Hearing of the House Committee on Science, Space, and Technology Subcommittee on Space
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Quantitative Planetary Image Analysis Via Machine Learning
Tina Memo No. 2013-008 External, PhD Thesis, University of Manchester Quantitative Planetary Image Analysis via Machine Learning. Paul Tar Last updated 25 / 09 / 2014 Centre for Imaging Sciences, Medical School, University of Manchester, Stopford Building, Oxford Road, Manchester, M13 9PT. Quantitative Planetary Image Analysis via Machine Learning A thesis submitted to the University of Manchester for the degree of PhD in the faculty of Engineering and Physical Sciences 2014 Paul D. Tar School of Earth, Atmospheric and Environmental Sciences 2 Contents 1 Introduction 19 1.1 Theriseofimagingfromspace. ...... 19 1.1.1 Historicalimages ............................... 20 1.1.2 Contemporaryimages . 20 1.1.3 Futureimages.................................. 21 1.2 Sciencecase ..................................... .. 22 1.2.1 Lunarscience .................................. 22 1.2.2 Martianscience ................................ 22 1.3 Imageinterpretation ............................. ..... 23 1.3.1 Manualanalysis................................ 24 1.3.2 Automatedanalysis.............................. 24 1.4 Measurements.................................... .. 25 1.4.1 Quantitative measurements and The Scientific Method . .......... 26 1.4.2 Theroleofstatistics . ... 27 1.4.3 Assumptionsandapproximations . .... 29 1.5 Argumentforquantitativeautomation . ........ 30 1.6 Criteriaforaquantitativesystem . ......... 31 1.7 Thesisoutline ................................... ... 32 2 Literature Review 35 2.1 Representations ................................ -
Lunar Orbiter Photographic Atlas of the Near Side of the Moon Charles J
Lunar Orbiter Photographic Atlas of the Near Side of the Moon Charles J. Byrne Lunar Orbiter Photographic Atlas of the Near Side of the Moon Charles J. Byrne Image Again Middletown, NJ USA Cover illustration: Earth-based photograph of the full Moon from the “Consolidated Lunar Atlas” on the Website of the Lunar and Planetary Institute. British Library Cataloging-in-Publication Data Byrne, Charles J., 1935– Lunar Orbiter photographic atlas of the near side of the Moon 1. Lunar Orbiter (Artificial satellite) 2. Moon–Maps 3. Moon–Photographs from space I. Title 523.3 0223 ISBN 1852338865 Library of Congress Cataloging-in-Publication Data Byrne, Charles J., 1935– Lunar Orbiter photographic atlas of the near side of the Moon : with 619 figures / Charles J. Byrne. p. cm. Includes bibliographical references and index. ISBN 1-85233-886-5 (acid-free paper) 1. Moon–Maps. 2. Moon–Photographs from space. 3. Moon–Remote-sensing images. 4. Lunar Orbiter (Artificial satellite) I. Title. G1000.3.B9 2005 523.3 022 3–dc22 2004045006 Additional material to this book can be downloaded from http://extras.springer.com. ISBN 1-85233-886-5 Printed on acid-free paper. © 2005 Springer-Verlag London Limited Apart from any fair dealing for the purposes of research or private study, or criticism, or review, as permitted under the Copyright, Designs and Patents Act 1988, this publication may only be repro- duced, stored or transmitted, in any form or by any means, with the prior permission in writing of the publishers, or in the case of reprographic reproduction in accordance with the terms of licenses issued by the Copyright Licensing Agency. -
Conceptual Human-System Interface Design for a Lunar Access Vehicle
