well being of the White Race that we use this term in its true literal meaning. We of the CHURCH OF THE CREATOR want to differentiate this term from "Natural Hygiene popularly used for many decades by health practitioners devoted to this worthy art and science. -
A Lunar Micro Rover System Overview for Aiding Science and ISRU Missions Virtual Conference 19–23 October 2020 R
i-SAIRAS2020-Papers (2020) 5051.pdf A lunar Micro Rover System Overview for Aiding Science and ISRU Missions Virtual Conference 19–23 October 2020 R. Smith1, S. George1, D. Jonckers1 1STFC RAL Space, R100 Harwell Campus, OX11 0DE, United Kingdom, E-mail: [email protected] ABSTRACT the form of rovers and landers of various size [4]. Due to the costly nature of these missions, and the pressure Current science missions to the surface of other plan- for a guaranteed science return, they have been de- etary bodies tend to be very large with upwards of ten signed to minimise risk by using redundant and high instruments on board. This is due to high reliability re- reliability systems. This further increases mission cost quirements, and the desire to get the maximum science as components and subsystems are expected to be ex- return per mission. Missions to the lunar surface in the tensively qualified. next few years are key in the journey to returning hu- mans to the lunar surface [1]. The introduction of the As an example, the Mars Science Laboratory, nick- Commercial lunar Payload Services (CLPS) delivery named the Curiosity rover, one of the most successful architecture for science instruments and technology interplanetary rovers to date, has 10 main scientific in- demonstrators has lowered the barrier to entry of get- struments, requires a large team of people to control ting science to the surface [2]. Many instruments, and and cost over $2.5 billion to build and fly [5]. Curios- In Situ Surface Utilisation (ISRU) experiments have ity had 4 main science goals, with the instruments and been funded, and are being built with the intention of the design of the rover specifically tailored to those flying on already awarded CLPS missions. -
PROJECT PENGUIN Robotic Lunar Crater Resource Prospecting VIRGINIA POLYTECHNIC INSTITUTE & STATE UNIVERSITY Kevin T
PROJECT PENGUIN Robotic Lunar Crater Resource Prospecting VIRGINIA POLYTECHNIC INSTITUTE & STATE UNIVERSITY Kevin T. Crofton Department of Aerospace & Ocean Engineering TEAM LEAD Allison Quinn STUDENT MEMBERS Ethan LeBoeuf Brian McLemore Peter Bradley Smith Amanda Swanson Michael Valosin III Vidya Vishwanathan FACULTY SUPERVISOR AIAA 2018 Undergraduate Spacecraft Design Dr. Kevin Shinpaugh Competition Submission i AIAA Member Numbers and Signatures Ethan LeBoeuf Brian McLemore Member Number: 918782 Member Number: 908372 Allison Quinn Peter Bradley Smith Member Number: 920552 Member Number: 530342 Amanda Swanson Michael Valosin III Member Number: 920793 Member Number: 908465 Vidya Vishwanathan Dr. Kevin Shinpaugh Member Number: 608701 Member Number: 25807 ii Table of Contents List of Figures ................................................................................................................................................................ v List of Tables ................................................................................................................................................................vi List of Symbols ........................................................................................................................................................... vii I. Team Structure ........................................................................................................................................................... 1 II. Introduction .............................................................................................................................................................. -
The Composition of the Lunar Crust: Radiative Transfer Modeling and Analysis of Lunar Visible and Near-Infrared Spectra
