Geoscience and a Lunar Base a Comprehensive Plan for Lunar Exploration
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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. -
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. -
Pfizer Vaccine
Find a Walgreens near you to receive an additional dose of the Pfizer COVID-19 vaccine Vaccines subject to availability, State-, age-, and health-related restrictions may apply. PFIZER STORES State Store Address City Zipcode AK 15092 1470 W NORTHERN LIGHTS BLVD ANCHORAGE 99503 AK 13656 725 E NORTHERN LIGHTS BLVD ANCHORAGE 99503 AK 12680 2197 W DIMOND BLVD ANCHORAGE 99515 AK 15653 4353 LAKE OTIS PARKWAY ANCHORAGE 99508 AK 13449 12405 BRANDON ST ANCHORAGE 99515 AK 15654 2550 E 88TH AVE ANCHORAGE 99507 AK 15362 12051 OLD GLENN HWY EAGLE RIVER 99577 AK 15944 530 OLD STEESE HWY FAIRBANKS 99701 AL 9951 9301 HIGHWAY 119 ALABASTER 35007 AL 11279 7155 US HIGHWAY 431 ALBERTVILLE 35950 AL 11819 1401 GOLDEN SPRINGS RD ANNISTON 36207 AL 19256 2413 HIGHWAY 431 NORTH ANNISTON 36206 AL 7951 800 QUINTARD AVE ANNISTON 36201 AL 11651 4700 HIGHWAY 280 BIRMINGHAM 35242 AL 6034 101 GREEN SPRINGS HWY BIRMINGHAM 35209 AL 7791 101 DOUG BAKER BLVD BIRMINGHAM 35242 AL 7245 668 LOMB AVE SW BIRMINGHAM 35211 AL 7306 4496 VALLEYDALE RD BIRMINGHAM 35242 AL 6035 2101 RICHARD ARRINGTON JR BLVD S BIRMINGHAM 35209 AL 15144 3020 CLAIRMONT AVE S BIRMINGHAM 35205 AL 10333 3150 GREEN VALLEY RD BIRMINGHAM 35243 AL 11469 9325 PARKWAY E BIRMINGHAM 35215 AL 4846 2301 CENTER POINT PKWY BIRMINGHAM 35215 AL 10965 920 US HIGHWAY 431 BOAZ 35957 AL 11531 16468 HIGHWAY 280 CHELSEA 35043 AL 15205 444 2ND AVE NW CULLMAN 35055 AL 11180 1700 2ND AVE SW CULLMAN 35055 AL 5606 3025 US HIGHWAY 98 DAPHNE 36526 AL 9976 1127 6TH AVE SE DECATUR 35601 AL 7404 2041 E MAIN ST DOTHAN 36301 AL 7405 2940 -
Mini-RF: Imaging Radars for Exploring the Lunar Poles
Mini-RF: Imaging Radars for Exploring the Lunar Poles Ben Bussey, Paul Spudis, Keith Raney, Helene Winters JHU/APL Stu Nozette, Chris Lichtenberg, Bill Marinelli NAWC 1 Mini-RF Organization, Science and Resource Evaluation Objectives • Mini-RF is a suite of radar instruments funded by NASA (SOMD & ESMD) and DoD. • Search for areas near the lunar poles that have the anomalous radar reflectivity signatures (high radar albedo and Circular Polarization Ratios) that differentiate volumetric water-ice deposits from more typical lunar surfaces • Map the morphology of permanently dark regions near the poles 2 Search for Ice • The case for water-ice can be resolved only if robust and repeatable data of the lunar polar regions support that conclusion. This rigorous standard can be met only by a dedicated polar-orbiting radar. • Mini-RF will use a unique hybrid polarity architecture to look for ice deposits • Transmit circular polarization (e.g. right-circular polarization RCP) • Receive coherent orthogonal polarizations • Derive Stokes parameters of the received signal • Use Stokes parameters to reconstruct and investigate the nature of the backscatter field. Distinguish between surface (roughness) and volume (ice) scattering 3 Top-level Radar Overview Parameter Chandrayaan-1 LRO • Frequency S-band S-band and X-band • Polarization Tx RCP Rx H & V • Scatterometry S-band (none) • Imager Regional maps Site-specific selections • Resolution (m/pixel) 75 75, 7.5 azimuth x 15 range • Looks 16 16 or 8 • Swath (km) 8 6 or 4 • Altitude (km) 100 50 • Incidence -
11 Get Continuances
