Communications and the Lunar Outpost Student Edition
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SPECIAL Comet Shoemaker-Levy 9 Collides with Jupiter
SL-9/JUPITER ENCOUNTER - SPECIAL Comet Shoemaker-Levy 9 Collides with Jupiter THE CONTINUATION OF A UNIQUE EXPERIENCE R.M. WEST, ESO-Garching After the Storm Six Hectic Days in July eration during the first nights and, as in other places, an extremely rich data The recent demise of comet Shoe ESO was but one of many profes material was secured. It quickly became maker-Levy 9, for simplicity often re sional observatories where observations evident that infrared observations, es ferred to as "SL-9", was indeed spectac had been planned long before the critical pecially imaging with the far-IR instru ular. The dramatic collision of its many period of the "SL-9" event, July 16-22, ment TIMMI at the 3.6-metre telescope, fragments with the giant planet Jupiter 1994. It is now clear that practically all were perfectly feasible also during day during six hectic days in July 1994 will major observatories in the world were in time, and in the end more than 120,000 pass into the annals of astronomy as volved in some way, via their telescopes, images were obtained with this facility. one of the most incredible events ever their scientists or both. The only excep The programmes at most of the other predicted and witnessed by members of tions may have been a few observing La Silla telescopes were also successful, this profession. And never before has a sites at the northernmost latitudes where and many more Gigabytes of data were remote astronomical event been so ac the bright summer nights and the very recorded with them. -
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 . -
Alternative Artemis III EVA Opportunities Near De Gerlache Crater D
Science NASADefinition-requested Team for input Artemis for the (2020 Artemis) III Science Definition Team, delivered September 8, 2020. 2044.pdf Alternative Artemis III EVA Opportunities near de Gerlache Crater D. A. Kring*, J. M. Bretzelder, I. Ganesh, N. Kumari, A. Lang, and M. A. Siegler Introduction. A topographic high point on the nearside rim of de Gerlache crater (Fig. 1) has an average solar illumination of 84% [1]. The point, site 011 of [1] and NASA’s Plan for Sustainable Lunar Exploration and Development is an attractive site to establish a solar power station if a distribution system can be developed. If that site is selected to be a long-term power station, then it may be important to avoid fouling or cluttering the location with a descent vehicle and deployed instruments until after a preliminary set of measurements has been made within the area. Thus, it may be interesting to consider other locations in the vicinity of site 011 for an Artemis III landing. Landing site and EVA options. To illustrate the types of options available, we provide a few details for an alternative area near the rim of de Gerlache crater (Fig. 1). The area occurs on an Earth-facing slope at an intersection created by the rim of de Gerlache crater and the rims of secondary craters that are mapped as the products of the Orientale basin-forming impact that occurred on the western limb of the Moon [2]. The area has a relatively smooth surface, but also contains a few small craters that may harbor small permanently shadowed regions (PSRs). -
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................................................................................. -
Planning a Mission to the Lunar South Pole
