THE PROSPECTOR's GUIDE to the GALAXY 237 on Whether Anyone Can Own Or Use Celestial Resources
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Return to the Moon Mission Overview
Return to the Moon Mission Overview The new millennium is still young, but humans using the lastest in transport technology to are preparing to Return to the Moon, reduce the travel time. In addition to verifying spurred on by the verification of ice water on the best site for the establishment of the the lunar surface by Lunar Prospector in lunar base, during the course of the mission, 1998. Composed of hydrogen and oxygen – the crew will recover a probe that is the elements that make up water – the lunar stranded in space and access the damage to ice provides a core resource for long-term the probe, and then build and launch an human presence on the lunar surface. equipment module to the lunar surface. Lunar Prospector was followed by a series of Some information has been previously successful robotic missions designed to obtained from the potential lunar base sites. probe the concept that the ice water could A detailed study has determined that the be harvested. Once collected, the ice water base site must contain solid, metals, and can be turned into drinking water, oxygen for potentially useful resources such as helium-3. life support of a lunar base, nutrients as the Rock and soil samples, soil composition, and basis for agriculture, components needed for seismic information have been gathered by rocket fuel, or when combined with lunar soil, previous missions from a portion of the the basics for construction materials. Not potential sites. Experiments on soil and rock only did those robotic missions successfully samples from other possible sites must be prove that concept, but since then, additional performed in order to determine the best robotic staging missions have landed and site for the lunar base. -
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................................................................................. -
Reviewing the Contribution of GRAIL to Lunar Science and Planetary Missions Maria T
EPSC Abstracts Vol. 12, EPSC2018-575, 2018 European Planetary Science Congress 2018 EEuropeaPn PlanetarSy Science CCongress c Author(s) 2018 Reviewing the contribution of GRAIL to lunar science and planetary missions Maria T. Zuber and David E. Smith Department of Earth, Atmospheric and Planetary Sciences, Massachusetts Institute of Technology, Cambridge, MA 02139- 4307, USA. ([email protected], [email protected]) Abstract Q of the Moon determined to be 41±4 at the monthly frequency. The GRAIL Discovery mission to the Moon in 2011 provided an unprecedentedly accurate gravity field model for the Moon. The goal of the mission was to provide insight into the structure of the Moon from its interior to the surface but it also made significant contributions to lunar spacecraft operations for all future lunar missions to the Moon. We discuss the science and the broader contributions from this mission that completed its objectives in December 2012 when the spacecraft impacted the lunar surface. 1. Introduction Figure 1: Free-air gravity of the Moon from GRAIL. GRAIL was a mission designed to measure the Full uniform resolution spherical harmonic models gravity field of the Moon with both high accuracy were obtained out to degree & order 1200 with and high resolution. The measurement goal was to special fields with higher resolutions over certain obtain the gravity at resolutions that would enable areas to degree and order 1800. interpretation of the crust at fractions of its thickness, estimated at the time of launch to be about 45 km. To 3. Mission Operations obtain a surface resolution of less than 10 km required the spacecraft to orbit the Moon at less than The significant improvement in our knowledge of the 20 km, an altitude that was considered dangerous at gravity field of the Moon by GRAIL enabled the re- that time without an accurate gravity field model. -
THE SOVIET MOON PROGRAM in the 1960S, the United States Was Not the Only Country That Was Trying to Land Someone on the Moon and Bring Him Back to Earth Safely
AIAA AEROSPACE M ICRO-LESSON Easily digestible Aerospace Principles revealed for K-12 Students and Educators. These lessons will be sent on a bi-weekly basis and allow grade-level focused learning. - AIAA STEM K-12 Committee. THE SOVIET MOON PROGRAM In the 1960s, the United States was not the only country that was trying to land someone on the Moon and bring him back to Earth safely. The Union of Soviet Socialist Republics, also called the Soviet Union, also had a manned lunar program. This lesson describes some of it. Next Generation Science Standards (NGSS): ● Discipline: Engineering Design ● Crosscutting Concept: Systems and System Models ● Science & Engineering Practice: Constructing Explanations and Designing Solutions GRADES K-2 K-2-ETS1-1. Ask questions, make observations, and gather information about a situation people want to change to define a simple problem that can be solved through the development of a new or improved object or tool. Have you ever been busy doing something when somebody challenges you to a race? If you decide to join the race—and it is usually up to you whether you join or not—you have to stop what you’re doing, get up, and start racing. By the time you’ve gotten started, the other person is often halfway to the goal. This is the sort of situation the Soviet Union found itself in when President Kennedy in 1961 announced that the United States would set a goal of landing a man on the Moon and returning him safely to the Earth before the end of the decade. -
