Lunar and Planetary Bases, Habitats, and Colonies
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Advances in the Interpretation and Analysis of Lunar Occultation Light Curves
A&A 538, A56 (2012) Astronomy DOI: 10.1051/0004-6361/201118476 & c ESO 2012 Astrophysics Advances in the interpretation and analysis of lunar occultation light curves A. Richichi1,2 and A. Glindemann2 1 National Astronomical Research Institute of Thailand, 191 Siriphanich Bldg., Huay Kaew Rd., Suthep, Muang, Chiang Mai 50200, Thailand e-mail: [email protected] 2 European Southern Observatory, Karl-Schwarzschild-Str. 2, 85748 Garching bei München, Germany Received 18 November 2011 / Accepted 23 December 2011 ABSTRACT Context. The introduction of fast 2D detectors and the use of very large telescopes have significantly advanced the sensitivity and accuracy of the lunar occultation technique. Recent routine observations at the ESO Very Large Telescope have yielded hundreds of events with results, especially in the area of binary stars, which are often beyond the capabilities of any other techniques. Aims. With the increase in the quality and in the number of the events, subtle features in the light curve patterns have occasionally been detected which challenge the standard analytical definition of the lunar occultation phenomenon as diffraction from an infinite straight edge. We investigate the possible causes for the observed peculiarities. Methods. We have evaluated the available statistics of distortions in occultation light curves observed at the ESO VLT, and compared it to data from other facilities. We have developed an alternative approach to model and interpret lunar occultation light curves, based on 2D diffraction integrals describing the light curves in the presence of an arbitrary lunar limb profile. We distinguish between large limb irregularities requiring the Fresnel diffraction formalism, and small irregularities described by Fraunhofer diffraction. -
Of 13 Human Mars Mission Design – the Ultimate Systems Challenge
Human Mars Mission Design – The Ultimate Systems Challenge John F. Connolly a, B. Kent Joostenb, Bret Drakec, Steve Hoffmanc, Tara Polsgroved, Michelle Ruckera, Alida Andrewsc, Nehemiah Williamsa a NASA Johnson Space Center, 2101 NASA Parkway, Houston, Texas 77058, john.connolly- [email protected], [email protected], [email protected] b Consultant,2383 York Harbour Ct., League City, TX 77573, [email protected] c The Aerospace Corporation, 2310 E El Segundo Blvd, El Segundo, California 90245, [email protected], [email protected], [email protected] d NASA Marshall Space Flight Center, Redstone Arsenal, Huntsville, Alabama 35812, [email protected] Abstract A human mission to Mars will occur at some time in the coming decades. When it does, it will be the end result of a complex network of interconnected design choices, systems analyses, technical optimizations, and non-technical compromises. This mission will extend the technologies, engineering design, and systems analyses to new limits, and may very well be the most complex undertaking in human history. It can be illustrated as a large menu, or as a large decision tree. Whatever the visualization tool, there are numerous design decisions required to assemble a human Mars mission, and many of these interconnect with one another. This paper examines these many decisions and further details a number of choices that are highly interwoven throughout the mission design. The large quantity of variables and their interconnectedness results in a highly complex systems challenge, and the paper illustrates how a change in one variable results in ripples (sometimes unintended) throughout many other facets of the design. -
Isolated and Confined Environments
17 Isolated and Confined Environments Carole Tafforin Ethospace, Toulouse, France Characteristics of space analogue environments with regard to human per- formance concern the crew adaptation in a socio-psychological context and in a temporal dynamics. Isolation, confinement and time are major features on Earth to reproduce an extra-terrestrial environment for manned mission simulations. In the current space missions (low Earth orbit, LEO) and in the perspective of interplanetary missions (near-Earth asteroid, Moon, Mars), men and women will have to adapt to social constraints (crew size, multinationality, mixed-gender) and spatial restrictions (volume, multi-chambers, life-support) on short-term, medium-term and long-term durations. The crewmembers also will have to perform intra-vehicular activities (IVA)and extra-vehicular activ- ities (EVA). For training, preventing and optimizing such tasks, simulations of living and working together in isolated and confined environments, and simulations of operating with a space suit on geological surfaces are the new requirements. During the two decades (1991–2011), space simulators (confinement) and analogue settings (isolation) were adequately developed on Earth with the ultimate goal of walking on Mars. Time periods extended up to 500 days. Space analogue environments are located worldwide (Canada, United States, Russia, Europe, Antarctica and Arctic). Mission durations in space analogue environments cover days, weeks and years. Isolation and confinement facilities implemented for such simulations are listed in Table 17.1. Over a 7-day duration, the Canadian Astronaut Program Space Unit Life Simulation (CAPSULS) was an Earth-based initiative that simulated a typical space shuttle or space station mission [1]. CAPSULS provided the Canadian astronaut participants with space mission training. -