Lunar Reconnaissance Orbiter: (Diviner) Audience Planning a Mission to Grades 9-10 the Lunar South Pole Time Recommended 1-2 hours AAAS STANDARDS Learning Objectives: • 12A/H1: Exhibit traits such as curiosity, honesty, open- • Learn about recent discoveries in lunar science. ness, and skepticism when making investigations, and value those traits in others. • Deduce information from various sources of scientific data. • 12E/H4: Insist that the key assumptions and reasoning in • Use critical thinking to compare and evaluate different datasets. any argument—whether one’s own or that of others—be • Participate in team-based decision-making. made explicit; analyze the arguments for flawed assump- • Use logical arguments and supporting information to justify decisions. tions, flawed reasoning, or both; and be critical of the claims if any flaws in the argument are found. • 4A/H3: Increasingly sophisticated technology is used Preparation: to learn about the universe. Visual, radio, and X-ray See teacher procedure for any details. telescopes collect information from across the entire spectrum of electromagnetic waves; computers handle Background Information: data and complicated computations to interpret them; space probes send back data and materials from The Moon’s surface thermal environment is among the most extreme of any remote parts of the solar system; and accelerators give planetary body in the solar system. With no atmosphere to store heat or filter subatomic particles energies that simulate conditions in the Sun’s radiation, midday temperatures on the Moon’s surface can reach the stars and in the early history of the universe before 127°C (hotter than boiling water) whereas at night they can fall as low as stars formed. -
Project Horizon Report
Volume I · SUMMARY AND SUPPORTING CONSIDERATIONS UNITED STATES · ARMY CRD/I ( S) Proposal t c• Establish a Lunar Outpost (C) Chief of Ordnance ·cRD 20 Mar 1 95 9 1. (U) Reference letter to Chief of Ordnance from Chief of Research and Devel opment, subject as above. 2. (C) Subsequent t o approval by t he Chief of Staff of reference, repre sentatives of the Army Ballistic ~tissiles Agency indicat e d that supplementar y guidance would· be r equired concerning the scope of the preliminary investigation s pecified in the reference. In particular these r epresentatives requested guidance concerning the source of funds required to conduct the investigation. 3. (S) I envision expeditious development o! the proposal to establish a lunar outpost to be of critical innportance t o the p. S . Army of the future. This eva luation i s appar ently shar ed by the Chief of Staff in view of his expeditious a pproval and enthusiastic endorsement of initiation of the study. Therefore, the detail to be covered by the investigation and the subs equent plan should be as com plete a s is feas ible in the tin1e limits a llowed and within the funds currently a vailable within t he office of t he Chief of Ordnance. I n this time of limited budget , additional monies are unavailable. Current. programs have been scrutinized r igidly and identifiable "fat'' trimmed awa y. Thus high study costs are prohibitive at this time , 4. (C) I leave it to your discretion t o determine the source and the amount of money to be devoted to this purpose. -
Fn000030.Pdf
1) Viaggi ed esplorazioni- 205 2) Collana Paravia Viaggi- 226 3)Collana Alpes Viaggi- 240 4) Ebraismo- 390 5) Colonialismo Fascista- 513 6) L'Illustrazione Italiana- 522 7) Storia- 546 8) Fascismo- 609 9) Spionaggio- 626 10) Letteratura italiana- 635 11) Letteratura straniera- 648 12) Il Corriere dei Piccoli-658 13) Libri per Ragazzi-693 14) Sport- 701 15) Arte-727 Le immagini di tutti i libri proposti in questo catalogo ( e molti altri) sono disponibili nella sezione RICERCA del sito www.ferraguti.it , continuamente aggiornato, che vi invitiamo a visitare. Preghiamo i gentili clienti di comunicarci l'indirizzo email, al fine di poter inviare, qualora lo gradissero, comunicazioni e cataloghi intermedi rispetto alle "classiche" pubblicazioni trimestrali. Siamo sempre interessati all'acquisto di intere biblioteche e partite o blocchi di libri, riviste e stampe d'epoca, saremo grati a chi ci fornirà opportune segnalazioni. FERRAGUTI SERVICE s.a.s. di Ferraguti Ivo & C. Borgo Bernabei 4 - 43125 Parma Tel. e Fax 0521-286980- [email protected] [email protected] P. IVA 01779470341- C.C.I.A.A. PR Reg. Ditte n. 177878 Iscrizione Tribunale di Parma n. 22291 Conto Corrente Postale n. 11724432 Catalogo numero 90- I semestre 2013- Gennaio,Febbraio, Marzo 2013 Editore: Ferraguti Service s.a.s. (Responsabile Ivo Ferraguti) Tipografie Riunite Donati - Borgo Santa Chiara 6- 43125 Parma 2 Albertini Gianni, ALLA RICERCA DEI NAUFRAGHI DELL'"ITALIA". mille kilometri sulla banchisa., Libreria d'Italia, Milano, 1929, 8o, brossura e sovracoperta., bs.,seconda ediz., pp. 165. La spedizione Nobile. Con numerose e bellissime foto. € 31,00 3 Albieri Adele, CRISTOFORO COLOMBO alla scoperta dell'America., Paravia G.B. -
