Astronautics and Aeronautics, 1968
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
WARP Ten, 1992 Columbia College Chicago
Columbia College Chicago Digital Commons @ Columbia College Chicago WARP ten Publications 2-1-1992 WARP ten, 1992 Columbia College Chicago Follow this and additional works at: https://digitalcommons.colum.edu/warpten Part of the Journalism Studies Commons This work is licensed under a Creative Commons Attribution-Noncommercial-No Derivative Works 4.0 License. Recommended Citation Columbia College Chicago, "WARP ten, 1992" (1992). WARP ten. 1. https://digitalcommons.colum.edu/warpten/1 This Book is brought to you for free and open access by the Publications at Digital Commons @ Columbia College Chicago. It has been accepted for inclusion in WARP ten by an authorized administrator of Digital Commons @ Columbia College Chicago. For more information, please contact [email protected]. A Science Newsletter of Columbia College Journalism Department Vol.I , No.I -~ Of Mars and Men By Robbie Robb the moon, a distance of 384,000km (239,000 miles) is but a three day voyage. A one-way trip to Mars, a distance of 56.4 million km. (35 million miles) rcquimi 280 days. The sheec The lure of the red planet has tantalized hlJIJUlllity for cen scope of the project thus demands a more expensive turies. Authors from H. G. Wells to Ray Bradbury havewriucn spacecraft. But traveling to Mars would also require more about life on Mars and coloni2ation of the planet. The Arnold resources at additional cosl Vast arnounlS of supplies, food. Schwanznegger movie, "Total Recall," portrayed a Martilln equipment, and fuel would be needed for a trip of this m11& world inhabited by tran.splanted earthlings. Now the idea of nitude. -
Potential of Polarization/Raman Lidar to Separate Fine Dust, Coarse Dust
Atmos. Meas. Tech., 10, 3403–3427, 2017 https://doi.org/10.5194/amt-10-3403-2017 © Author(s) 2017. This work is distributed under the Creative Commons Attribution 3.0 License. Potential of polarization/Raman lidar to separate fine dust, coarse dust, maritime, and anthropogenic aerosol profiles Rodanthi-Elisavet Mamouri1,2 and Albert Ansmann3 1Cyprus University of Technology, Dep. of Civil Engineering and Geomatics, Limassol, Cyprus 2The Cyprus Institute, Energy, Environment, and Water Research Center, Nicosia, Cyprus 3Leibniz Institute for Tropospheric Research, Leipzig, Germany Correspondence to: Rodanthi-Elisavet Mamouri ([email protected]) Received: 26 April 2017 – Discussion started: 4 May 2017 Revised: 28 July 2017 – Accepted: 2 August 2017 – Published: 19 September 2017 Abstract. We applied the recently introduced polarization advantages in comparison to 355 and 1064 nm polarization lidar–photometer networking (POLIPHON) technique for lidar approaches and leads to the most robust and accurate the first time to triple-wavelength polarization lidar measure- POLIPHON products. ments at 355, 532, and 1064 nm. The lidar observations were performed at Barbados during the Saharan Aerosol Long- Range Transport and Aerosol-Cloud-Interaction Experiment (SALTRACE) in the summer of 2014. The POLIPHON 1 Introduction method comprises the traditional lidar technique to separate mineral dust and non-dust backscatter contributions and the Polarization lidar is a very powerful remote sensing tool for new, extended approach to separate even the fine and coarse aerosol and cloud research. The technique has been used for dust backscatter fractions. We show that the traditional and a long time to monitor and investigate cirrus cloud systems the advanced method are compatible and lead to a consis- (e.g., Sassen, 1991, 2005; Reichardt et al., 2002, 2008) and tent set of dust and non-dust profiles at simplified, less com- polar stratospheric cloud evolution (see, e.g., Browell et al., plex aerosol layering and mixing conditions as is the case 1990; Achtert and Tesche, 2014). -
General Vertical Files Anderson Reading Room Center for Southwest Research Zimmerman Library
“A” – biographical Abiquiu, NM GUIDE TO THE GENERAL VERTICAL FILES ANDERSON READING ROOM CENTER FOR SOUTHWEST RESEARCH ZIMMERMAN LIBRARY (See UNM Archives Vertical Files http://rmoa.unm.edu/docviewer.php?docId=nmuunmverticalfiles.xml) FOLDER HEADINGS “A” – biographical Alpha folders contain clippings about various misc. individuals, artists, writers, etc, whose names begin with “A.” Alpha folders exist for most letters of the alphabet. Abbey, Edward – author Abeita, Jim – artist – Navajo Abell, Bertha M. – first Anglo born near Albuquerque Abeyta / Abeita – biographical information of people with this surname Abeyta, Tony – painter - Navajo Abiquiu, NM – General – Catholic – Christ in the Desert Monastery – Dam and Reservoir Abo Pass - history. See also Salinas National Monument Abousleman – biographical information of people with this surname Afghanistan War – NM – See also Iraq War Abousleman – biographical information of people with this surname Abrams, Jonathan – art collector Abreu, Margaret Silva – author: Hispanic, folklore, foods Abruzzo, Ben – balloonist. See also Ballooning, Albuquerque Balloon Fiesta Acequias – ditches (canoas, ground wáter, surface wáter, puming, water rights (See also Land Grants; Rio Grande Valley; Water; and Santa Fe - Acequia Madre) Acequias – Albuquerque, map 2005-2006 – ditch system in city Acequias – Colorado (San Luis) Ackerman, Mae N. – Masonic leader Acoma Pueblo - Sky City. See also Indian gaming. See also Pueblos – General; and Onate, Juan de Acuff, Mark – newspaper editor – NM Independent and -