The Soviet Space Program
C05500088 TOP eEGRET iuf 3EEA~ NIE 11-1-71 THE SOVIET SPACE PROGRAM Declassified Under Authority of the lnteragency Security Classification Appeals Panel, E.O. 13526, sec. 5.3(b)(3) ISCAP Appeal No. 2011 -003, document 2 Declassification date: November 23, 2020 ifOP GEEAE:r C05500088 1'9P SloGRET CONTENTS Page THE PROBLEM ... 1 SUMMARY OF KEY JUDGMENTS l DISCUSSION 5 I. SOV.IET SPACE ACTIVITY DURING TfIE PAST TWO YEARS . 5 II. POLITICAL AND ECONOMIC FACTORS AFFECTING FUTURE PROSPECTS . 6 A. General ............................................. 6 B. Organization and Management . ............... 6 C. Economics .. .. .. .. .. .. .. .. .. .. .. ...... .. 8 III. SCIENTIFIC AND TECHNICAL FACTORS ... 9 A. General .. .. .. .. .. 9 B. Launch Vehicles . 9 C. High-Energy Propellants .. .. .. .. .. .. .. .. .. 11 D. Manned Spacecraft . 12 E. Life Support Systems . .. .. .. .. .. .. .. .. 15 F. Non-Nuclear Power Sources for Spacecraft . 16 G. Nuclear Power and Propulsion ..... 16 Te>P M:EW TCS 2032-71 IOP SECl<ET" C05500088 TOP SECRGJ:. IOP SECREI Page H. Communications Systems for Space Operations . 16 I. Command and Control for Space Operations . 17 IV. FUTURE PROSPECTS ....................................... 18 A. General ............... ... ···•· ................. ····· ... 18 B. Manned Space Station . 19 C. Planetary Exploration . ........ 19 D. Unmanned Lunar Exploration ..... 21 E. Manned Lunar Landfog ... 21 F. Applied Satellites ......... 22 G. Scientific Satellites ........................................ 24 V. INTERNATIONAL SPACE COOPERATION ............. 24 A. USSR-European Nations .................................... 24 B. USSR-United States 25 ANNEX A. SOVIET SPACE ACTIVITY ANNEX B. SOVIET SPACE LAUNCH VEHICLES ANNEX C. SOVIET CHRONOLOGICAL SPACE LOG FOR THE PERIOD 24 June 1969 Through 27 June 1971 TCS 2032-71 IOP SLClt~ 70P SECRE1- C05500088 TOP SEGR:R THE SOVIET SPACE PROGRAM THE PROBLEM To estimate Soviet capabilities and probable accomplishments in space over the next 5 to 10 years.' SUMMARY OF KEY JUDGMENTS A. -
Comparative Influences of Human Factors on National Space Activities and Practices [United States, Russia, China, and Others]
Comparative Influences of Human Factors on National Space Activities and Practices [United States, Russia, China, and others] ● National Space Biomedical Research Institute [NSBRI] ● Piloting Spacecraft Guidance & Control of Human Space Vehicles ● September 21-22, 2016 ● Houston, Texas ● James Oberg [WWW.jamesoberg.com] Approach ● How do external cultural and other national factors influence a space program? ● What illuminating analogies offer insights? ● What differences can we see in national programs that can be traced back to such human [as opposed to technological] factors? ● How can lack of appreciation for these subtle influences diminish assessment accuracy? ● Why is this BAD? ● How can realistic appreciation for these subtle influences help future joint projects? Professional specialty – human spaceflight operations [1975-1997] Baykonur & Star City etc. Congressional Testimony [1997,1998] Analogy with “Terroir” – influence of environmental factors on quality of wine “Terroir” for a space program CLIMATE SOIL TRADITION TERRAIN An analogy with wine, and how its quality reflects its environment – both NATIONAL and INTERNATIONAL International Environmental Factors Space programs don’t exist in isolation Competition often spurs on each player Space programs develop special capabilities which they protect ‘Many justifications for learning from others Direct copying not always ‘best fit’ ASSUMING copying by others can be misleading CAUTIONARY COMMENT REGARDING THE CONCEPT OF “COPYING” Inspiration may be as influential as direct ‘copying’ Humanned spacecraft with aero shroud and ‘escape tower’: left, Russian Soyuz; center & right, Chinese Shenzhou. Huang Chunping on stabilization flaps: “This is the most difficult part of the escape system. We once wanted to inquire about it from Russian experts, but they set the price at $10 million. -
Robotic Asteroid Prospector