Conceptual Human-System Interface Design for a Lunar Access Vehicle Mary Cummings Enlie Wang Cristin Smith Jessica Marquez Mark Duppen Stephane Essama Massachusetts Institute of Technology* Prepared For Draper Labs Award #: SC001-018 PI: Dava Newman HAL2005-04 September, 2005 http://halab.mit.edu e-mail: [email protected] *MIT Department of Aeronautics and Astronautics, Cambridge, MA 02139 TABLE OF CONTENTS 1 INTRODUCTION..................................................................................................... 1 1.1 THE GENERAL FRAMEWORK................................................................................ 1 1.2 ORGANIZATION.................................................................................................... 2 2 H-SI BACKGROUND AND MOTIVATION ........................................................ 3 2.1 APOLLO VS. LAV H-SI........................................................................................ 3 2.2 APOLLO VS. LUNAR ACCESS REQUIREMENTS ...................................................... 4 3 THE LAV CONCEPTUAL PROTOTYPE............................................................ 5 3.1 HS-I DESIGN ASSUMPTIONS ................................................................................ 5 3.2 THE CONCEPTUAL PROTOTYPE ............................................................................ 6 3.3 LANDING ZONE (LZ) DISPLAY............................................................................. 8 3.3.1 LZ Display Introduction................................................................................. -
Apollo 11 Lunar Landing Mission Press Kit, Part 2
-lOl- The ascent stage engine compartment is formed by two beams running across the lower midsection deck and mated to the fore and aft bulkheads. Systems located in the midsection include the LM guidance computer, the power and servo assembly, ascent engine propellant tanks, RCS pro- pellant tanks, the environmental control system, and the waste management section. A tunnel ring atop the ascent stage meshes with the command module docking latch assemblies. During docking, the CM docking ring and latches are aligned by the LM drogue and the CSM probe. The dockingtunnel extends downward into the midsection 16 inches (40 cm). The tunnel is B2 inches (0.81 cm) in dia- meter and Is used for crew transfer between the CSM and LM. The upper hatch on the inboard end of the docking tunnel hinges downward and cannot be opened with the LM pressurized and u_docked. A thermal and mlcrometeoroid shield of multiple layers of mylar and a single thickness of thin aluminum skin encases the entire ascent stage structure. Descent Stase The descent stage consists of a cruciform load-carrylng structure of two pairs of parallel beams, upper and lower decks, and enclosure bulkheads -- all of conventional skln-and-strlnger aluminum alloy construction. The center compartment houses the descent engine, and descent propellant tanks are housed in the four square bays around the engine. The descent stage measures i0 feet 7 inches high by 14 feet 1 inch in diameter. Four-legged truss outriggers mounted on the ends of each pair of beams serve as SLA attach points and as "knees" for the landing gear main struts. -
Lunar Orbiter Ii
NASA CONTRACTOR NASA CR-883 REPORT LUNAR ORBITER II Photographic Mission Summary Prepared by THE BOEING COMPANY Seattle, Wash. for Langley Research Center NATIONAl AERONAUTICS AND SPACE ADMINISTRATION • WASHINGTON, D. C. • OCTOBER 1967 THE CRATER COPERNICUS - Photo taken by NASA-Boeing Lunar Orbiter II, November 23, 1966,00:05:42 GMT, from a distance of 150 miles. NASA CR-883 LUNAR ORBITER II Photographic Mission Summary Distribution of this report is provided in the interest of information exchange. Responsibility for the contents resides in the author or organization that prepared it. Issued by Originator as Document No. D2-100752-1 Prepared under Contract No. NAS 1-3800 by THE BOEING COMPANY Seattle, Wash. for Langley Research Center NATIONAL AERONAUTICS AND SPACE ADMINISTRATION For sole by the Clearinghouse for Federal Scientific and Technical Information Springfield, Virginia 22151 - CFSTI price $3.00 CONTENTS Page No. 1.0 LUNAR ORBITER II MISSION SUMMARY 1 1.1 INTRODUCTION 4 1.1.1 Program Description 4 1.1.2 Program Management 5 1.1.3 Program Objectives 6 1.1.3.1 Mission II Objectives 6 1.1.4 Mission Design 8 1.1.5 Flight Vehicle Description 12 1.2 LAUNCH PREPARATION AND OPERATIONS 19 1.2.1 Launch Vehicle Preparation 19 1.2.2 Spacecraft Preparation 21 1.2.3 Launch Countdown 21 1.2.4 Launch Phase 22 1.2.4.1 Flight Vehicle Performance 22 1.2.5 Data Acquisition 24 1.3 MISSION OPERATIONS 29 1.3.1 Mission Profile 29 1.3.2 Spacecraft Performance 31 1.3.2.1 Photo Subsystem Performance 32 1.3.2.2 Power Subsystem Performance 34 1.3.2.3 Communications -