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. -
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. -
COURT of CLAIMS of THE
REPORTS OF Cases Argued and Determined IN THE COURT of CLAIMS OF THE STATE OF ILLINOIS VOLUME 39 Containing cases in which opinions were filed and orders of dismissal entered, without opinion for: Fiscal Year 1987 - July 1, 1986-June 30, 1987 SPRINGFIELD, ILLINOIS 1988 (Printed by authority of the State of Illinois) (65655--300-7/88) PREFACE The opinions of the Court of Claims reported herein are published by authority of the provisions of Section 18 of the Court of Claims Act, Ill. Rev. Stat. 1987, ch. 37, par. 439.1 et seq. The Court of Claims has exclusive jurisdiction to hear and determine the following matters: (a) all claims against the State of Illinois founded upon any law of the State, or upon an regulation thereunder by an executive or administrative ofgcer or agency, other than claims arising under the Workers’ Compensation Act or the Workers’ Occupational Diseases Act, or claims for certain expenses in civil litigation, (b) all claims against the State founded upon any contract entered into with the State, (c) all claims against the State for time unjustly served in prisons of this State where the persons imprisoned shall receive a pardon from the Governor stating that such pardon is issued on the grounds of innocence of the crime for which they were imprisoned, (d) all claims against the State in cases sounding in tort, (e) all claims for recoupment made by the State against any Claimant, (f) certain claims to compel replacement of a lost or destroyed State warrant, (g) certain claims based on torts by escaped inmates of State institutions, (h) certain representation and indemnification cases, (i) all claims pursuant to the Law Enforcement Officers, Civil Defense Workers, Civil Air Patrol Members, Paramedics and Firemen Compensation Act, (j) all claims pursuant to the Illinois National Guardsman’s and Naval Militiaman’s Compensation Act, and (k) all claims pursuant to the Crime Victims Compensation Act. -
We Help Earth Benefit from Space in Summary 2019 Contents
WE HELP EARTH BENEFIT FROM SPACE IN SUMMARY 2019 CONTENTS About this report 2019 HIGHLIGHTS This is an English summary of Swedish 3 Space Corporation’s (SSC) 2019 Annual and Sustainability Report. CEO STATEMENT The Swedish report, available at our web- 4 site, is the legally binding annual report. THIS IS SSC The report summarizes the 2019 fiscal 6 year and covers performance on issues most important to SSC's ability to deliver SSC GLOBAL PRESENCE value to stakeholders in a changing and complex business environment. This 8 summary serves as our United Nations Global Compact (UNGC) Communi- EVOLVING SPACE LANDSCAPE 9 cations on Progress. Visit: STRATEGIC APPROACH https://www.sscspace.com/about-ssc/finances/reports-archive/ 10 Copyright: Unless otherwise indicated, SSC has the copyright to images in this publication. FOCUS AREAS FOR PROFITABLE SUSTAINABLE GROWTH 12 EMPLOYEES - OUR GREATEST ASSET 14 MEET OUR PEOPLE 15 2019 HIGHLIGHTS 2019 HIGHLIGHTS 2019 was another year of exciting space missions and projects for the space sector as a whole, but also for SSC. The rapid development has allowed us to grow and take new steps to prepare for the future. MASER 14 and inauguration of SubOrbital Express as a service Our MASER 14 sounding rocket reached an altitude of approximately 250 kilometers and spent over six minutes in microgravity. The mission inaugurated SubOrbital Express, a service to enable research into microgravity applications, atmospheric physics or other scientific disciplines. In this microgravity environment, we conducted experiments on fluid drainage, X-ray radio graphy and dust formation. Read more: https://www.suborbitalexpress.com Inauguration of exciting antenna art in Inuvik The two SSC antennas at the Inuvik site are painted by the local artists Anick Jenks and Ron English. -
Impact Cratering