' 0# triton ti Vo'ume 12, Hum"" 6 University 01 (a'ilornia, San Diego FriJay, January 22, '''' Regent's Meeting UCNewspaper Guidelines Approved With Provisions Carl Neiburger UCSD Vice Chancellor of Student Affairs City Editor George Murphy agreed with Haskins in an The Regents' Committee on Educational interview with the TRITO TIMES . He said Policy approved guidelines for student that before the amendement it was presumed newspapers yesterday. The approval, however, that " the papers would be consistent with the included the understanding that a guidelines" which, he observed, they had helped representative delegated by the chancellor to write. He said that " the reversal (of this review each issue within 24 hours after publication for rule violations. The proposal will come before the full board today for final On Page 3 Interview with approval. WILSON RILES, Supt. of Public Regent John Canaday, who first brought the matter of student papers before the board , Instruction and New UC Regent. introduced the 24 hour provision as one of four provisions he desired to be amended to the guidelines submitted to the Regents. The other presumption ) is what I think is not really three provisions stated that " responsibility for necessary." However, he foresaw no change in the conduct of student publications is vested in administrative policy at UCSD, other than that UCSD Scientists mesmerize media representatives at conference on Tuesday. (story on page 2) the chancellor, that apparent violations of the someone will be required to read the TRfTON -
LPSC Conference Logo
LPSC: 30 YEARS AT A GLANCE This year’s Lunar and Planetary Science Conference marked the 30th anniversary of the conference that had its origins as a controlled report to NASA on the first lunar samples returned to Earth by Apollo 11. In the following pages, we present a retrospective of the conference, including photographs from the past 30 years and insights from LPI scientists and staff members David Black, Paul Spudis, Graham Ryder, LeBecca Simmons, and Pam “The first meeting was at the Albert Thomas Convention Center. I stayed Thompson. The quotations were taken from in the Old Rice Hotel. It was cold, a blue norther had come through. an informal roundtable discussion on the We’re standing in about 30 degrees, we had the windows closed, and we history and origins of the conference. The had towels up against the windows. It was freezing. When I came back 30th LPSC, held at Johnson Space Center for the 20th, the conference had taken on this wide and diverse topical and the Lunar and Planetary Institute in nature, with numerous sessions instead of just one. There were Houston, March 15–19, 1999, again obviously changes in the faces — although some of the same faces were attracted a record-breaking number of there, — but it was the structure of the meeting that changed so much.” abstracts and attendees. The official count — David Black, LPI Director, who tallied 1052 abstracts submitted and 1071 attended the first conference as a graduate student and then did not people attending the conference. attend again for 20 years L U N A R A N D P L A N E T A R Y I N F O R M A T I O N B U L L E T I N 2 “The conference started out as a way to embargo the results of lunar sample stuff — so no one would scoop anyone else. -
Lunar Sourcebook : a User's Guide to the Moon
4 LUNAR SURFACE PROCESSES Friedrich Hörz, Richard Grieve, Grant Heiken, Paul Spudis, and Alan Binder The Moon’s surface is not affected by atmosphere, encounters with each other and with larger planets water, or life, the three major agents for altering throughout the lifetime of the solar system. These terrestrial surfaces. In addition, the lunar surface has orbital alterations are generally minor, but they not been shaped by recent geological activity, because ensure that, over geological periods, collisions with the lunar crust and mantle have been relatively cold other bodies will occur. and rigid throughout most of geological time. When such a collision happens, two outcomes are Convective internal mass transport, which dominates possible. If “target” and “projectile” are of comparable the dynamic Earth, is therefore largely absent on the size, collisional fragmentation and annihilation Moon, and so are the geological effects of such occurs, producing a large number of much smaller internal motions—volcanism, uplift, faulting, and fragments. If the target object is very large compared subduction—that both create and destroy surfaces on to the projectile, it behaves as an “infinite halfspace,” Earth. The great contrast between the ancient, stable and the result is an impact crater in the target body. Moon and the active, dynamic Earth is most clearly For collisions in the asteroid belt, many of the shown by the ages of their surfaces. Nearly 80% of the resulting collisional fragments or crater ejecta escape entire solid surface of Earth is <200 m.y. old. In the gravitational field of the impacted object; many of contrast, >99% of the lunar surface formed more than these fragments are then further perturbed into 3 b.y. -