Martian Ice How One Neutrino Changed Astrophysics Remembering Two Former League Presidents
Published by the Astronomical League Vol. 71, No. 3 June 2019 MARTIAN ICE HOW ONE NEUTRINO 7.20.69 CHANGED ASTROPHYSICS 5YEARS REMEMBERING TWO APOLLO 11 FORMER LEAGUE PRESIDENTS ONOMY T STR O T A H G E N P I E G O Contents N P I L R E B 4 . President’s Corner ASTRONOMY DAY Join a Tour This Year! 4 . All Things Astronomical 6 . Full Steam Ahead OCTOBER 5, From 37,000 feet above the Pacific Total Eclipse Flight: Chile 7 . Night Sky Network 2019 Ocean, you’ll be high above any clouds, July 2, 2019 For a FREE 76-page Astronomy seeing up to 3¼ minutes of totality in a PAGE 4 9 . Wanderers in the Neighborhood dark sky that makes the Sun’s corona look Day Handbook full of ideas and incredibly dramatic. Our flight will de- 10 . Deep Sky Objects suggestions, go to: part from and return to Santiago, Chile. skyandtelescope.com/2019eclipseflight www.astroleague.org Click 12 . International Dark-Sky Association on "Astronomy Day” Scroll 14 . Fire & Ice: How One Neutrino down to "Free Astronomy Day African Stargazing Safari Join astronomer Stephen James ̃̃̃Changed a Field Handbook" O’Meara in wildlife-rich Botswana July 29–August 4, 2019 for evening stargazing and daytime PAGE 14 18 . Remembering Two Former For more information, contact: safari drives at three luxury field ̃̃̃Astronomical League Presidents Gary Tomlinson camps. Only 16 spaces available! Astronomy Day Coordinator Optional extension to Victoria Falls. 21 . Coming Events [email protected] skyandtelescope.com/botswana2019 22 . Gallery—Moon Shots 25 . Observing Awards Iceland Aurorae September 26–October 2, 2019 26 . -
Project Apollo: Americans to the Moon 440 Document II-1 Document Title
440 Project Apollo: Americans to the Moon Document II-1 Document Title: NASA, “ Minutes of Meeting of Research Steering Committee on Manned Space Flight,” 25–26 May 1959. Source: Folder 18675, NASA Historical Reference Collection, History Division, NASA Headquarters, Washington, DC. Within less than a year after its creation, NASA began looking at follow-on programs to Project Mercury, the initial human spacefl ight effort. A Research Steering Committee on Manned Space Flight was created in spring 1959; it consisted of top-level representatives of all of the NASA fi eld centers and NASA Headquarters. Harry J. Goett from Ames, but soon to be head of the newly created Goddard Space Flight Center, was named chair of the committee. The fi rst meeting of the committee took place on 25 and 26 May 1959, in Washington. Those in attendance provided an overview of research and thinking related to human spacefl ight at various NASA centers, the Jet Propulsion Laboratory (JPL), and the High Speed Flight Station (HSFS) at Edwards Air Force Base. George Low, then in charge of human spacefl ight at NASA Headquarters, argued for making a lunar landing NASA’s long-term goal. He was backed up by engineer and designer Maxime Faget of the Space Task Group of the Langley Research Center and Bruce Lundin of the Lewis Research Center. After further discussion at its June meeting, the Committee agreed on the lunar landing objective, and by the end of the year a lunar landing was incorporated into NASA’s 10-year plan as the long-range objective of the agency’s human spacefl ight program. -
NASA and Planetary Exploration