Robotic Asteroid Prospector Marc M. Cohen1 Marc M. Cohen Architect P.C. – Astrotecture™, Palo Alto, CA, USA 94306-3864 Warren W. James2 V Infinity Research LLC. – Altadena, CA, USA Kris Zacny,3 Philip Chu, Jack Craft Honeybee Robotics Spacecraft Mechanisms Corporation – Pasadena, CA, USA This paper presents the results from the nine-month, Phase 1 investigation for the Robotic Asteroid Prospector (RAP). This project investigated several aspects of developing an asteroid mining mission. It conceived a Space Infrastructure Framework that would create a demand for in space-produced resources. The resources identified as potentially feasible in the near-term were water and platinum group metals. The project’s mission design stages spacecraft from an Earth Moon Lagrange (EML) point and returns them to an EML. The spacecraft’s distinguishing design feature is its solar thermal propulsion system (STP) that provides two functions: propulsive thrust and process heat for mining and mineral processing. The preferred propellant is water since this would allow the spacecraft to refuel at an asteroid for its return voyage to Cis- Lunar space thus reducing the mass that must be launched from the EML point. The spacecraft will rendezvous with an asteroid at its pole, match rotation rate, and attach to begin mining operations. The team conducted an experiment in extracting and distilling water from frozen regolith simulant. Nomenclature C-Type = Carbonaceous Asteroid EML = Earth-Moon Lagrange Point ESL = Earth-Sun Lagrange Point IPV = Interplanetary Vehicle M-Type = Metallic Asteroid NEA = Near Earth Asteroid NEO = Near Earth Object PGM = Platinum Group Metal STP = Solar Thermal Propulsion S-Type = Stony Asteroid I. -
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Y L F M A E T Team-Fly® Streaming Media Demystified Michael Topic McGraw-Hill New York Chicago San Francisco Lisbon London Madrid Mexico City Milan New Delhi San Juan Seoul Singapore Sydney Toronto McGraw-Hill abc Copyright © 2002 by The McGraw-Hill Companies, Inc. All rights reserved. Manufactured in the United States of America. Except as permitted under the United States Copyright Act of 1976, no part of this publication may be reproduced or distrib- uted in any form or by any means, or stored in a database or retrieval system, without the prior written permission of the publisher. 0-07-140962-9 The material in this eBook also appears in the print version of this title: 0-07-138877-X. All trademarks are trademarks of their respective owners. Rather than put a trademark symbol after every occurrence of a trademarked name, we use names in an editorial fashion only, and to the benefit of the trademark owner, with no intention of infringement of the trademark. Where such designations appear in this book, they have been printed with initial caps. McGraw-Hill eBooks are available at special quantity discounts to use as premiums and sales promotions, or for use in cor- porate training programs. For more information, please contact George Hoare, Special Sales, at george_hoare@mcgraw- hill.com or (212) 904-4069. TERMS OF USE This is a copyrighted work and The McGraw-Hill Companies, Inc. (“McGraw-Hill”) and its licensors reserve all rights in and to the work. Use of this work is subject to these terms. -
The 1960 Presidential Election in Florida: Did the Space Race and the National Prestige Issue Play an Important Role?
UNF Digital Commons UNF Graduate Theses and Dissertations Student Scholarship 2000 The 1960 rP esidential Election in Florida: Did the Space Race and the National Prestige Issue Play an Important Role? Randy Wade Babish University of North Florida Suggested Citation Babish, Randy Wade, "The 1960 rP esidential Election in Florida: Did the Space Race and the National Prestige Issue Play an Important Role?" (2000). UNF Graduate Theses and Dissertations. 134. https://digitalcommons.unf.edu/etd/134 This Master's Thesis is brought to you for free and open access by the Student Scholarship at UNF Digital Commons. It has been accepted for inclusion in UNF Graduate Theses and Dissertations by an authorized administrator of UNF Digital Commons. For more information, please contact Digital Projects. © 2000 All Rights Reserved THE 1960 PRESIDENTIAL ELECTION IN FLORIDA: DID THE SPACE RACE AND THE NATIONAL PRESTIGE ISSUE PLAY AN IMPORTANT ROLE? by Randy Wade Babish A thesis submitted to the Department of History in partial fulfillment of the requirements for the degree of Master of Arts in History UNIVERSITY OF NORTH FLORIDA COLLEGE OF ARTS AND SCIENCES December, 2000 Unpublished work © Randy Wade Babish The thesis of Randy Wade Babish is approved: (Date) Signature Deleted Signature Deleted Signature Deleted Signature Deleted Accepted for the College: Signature Deleted Signature Deleted eanofGfaduate rues ACKNOWLEDGEMENTS Although my name appears on the title page and I assume full responsibility for the final product and its content, the quality of this work was greatly enhanced by the guidance of several individuals. First, the members of my thesis committee, Dr. -
Imagining and Building a New Encyclopedia