Surveyor 1 Space- Craft on June 2, 1966 As Seen by the Narrow Angle Camera of the Lunar Re- Connaissance Orbiter Taken on July 17, 2009 (Also See Fig
i “Project Surveyor, in particular, removed any doubt that it was possible for Americans to land on the Moon and explore its surface.” — Harrison H. Schmitt, Apollo 17 Scientist-Astronaut ii Frontispiece: Landing site of the Surveyor 1 space- craft on June 2, 1966 as seen by the narrow angle camera of the Lunar Re- connaissance Orbiter taken on July 17, 2009 (also see Fig. 13). The white square in the upper photo outlines the area of the enlarged view below. The spacecraft is ca. 3.3 m tall and is casting a 15 m shadow to the East. (NASA/LROC/ ASU/GSFC photos) iii iv Surveyor I: America’s First Moon Landing by William F. Mellberg v © 2014, 2015 William F. Mellberg vi About the author: William Mellberg was a marketing and public relations representative with Fokker Aircraft. He is also an aerospace historian, having published many articles on both the development of airplanes and space vehicles in various magazines. He is the author of Famous Airliners and Moon Missions. He also serves as co-Editor of Harrison H. Schmitt’s website: http://americasuncommonsense.com Acknowledgments: The support and recollections of Frank Mellberg, Harrison Schmitt, Justin Rennilson, Alexander Gurshstein, Paul Spudis, Ronald Wells, Colin Mackellar and Dwight Steven- Boniecki is gratefully acknowledged. vii Surveyor I: America’s First Moon Landing by William F. Mellberg A Journey of 250,000 Miles . December 14, 2013. China’s Chang’e 3 spacecraft successfully touched down on the Moon at 1311 GMT (2111 Beijing Time). The landing site was in Mare Imbrium, the Sea of Rains, about 25 miles (40 km) south of the small crater, Laplace F, and roughly 100 miles (160 km) east of its original target in Sinus Iridum, the Bay of Rainbows. -
Expert Perspectives on Nasa's Human Exploration
CHARTING A COURSE: EXPERT PERSPECTIVES ON NASA’S HUMAN EXPLORATION PROPOSALS HEARING BEFORE THE SUBCOMMITTEE ON SPACE COMMITTEE ON SCIENCE, SPACE, AND TECHNOLOGY HOUSE OF REPRESENTATIVES ONE HUNDRED FOURTEENTH CONGRESS FIRST SESSION February 3, 2016 Serial No. 114–58 Printed for the use of the Committee on Science, Space, and Technology ( Available via the World Wide Web: http://science.house.gov U.S. GOVERNMENT PUBLISHING OFFICE 20–828PDF WASHINGTON : 2017 For sale by the Superintendent of Documents, U.S. Government Publishing Office Internet: bookstore.gpo.gov Phone: toll free (866) 512–1800; DC area (202) 512–1800 Fax: (202) 512–2104 Mail: Stop IDCC, Washington, DC 20402–0001 COMMITTEE ON SCIENCE, SPACE, AND TECHNOLOGY HON. LAMAR S. SMITH, Texas, Chair FRANK D. LUCAS, Oklahoma EDDIE BERNICE JOHNSON, Texas F. JAMES SENSENBRENNER, JR., ZOE LOFGREN, California Wisconsin DANIEL LIPINSKI, Illinois DANA ROHRABACHER, California DONNA F. EDWARDS, Maryland RANDY NEUGEBAUER, Texas SUZANNE BONAMICI, Oregon MICHAEL T. MCCAUL, Texas ERIC SWALWELL, California MO BROOKS, Alabama ALAN GRAYSON, Florida RANDY HULTGREN, Illinois AMI BERA, California BILL POSEY, Florida ELIZABETH H. ESTY, Connecticut THOMAS MASSIE, Kentucky MARC A. VEASEY, Texas JIM BRIDENSTINE, Oklahoma KATHERINE M. CLARK, Massachusetts RANDY K. WEBER, Texas DONALD S. BEYER, JR., Virginia BILL JOHNSON, Ohio ED PERLMUTTER, Colorado JOHN R. MOOLENAAR, Michigan PAUL TONKO, New York STEPHEN KNIGHT, California MARK TAKANO, California BRIAN BABIN, Texas BILL FOSTER, Illinois BRUCE WESTERMAN, Arkansas BARBARA COMSTOCK, Virginia GARY PALMER, Alabama BARRY LOUDERMILK, Georgia RALPH LEE ABRAHAM, Louisiana DRAIN LAHOOD, Illinois SUBCOMMITTEE ON SPACE HON. BRIAN BABIN, Texas, Chair DANA ROHRABACHER, California DONNA F. EDWARDS, Maryland FRANK D. -