THE COMPOSITION OF THE LUNAR CRUST: RADIATIVE TRANSFER MODELING AND ANALYSIS OF LUNAR VISIBLE AND NEAR-INFRARED SPECTRA A DISSERTATION SUBMITTED TO THE GRADUATE DIVISION OF THE UNIVERSITY OF HAWAI‘I IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF DOCTOR OF PHILOSOPHY IN GEOLOGY AND GEOPHYSICS DECEMBER 2009 By Joshua T.S. Cahill Dissertation Committee: Paul G. Lucey, Chairperson G. Jeffrey Taylor Patricia Fryer Jeffrey J. Gillis-Davis Trevor Sorensen Student: Joshua T.S. Cahill Student ID#: 1565-1460 Field: Geology and Geophysics Graduation date: December 2009 Title: The Composition of the Lunar Crust: Radiative Transfer Modeling and Analysis of Lunar Visible and Near-Infrared Spectra We certify that we have read this dissertation and that, in our opinion, it is satisfactory in scope and quality as a dissertation for the degree of Doctor of Philosophy in Geology and Geophysics. Dissertation Committee: Names Signatures Paul G. Lucey, Chairperson ____________________________ G. Jeffrey Taylor ____________________________ Jeffrey J. Gillis-Davis ____________________________ Patricia Fryer ____________________________ Trevor Sorensen ____________________________ ACKNOWLEDGEMENTS I must first express my love and appreciation to my family. Thank you to my wife Karen for providing love, support, and perspective. And to our little girl Maggie who only recently became part of our family and has already provided priceless memories in the form of beautiful smiles, belly laughs, and little bear hugs. The two of you provided me with the most meaningful reasons to push towards the "finish line". I would also like to thank my immediate and extended family. Many of them do not fully understand much about what I do, but support the endeavor acknowledging that if it is something I’m willing to put this much effort into, it must be worthwhile. -
Workshop on Geology of the Apollo 17 Landing Site
NASA-CR-191637 \ WORKSHOP ON GEOLOGY OF THE APOLLO 17 LANDING SITE (NASA-CR-191637) WORKSHOP ON N93-18786 GEOLOGY OF THE APOLLO 17 LANDING --THRU-- SITE (Lunar Science Inst.) 70 p N93-18817 Unclas G3/91 0141290 __ LPI Technical Report Number 92-09, Part 1 LUNAR AND PLANETARY INSTITUTE 3600 BAY AREA BOULEVARD HOUSTON TX 77058-1113 LPI/TR--92-09, Part 1 WORKSHOP ON GEOLOGY OF THE APOLLO 17 LANDING SITE Edited by G. Ryder, H. H. Schmitt, and P. D. Spudis Held at Houston, Texas December 2-4, 1992 Sponsored by Lunar and Planetary Sample Team Lunar and Planetary Institute Lunar and Planetary Institute 3600 Bay Area Boulevard Houston TX 77058-1113 LPI Technical Report Number 92-09, Part 1 LPI/TR--92-09, Part 1 Compiledin 1992by LUNAR AND PLANETARY INSTITUTE TheInstituteis operatedby theUniversitySpaceResearchAssociationunderContractNo. NASW- 4574with theNationalAeronauticsandSpaceAdministration. Materialin this volume may be copied without restraint for library, abstract service, education, or per- sonal research purposes; however, republication of any paper or portion thereof requires the written permission of the authors as well as the appropriate acknowledgment of this publication. This report may be cited as Ryder G., Schmitt H. H., and Spudis P. D., eds. (1992) Workshop on Geology of the Apollo 17 Landing Site. LPI Tech. Rpt. 92-09, Part 1, Lunar and Planetary Institute, Houston. 63 pp. This report is distributed by ORDER DEPARTMENT Lunar and Planetary Institute 3600 Bay Area Boulevard Houston TX 77058-1113 Mail order requestors will be invoiced for the cost of shipping and handling. Cover: Station 4 at Taurus-LiUrow, Apollo 17 landing site. -
South Pole-Aitken Basin
Feasibility Assessment of All Science Concepts within South Pole-Aitken Basin INTRODUCTION While most of the NRC 2007 Science Concepts can be investigated across the Moon, this chapter will focus on specifically how they can be addressed in the South Pole-Aitken Basin (SPA). SPA is potentially the largest impact crater in the Solar System (Stuart-Alexander, 1978), and covers most of the central southern farside (see Fig. 8.1). SPA is both topographically and compositionally distinct from the rest of the Moon, as well as potentially being the oldest identifiable structure on the surface (e.g., Jolliff et al., 2003). Determining the age of SPA was explicitly cited by the National Research Council (2007) as their second priority out of 35 goals. A major finding of our study is that nearly all science goals can be addressed within SPA. As the lunar south pole has many engineering advantages over other locations (e.g., areas with enhanced illumination and little temperature variation, hydrogen deposits), it has been proposed as a site for a future human lunar outpost. If this were to be the case, SPA would be the closest major geologic feature, and thus the primary target for long-distance traverses from the outpost. Clark et al. (2008) described four long traverses from the center of SPA going to Olivine Hill (Pieters et al., 2001), Oppenheimer Basin, Mare Ingenii, and Schrödinger Basin, with a stop at the South Pole. This chapter will identify other potential sites for future exploration across SPA, highlighting sites with both great scientific potential and proximity to the lunar South Pole.