UvA-DARE (Digital Academic Repository) Sum of all knowledge: Wikipedia and the encyclopedic urge Salor, F.E. Publication date 2012 Link to publication Citation for published version (APA): Salor, F. E. (2012). Sum of all knowledge: Wikipedia and the encyclopedic urge. General rights It is not permitted to download or to forward/distribute the text or part of it without the consent of the author(s) and/or copyright holder(s), other than for strictly personal, individual use, unless the work is under an open content license (like Creative Commons). Disclaimer/Complaints regulations If you believe that digital publication of certain material infringes any of your rights or (privacy) interests, please let the Library know, stating your reasons. In case of a legitimate complaint, the Library will make the material inaccessible and/or remove it from the website. Please Ask the Library: https://uba.uva.nl/en/contact, or a letter to: Library of the University of Amsterdam, Secretariat, Singel 425, 1012 WP Amsterdam, The Netherlands. You will be contacted as soon as possible. UvA-DARE is a service provided by the library of the University of Amsterdam (https://dare.uva.nl) Download date:29 Sep 2021 2. Imagining and Building a New Encyclopedia It is quite natural that such developments should seem like marvels and that initially, deeming them to be impossible, the mind should reject any pursuit of them. But, according to a common slogan, do we not live in a time in which yesterday’s utopia is today’s dream and tomorrow’s reality? Paul Otlet Microphotographic Book, 1906 2.1 Introduction The modern encyclopedia, as it existed in the beginning of the 20th century, was the culmination of a continuous evolution that can be traced back to its Enlightenment origins, which in turn was the transformation of a much older ideal. -
Hitchhiker's Guide to the Galaxy
THE HITCHHIKER'S GUIDE TO THE GALAXY BY DOUGLAS ADAMS 2001 HANOMAG D OCUMENT VERSION 1.0 C OPYRIGHT © DOUGLAS A DAMS for Jonny Brock and Clare Gorst and all other Arlingtonians for tea, sympathy, and a sofa Far out in the uncharted backwaters of the unfashionable end of the western spiral arm of the Galaxy lies a small unregarded yellow sun. Orbiting this at a distance of roughly ninety-two million miles is an utterly insignificant little blue green planet whose ape- descended life forms are so amazingly primitive that they still think digital watches are a pretty neat idea. This planet has - or rather had - a problem, which was this: most of the people on it were unhappy for pretty much of the time. Many solutions were suggested for this problem, but most of these were largely concerned with the movements of small green pieces of paper, which is odd because on the whole it wasn't the small green pieces of paper that were unhappy. And so the problem remained; lots of the people were mean, and most of them were miserable, even the ones with digital watches. Many were increasingly of the opinion that they'd all made a big mistake in coming down from the trees in the first place. And some said that even the trees had been a bad move, and that no one should ever have left the oceans. And then, one Thursday, nearly two thousand years after one man had been nailed to a tree for saying how great it would be to be nice to people for a change, one girl sitting on her own in a small cafe in Rickmansworth suddenly realized what it was that had been going wrong all this time, and she finally knew how the world could be made a good and happy place. -
The Lunar Orbital Prospector
THE LUNAR ORBITAL PROSPECTOR FrankJ. Redd, James N. Cantrell, and Greg McCurdy N 9 _ " 174 6 Center for Space Engineering Utah State University Logan UT 84322 The establishment of lunar bases will not end the need for remote sensing of the lunar surface by orbiting ldatforms. Human and robotic surface exploration u_ necessarily be limited to some proximate distance from the _ base..Near real-time, higlvresolulior_ global characterization of the lunar surface by orOiting sensing systems will continue to be essential to the understaru_'ng of the Moon's geophysical structure and the location of exploitable minerals and deposits of raw materials. 7be Lunar OrM'tal Prospector (LOP) is an orbiting sensing platforra capable of supIxgt_ng a varleO_ of modular sensing packages. Serviced by a lunarbased shuttle, the LOP will permit the exchange of instrument packages to meet evolving mission needs. The ability to recover, modify, and rotate sensing pack, ages allows their reuse in varying combinations. Combining this _'OJ u_th robust orbit moa_'fication capabilities and near real-time telemetry links provides considerable system responsiveness. Maintenance and mo_'fication of the LOP orbit are accomplished through use of an onboard propuL_n system that burns lunar-supplied oxygen and aluminum. The relatively low performance of such a system is more than comlxomated for by the elimination of the need for Earth-supplied prolx, liants. The LOP concept envisions a continuous expansion of capability through the incorporation of new instrument technologies and the addition of ptatforms. INTRODUCTION surface (Hood et aL, 1985). A long-term remote-sensing mission, in conjunction with a manned lunar base, can expand the LGO's Human and robotic exploration of the Moon during the last geophysical and geochemical database and serve as the "eyes and two decades has greatly increased our knowledge of the Moon's ears" of the manned base by searching for hmar transient events geophysical and geochemical nature.