Space Colonies & Lunar Bases
Space Colonies & Why Build Colonies? Lunar Bases ! It isn’t so expensive – US military is many 100’s of billions $ a year ! Fewer casualties than war – 17 astronauts in 45 years of space Karen J. Meech, flight were lost Astronomer ! Humans have an “expansionist” spirit – Much more real estate! ! Valuable resources could be brought to Earth. Institute for Astronomy ! Enough solar energy to rid the world of oil dependency could be brought to Earth for less than the cost of the Iraq war ! Profitable: e.g. 1 Metallic NEO $20 trillion, 3He as a fuel . ! Maybe the time has not yet come, but someday we will need what space can provide Space Habitat Design Shielding – Radiation Protection Considerations ! Shielding characterization ! Aereal density, d [gm/cm2] ! Physiological Needs ! Total amount of material matters ! Shielding ! Type of material: secondary ! Ionizing radiation & particles 3 2 ! Meteoritic impact ! 1 Earth Atmosphere: 10 gm/cm ! Atmospheric containment ! ! = mass / volume ! What pressure needed? ! ! = mass / (area ! thickness) ! Psychological Needs ! What mix of gasses? ! ! = m/(ax) = d / x ! Environment stress ! Gravitational acceleration ! x = thickness = d / ! ! Isolation ! Why it is needed 3 ! Personal space ! How to do it Substance ! [gm/cm ] d / !" x [cm] x [m] ! Illumination / Energy 3 ! Entertainment Lead 8 10 /8 125 1.25 ! ! Aesthetics Food / Water Styrofoam 0.01 103/10-2 105 103 ! Space Requirements Water 1 103/1 103 10 Shielding Types – Active Shielding Types – Passive ! Enough matter between us & radiation ! Examples -
No. 40. the System of Lunar Craters, Quadrant Ii Alice P
NO. 40. THE SYSTEM OF LUNAR CRATERS, QUADRANT II by D. W. G. ARTHUR, ALICE P. AGNIERAY, RUTH A. HORVATH ,tl l C.A. WOOD AND C. R. CHAPMAN \_9 (_ /_) March 14, 1964 ABSTRACT The designation, diameter, position, central-peak information, and state of completeness arc listed for each discernible crater in the second lunar quadrant with a diameter exceeding 3.5 km. The catalog contains more than 2,000 items and is illustrated by a map in 11 sections. his Communication is the second part of The However, since we also have suppressed many Greek System of Lunar Craters, which is a catalog in letters used by these authorities, there was need for four parts of all craters recognizable with reasonable some care in the incorporation of new letters to certainty on photographs and having diameters avoid confusion. Accordingly, the Greek letters greater than 3.5 kilometers. Thus it is a continua- added by us are always different from those that tion of Comm. LPL No. 30 of September 1963. The have been suppressed. Observers who wish may use format is the same except for some minor changes the omitted symbols of Blagg and Miiller without to improve clarity and legibility. The information in fear of ambiguity. the text of Comm. LPL No. 30 therefore applies to The photographic coverage of the second quad- this Communication also. rant is by no means uniform in quality, and certain Some of the minor changes mentioned above phases are not well represented. Thus for small cra- have been introduced because of the particular ters in certain longitudes there are no good determi- nature of the second lunar quadrant, most of which nations of the diameters, and our values are little is covered by the dark areas Mare Imbrium and better than rough estimates. -
Analysis of Photography and Visual Observations
CASE c o ANALYSIS OF PHOTOGRAPHY AND VISUAL OBSERVATIONS NATIONAL AERONAUTICS AN_SP.A_E NASA SP-232 ANALYSIS OF PHOTOGRAPHY AND VISUAL OBSERVATIONS COMPILED BY NASA MANNED SPACECRAFT CENTER Scientific and Technical ln[ormation Office 19"I Is, S._. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Washington, D.C. For sale by the Superintendent of Documents, U.S. Government Printing Office, Washington, D.C. 20402 Price $4.25 Library of Congress Catalog Card Number 72-606239 Foreword The Apollo 10 mission was a vital step toward the national goal of landing men on the Moon and returning them safely to Earth. This mission used the first complete Apollo spacecraft flown in lunar orbit and took men closer to the Moon than ever before. The mission clearly demonstrated that the Nation was ready to embark with the Apollo 11 crew on the voyage that has been the dream of men for thousands of years. Each Apollo lunar mission acquires photographs of areas on the Moon never before seen in such great detail. This report provides only a small sample of the types of analysis that can be performed with this photography. Even more important, however, this report provides scientists throughout the world with a knowledge of what new lunar photography is available and how the photograph can be obtained. It is hoped that more extensive analysis of this photography will continue, and it is certain that the photographs will be used for many decadesl RICHARD J. ALLENBY 01_ice of Manned Space Flight 111 Contents Page INTRODUCTION ........................................ vii Jamcs H. Sasser CHAPTER 1. VISUAL OBSERVATIONS ............. -
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. -
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 . -
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 -
University Microfilms, a XEROX Company, Ann Arbor, Michigan