6 Impact cratering The dominant surface features of the Moon are approximately circular depressions, which may be designated by the general term craters … Solution of the origin of the lunar craters is fundamental to the unravel- ing of the history of the Moon and may shed much light on the history of the terrestrial planets as well. E. M. Shoemaker (1962) Impact craters are the dominant landform on the surface of the Moon, Mercury, and many satellites of the giant planets in the outer Solar System. The southern hemisphere of Mars is heavily affected by impact cratering. From a planetary perspective, the rarity or absence of impact craters on a planet’s surface is the exceptional state, one that needs further explanation, such as on the Earth, Io, or Europa. The process of impact cratering has touched every aspect of planetary evolution, from planetary accretion out of dust or planetesimals, to the course of biological evolution. The importance of impact cratering has been recognized only recently. E. M. Shoemaker (1928–1997), a geologist, was one of the irst to recognize the importance of this process and a major contributor to its elucidation. A few older geologists still resist the notion that important changes in the Earth’s structure and history are the consequences of extraterres- trial impact events. The decades of lunar and planetary exploration since 1970 have, how- ever, brought a new perspective into view, one in which it is clear that high-velocity impacts have, at one time or another, affected nearly every atom that is part of our planetary system. -
Highlights in Space 2010
International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no. -
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. -
Space Astronomy in India: 43 Years and Counting
Interstellar Matter and Star Formation: A Multi-wavelength Perspective ASI Conference Series, 2010, Vol. 1, pp 177{191 Edited by D. K. Ojha Space astronomy in India: 43 years and counting R. K. Manchanda¤ Tata Institute of Fundamental Research, Colaba, Mumbai 400 005, India Abstract. The beginning of Space astronomy in India took place at TIFR in 1966, with the development of a small balloon borne X- ray astronomy payload. During the 1966-1976 period, studies in the X-ray and Gamma ray energy bands were pursued both at TIFR and PRL, Ahmedabad. Infrared astronomy made its beginning in 1975. The rapid progress of Space astronomy in the early years was mainly due to the availability of large plastic balloons and detector tools de- veloped by the High altitude studies group of TIFR, which I joined in 1966 and initiated the fabrication of the X-ray payload. Balloon borne astronomy has thrived during the past 43 years while satellite opportunities during this period were few and only for piggyback pay- loads. At present, a full fledged multi-wavelength astronomy satellite mission named ASTROSAT is under fabrication and will be launched in 2011. Keywords : X-ray astronomy, Space astronomy, Balloon borne ex- periments, History of astronomy 1. Early phase Space astronomy in India was born in 1966 at TIFR as a Balloon-borne ex- ploratory programme soon after the chance discovery of the ¯rst X-ray sources in 1962 and within one year became the key project of the High Altitude Stud- ies group. Simultaneously, balloon borne X-ray and gamma ray astronomy work started at Physical Research Laboratory, Ahmedabad. -
Project: Apollo 8
v ._. I / I NATIONAL AERONAUTICS AND SPACE ADMINISTRATION TELS WO 2-4155 NEWS WASHINGTON,D.C.20546 • WO 3-6925 FOR RELEASE: SUNDAY December 15, 1968 RELEASE NO: 68.208 P PROJECT: APOLLO 8 R E contents GENERAL RELEASE----------~-------~·~-~-~--~~----~----~-~--~-l-lO MISSION OBJECTIVES------------------------------------------11 SEQUENCE OF EVENTS-------------~-------------~----~----~--~~12-14 5 Launch W1ndow~~-~----~--~-~--~-------~-----~---------w--~-14 MISSION DESCRIPTION-----------------------------------------15-19 FLIGHT PLAN--~---~-----·------------~------~----~---~----~--20-23 ALTERNATE MISSIONS---------------------------------~--------24-26 5 ABORT MODES-----~--------------~--~--~------------~---~~--~-27~29 PHOTOGRAPHIC TASKS------------------------------------------30-32 SPACECRAFT STRUCTURE SYSTEMS--------------------------------33-37 SATURN V LAUNCH VEHICLE-------------------------------------38-50 APOLLO 8 LAUNCH OPERATIONS----------------------------------51.64 MISSION CONTROL CENTER--------------------------------------65-66 MANNED SPACE FLIGHT NETWORK---------------------------------67-71 APOLLO 8 RECOVERY-------------------------------------------72-73 APOLLO 8 CREW-------------~--~--~~-~~---~---~~~-------------74-86 K LUNAR DESCRIPTION-------------------------------------------87-88 APOLLO PROGRAM MANAGEMENT/CONTRACTORS---~-------------------39-94 I APOLLO 8 GLOSSARY-------- -----------------------------------95-101 T -0- 12/6/68 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WO 2-4155 NEWS WASHINGTON, D.C. 20546 TELS.