**EU5 Chap 2(263-300) 2/20/03 1:16 PM Page 263 Chapter Two NASA and Planetary Exploration by Amy Paige Snyder Prelude to NASA’s Planetary Exploration Program Four and a half billion years ago, a rotating cloud of gaseous and dusty material on the fringes of the Milky Way galaxy flattened into a disk, forming a star from the inner- most matter. Collisions among dust particles orbiting the newly-formed star, which humans call the Sun, formed kilometer-sized bodies called planetesimals which in turn aggregated to form the present-day planets.1 On the third planet from the Sun, several billions of years of evolution gave rise to a species of living beings equipped with the intel- lectual capacity to speculate about the nature of the heavens above them. Long before the era of interplanetary travel using robotic spacecraft, Greeks observing the night skies with their eyes alone noticed that five objects above failed to move with the other pinpoints of light, and thus named them planets, for “wan- derers.”2 For the next six thousand years, humans living in regions of the Mediterranean and Europe strove to make sense of the physical characteristics of the enigmatic planets.3 Building on the work of the Babylonians, Chaldeans, and Hellenistic Greeks who had developed mathematical methods to predict planetary motion, Claudius Ptolemy of Alexandria put forth a theory in the second century A.D. that the planets moved in small circles, or epicycles, around a larger circle centered on Earth.4 Only partially explaining the planets’ motions, this theory dominated until Nicolaus Copernicus of present-day Poland became dissatisfied with the inadequacies of epicycle theory in the mid-sixteenth century; a more logical explanation of the observed motions, he found, was to consider the Sun the pivot of planetary orbits.5 1. -
Lunar Orbiter Iv
NASA CONTRACTOR NASA CR-1054 REPORT LUNAR ORBITER IV Photographic Mission Summary Prepared by THE BOEING COMPANY Seattle, Wash. for Langley Research Center NATIONAL AERONAUTICS AND SPACE ADMINISTRATION • WASHINGTON, D. C. • JUNE 1968 First Detailed View of Orientale Basin Photo taken by NASA-Boeing Lunar Orbiter IV, May 25, 1967, 05:33:34 GMT, from an altitude o£2,721 kilometers. NASA CR-1054 LUNAR ORBITER IV Photographic Mission Summary Distribution of this report is provided in the interest of information exchange. Responsibility for the contents resides in the author or organization that prepared it. Issued by Originator as Boeing Document No. 02-100754-1 (Vol. 1) Prepared under Contract No. NAS 1-3800 by THE BOEING COMPANY Seattle, Wash. for Langley Research Center NATIONAL AERONAUTICS AND SPACE ADMINISTRATION For sale by the Clearinghouse for Federal Scientific and Technical Information Springfield, Virginia 22151 - CFSTI price $3.00 Contents Page 1.0 INTRODUCTION . ........ ............ ............... ....... ............... 5 1.1 Program Description ....................................................... 5 1.2 Program Management ...................................................... 5 1.3 Program Objectives ........................................................ 6 1.3.1 Mission IV Objectives ................................................. 7 1.4 Mission Design ............................... ..... ....... .... ............ 8 1.5 Flight Vehicle Description ... ......... ............................. .... .. .. 11 2.0 LAUNCH PREPARATION -
The Ranger Telerobotic Shuttle Experiment: an On-Orbit Satellite Servicer
THE RANGER TELEROBOTIC SHUTTLE EXPERIMENT: AN ON-ORBIT SATELLITE SERVICER Joseph C. Parrish NASA Headquarters Office of Space Science, Advanced Technologies & Mission Studies Division Mail Code SM, Washington, DC, 20546-0001, U.S.A. phone: +1 301 405 0291, fax: +1 209 391 9785, e-mail: [email protected] Abstract 1 Introduction As space operations enter the 21st century, the role The Ranger Telerobotic Shuttle Experiment (RTSX) of robotic satellite servicing systems will increase dra- is a Space Shuttle-based flight experiment to demon- matically. Several such systems are currently in de- strate key telerobotic technologies for servicing as- velopment for use on the International Space Sta- sets in Earth orbit. The flight system will be tele- tion, including the Canadian Mobile Servicing Sys- operated from onboard the Space Shuttle and from a tem (MSS)[2] and the Japanese Experiment Module ground control station at the NASA Johnson Space Remote Manipulator System (JEM-RMS). Another Center. The robot, along with supporting equipment Japanese system, the Experimental Test System