.72-4480 FAJEMIROKUN, Francis Afolabi, 1941- APPLICATION OF NEW OBSERVATIONAL SYSTEMS FOR SELENODETIC CONTROL. The Ohio State University, Ph.D., 1971 Geodesy University Microfilms, A XEROX Company, Ann Arbor, Michigan THIS DISSERTATION HAS BEEN MICROFILMED EXACTLY AS RECEIVED APPLICATION OF NEW OBSERVATIONAL SYSTEMS FOR SELENODETIC CONTROL DISSERTATION Presented in Partial Fulfillment of the Requirements for the Degree Doctor of Philosophy in the Graduate School of The Ohio State University by Francis Afolabi Fajemirokun, B. Sc., M. Sc. The Ohio State University 1971 Approved by l/m /• A dviser Department of Geodetic Science PLEASE NOTE: Some Pages have indistinct p rin t. Filmed as received. UNIVERSITY MICROFILMS To Ijigbola, Ibeolayemi and Oladunni ACKNOW LEDGEME NTS The author wishes to express his deep gratitude to the many persons, without whom this work would not have been possible. First and foremost, the author is grateful to the Department of Geodetic Science and themembers of its staff, for the financial support and academic guidance given to him during his studies here. In particular, the author wishes to thank his adviser Professor Ivan I. Mueller, for his encouragement, patience and guidance through the various stages of this work. Professors Urho A. Uotila, Richard H. Rapp and Gerald H. Newsom served on the author’s reading committee, and offered many valuable suggestions to help clarify many points. The author has also enjoyed working with other graduate students in the department, especially with the group at 231 Lord Hall, where there was always an atmosphere of enthusiastic learning and of true friendship. The author is grateful to the various scientists outside the department, with whom he had discussions on the subject of this work, especially to the VLBI group at the Smithsonian Astrophysical Observatory in Cambridge, Ma s sachu s s etts . -
1 Lifetime of a Transient Atmosphere Produced by Lunar Volcanism O. J
Lifetime of a transient atmosphere produced by Lunar Volcanism O. J. Tucker1, R. M. Killen1, R. E. Johnson2, P. Saxena1 1NASA Goddard Space Flight Center, Greenbelt, Maryland 20771 2University of Virginia, Charlottesville, Virginia 48109 1 Abstract. Early in the Moon’s history volcanic outgassing may have produced a periodic millibar level atmosphere (Needham and Kring, 2017). We examined the relevant atmospheric escape processes and lifetime of such an atmosphere. Thermal escape rates were calculated as a function of atmospheric mass for a range of temperatures including the effect of the presence of a light constituent such as H2. Photochemical escape and atmospheric sputtering were calculated using estimates of the higher EUV and plasma fluxes consistent with the early Sun. The often used surface Jeans calculation carried out in Vondrak (1974) is not applicable for the scale and composition of the atmosphere considered. We show that solar driven non-thermal escape can remove an early CO millibar level atmosphere on the order of ~1 Myr if the average exobase temperature is below ~ 350 – 400 K. However, if solar UV/EUV absorption heats the upper atmosphere to temperatures > ~ 400 K thermal escape increasingly dominates the loss rate, and we estimated a minimum lifetime of 100’s of years considering energy limited escape. 2 1) Introduction The possibility of harvesting water in support of manned space missions has reinvigorated interest about the inventory of volatiles on our Moon. It has a very tenuous atmosphere primarily composed of the noble gases with sporadic populations of other atoms and molecules. This rarefied envelope of gas, commonly referred to as an exosphere, is derived from the Moon’s surface and subsurface (Killen & Ip, 1999). -
The Association Between the Lunar Cycle and Patterns
THE ASSOCIATION BETWEEN THE LUNAR CYCLE AND PATTERNS OF PATIENT PRESENTATION TO THE EMERGENCY DEPARTMENT. Grant Dudley Futcher Student number: 7709742 A research report submitted to the Faculty of Health Sciences, University of the Witwatersrand, in partial fulfilment of the requirements for the degree of Master of Science in Medicine in Emergency Medicine. Johannesburg, 2015 i DECLARATION I, Grant Dudley Futcher, declare that this research report is my own work. It is being submitted for the degree of Master of Science in Medicine (Emergency Medicine) in the University of the Witwatersrand, Johannesburg. It has not been submitted before for any degree or examination at this or any other University. Signed on 25th day of August 2015 ii DEDICATION This work is dedicated to my children, Charis, Luke and Jarryd, who have patiently endured their father’s choice of medical discipline. iii PUBLICATIONS ARISING FROM THIS STUDY Nil iv ABSTRACT Aim: To determine any association between the lunar synodic or anomalistic months and the nature and volume of emergency department patient consultations and hospital admissions from the emergency department (ED). Design: A retrospective, descriptive study. Setting: All South African EDs of a private hospital group. Patients: All patients consulted from 01 January 2005 to 31 December 2010. Methods: Data was extracted from monthly records and statistically evaluated, controlling for calendric variables. Lunar variables were modelled with volumes of differing priority of hospital admissions and consultation categories including; trauma, medical, paediatric, work injuries, obstetrics and gynaecology, intentional self harm, sexual assault, dog bites and total ED consultations. Main Results: No significant differences were found in all anomalistic and most synodic models with the consultation categories.