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. -
LRO Instrument Suite and Measurements
The Lunar Reconnaissance Orbiter – Instrument Suite and Measurements Presented for the LRO team by Stephanie Stockman, LRO EPO lead Vision For Space Exploration Jan. 14 2004 – The President announced a new vision for space exploration that included among its goals “… to return to the moon by 2020, as the launching point for missions beyond. Beginning no later than 2008, we will send a series of robotic missions to the lunar surface to research and prepare for future human exploration.” Vision implies extended periods in space Unknown terrain, poor maps Radiation Environment Long Cold Nights and Warm Days Daytime 400 K (266 F) Nighttime 100 K (-280 F) Long Way From Home Exploitable Resources? - Water - Shelter - Energy LRO Objectives • Safe Landing Sites • Locate potential • Space – High resolution resources Environment imagery – Water at the lunar – Energetic – Global geodetic poles? particles grid – Continuous source – Neutrons • Topography of solar energy • Rock – abundances Mineralogy • New Technology – Advanced Radar LRO Follows in the Footsteps of the Apollo Robotic Precursors • Apollo had three (Ranger, Lunar Orbiter and Surveyor) robotic exploration programs with 21 precursor missions from 1961-68 1. Lunar Orbiters provided medium & high resolution imagery (1-2m resolution) which was acquired to support selection of Apollo and Surveyor landing sites. 2. Surveyor Landers made environmental measurements including surface physical characteristics. 3. Ranger hard landers took the first close-up photos of the lunar surface • Exploration needs the above information to go to new sites and resource data to enable sustainable exploration. Lunar Orbiter ETU in Smithsonian Air & Space Museum, Washington DC NRC Decadal (2002) lists priorities for the MOON (all mission classes thru 2013) : NRC Priority Investigation NRC approach LRO measurements Geodetic Topography Altimetry from Global geodetic (crustal evolution) orbit (with topography at ~100m precision orbits) scales (< 1 m rms) Local Geologic Studies Imaging, Sub-meter scale In 3D (geol. -
Lunarprobereadytobitethedust
NATURE|Vol 442|31 August 2006 NEWS MOON SPECIAL Check the website from 1 September for slideshows, NASA features and more. www.nature.com/ specials Lunar probe ready to bite the dust After nearly three years in space, Europe’s Moon mission is out of fuel. On 3 September the spacecraft SMART-1 will smash into the lunar surface near the Lake of Excellence in ESA/SPACE-X the Moon’s mid-southern latitudes. Astrono- mers hope the dust kicked up from the rocky site will provide information about the Moon’s composition and impact history. Researchers at the European Space Agency (ESA) are very happy with what the mission has achieved. The craft was the agency’s test- bed for a new type of thruster called an ion engine. SMART-1 is the second such engine to be used in space — the first was on board NASA’s comet-chaser Deep Space 1. Ion engines work by accelerating a stream of ionized atoms through an electric field. The one on SMART-1 provides about as much force as a postcard resting in the palm of your hand. That made its journey painfully slow: it took 14 months and a roundabout trip of 84 million kilometres for it to spiral out of Earth’s orbit and reach the Moon. In contrast, Apollo 11’s conventional propellants allowed it to travel a roughly 400,000-kilometre line between Earth and the Moon in just over 3 days. The upside is that SMART-1’s journey used around 70 kilograms of fuel, about ten times less than would have been needed with regular pro- pellants.