VII and task elements, will be located in the Shuttle pay- (ETS-VII) [I],has already demonstrated the ability for load bay. A number of relevant servicing operations rendezvous and docking, followed by ORU manipula- will be performed-including extravehicular activity tion under supervisory control. Under development by (EVA) worksite setup, orbit replaceable unit (ORU) the United States, the Ranger Telerobotic Shuttle Ex- exchange, and other dexterous tasks. The program periment (RTSX)[3] is progressing toward its mission is underway toward an anticipated launch date in on the NASA Space Shuttle to demonstrate telerobotic CY2001, and the hardware and software for the flight servicing of orbital assets. -
Assessing & Protecting Dark Night Skies in El Morro National Monument
ASSESSING & PROTECTING DARK NIGHT SKIES IN EL MORRO NATIONAL MONUMENT by Leslie Kobinsky October 1st, 2019 A capstone report submitted in partial fulfillment of the requirements for the degree of MASTER OF NATURAL RESOURCES and NREE Certificate Program Committee Members: Mark Brunson, Chair Mark Larese-Casanova Melanie Conrad UTAH STATE UNIVERSITY Logan, UT 2019 1 TABLE OF CONTENTS ABSTRACT.................................................................................................................................................. 3 LIST OF FIGURES ...................................................................................................................................... 3 INTRODUCTION ........................................................................................................................................ 4 Problem Statement.................................................................................................................................... 4 Audience ................................................................................................................................................... 5 Background Information........................................................................................................................... 5 Project Goals and Objectives.................................................................................................................... 5 METHOD OF ANALYSIS AND DESCRIPTION OF STUDY SITE........................................................ 6 -
Locations of Anthropogenic Sites on the Moon R
Locations of Anthropogenic Sites on the Moon R. V. Wagner1, M. S. Robinson1, E. J. Speyerer1, and J. B. Plescia2 1Lunar Reconnaissance Orbiter Camera, School of Earth and Space Exploration, Arizona State University, Tempe, AZ 85287-3603; [email protected] 2The Johns Hopkins University, Applied Physics Laboratory, Laurel, MD 20723 Abstract #2259 Introduction Methods and Accuracy Lunar Reconnaissance Orbiter Camera (LROC) Narrow Angle Camera To get the location of each object, we recorded its line and sample in (NAC) images, with resolutions from 0.25-1.5 m/pixel, allow the each image it appears in, and then used USGS ISIS routines to extract identifcation of historical and present-day landers and spacecraft impact latitude and longitude for each point. The true position is calculated to be sites. Repeat observations, along with recent improvements to the the average of the positions from individual images, excluding any extreme spacecraft position model [1] and the camera pointing model [2], allow the outliers. This process used Spacecraft Position Kernels improved by LOLA precise determination of coordinates for those sites. Accurate knowledge of cross-over analysis and the GRAIL gravity model, with an uncertainty of the coordinates of spacecraft and spacecraft impact craters is critical for ±10 meters [1], and a temperature-corrected camera pointing model [2]. placing scientifc and engineering observations into their proper geologic At sites with a retrorefector in the same image as other objects (Apollo and geophysical context as well as completing the historic record of past 11, 14, and 15; Luna 17), we can improve the accuracy signifcantly. Since trips to the Moon.