Go for Lunar Landing Conference Report
CONFERENCE REPORT Sponsored by: REPORT OF THE GO FOR LUNAR LANDING: FROM TERMINAL DESCENT TO TOUCHDOWN CONFERENCE March 4-5, 2008 Fiesta Inn, Tempe, AZ Sponsors: Arizona State University Lunar and Planetary Institute University of Arizona Report Editors: William Gregory Wayne Ottinger Mark Robinson Harrison Schmitt Samuel J. Lawrence, Executive Editor Organizing Committee: William Gregory, Co-Chair, Honeywell International Wayne Ottinger, Co-Chair, NASA and Bell Aerosystems, retired Roberto Fufaro, University of Arizona Kip Hodges, Arizona State University Samuel J. Lawrence, Arizona State University Wendell Mendell, NASA Lyndon B. Johnson Space Center Clive Neal, University of Notre Dame Charles Oman, Massachusetts Institute of Technology James Rice, Arizona State University Mark Robinson, Arizona State University Cindy Ryan, Arizona State University Harrison H. Schmitt, NASA, retired Rick Shangraw, Arizona State University Camelia Skiba, Arizona State University Nicolé A. Staab, Arizona State University i Table of Contents EXECUTIVE SUMMARY..................................................................................................1 INTRODUCTION...............................................................................................................2 Notes...............................................................................................................................3 THE APOLLO EXPERIENCE............................................................................................4 Panelists...........................................................................................................................4 -
JAXA's Space Exploration Activities
JAXA’s Space Exploration Activities Jun Gomi, Deputy Director General, JAXA Hayabusa 2 ✓ Asteroid Explorer of the C-type asteroid ✓ Launched in December, 2014 ✓ Reached target asteroid “Ryugu” in 2018 ✓ First successful touchdown to Ryugu on February 22, 2019 ✓ Return to Earth in 2020 (162173) Ryugu 2 Hayabusa 2 (c) JAXA, University of Tokyo, Kochi University, Rikkyo University, (c) JAXA, University of Tokyo, Kochi University, Rikkyo University, Nagoya University, Chiba Institute of Technology, Meiji University, Nagoya University, Chiba Institute of Technology, Meiji University, University of Aizu and AIST. University of Aizu, AIST Asteroid Ryugu photographed from a Asteroid Ryugu from an altitude of 6km. distance of about 20 km. The image Image was captured with the Optical was taken on June 30, 2018. Navigation Camera on July 20, 2018. Hayabusa 2 4 JAXA’s Plan for Space Exploration International • Utilization of ISS/Kibo • Cis-Lunar Platform (Gateway) Cooperation • Lunar exploration and beyond Industry & • JAXA Space Exploration Innovation Academia Hub Partnerships • Science Community discussions JAXA’s Overall Scenario for International Space Exploration Mars, others ★ Initial Exploration ★ Full Fledge Exploration MMX: JFY2024 • Science and search for life • Utilization feasibility exam. Kaguya Moon ©JAXA ©JAXA ©JAXA ©JAXA ©JAXA Full-fledged Exploration & SLIM Traversing exploration(2023- ) Sample Return(2026- ) Utilization (JFY2021) • Science exploration • S/R from far side • Cooperative science/resource • Water prospecting • Technology demo for human mission exploration by robotic and human HTV-X der.(2026- ) • Small probe deploy, data relay etc. Gateway Phase 1 Gateway (2022-) Phase 2 • Support for Lunar science Earth • Science using deep space Promote Commercialization International Space Station 6 SLIM (Smart Lander for Investigating Moon) ✓ Demonstrate pin-point landing on the moon. -
LRO Makes a Temperature Map of the Lunar South Pole 42
LRO Makes a Temperature Map of the Lunar South Pole 42 The Lunar Reconnaissance Orbiter (LRO) has recently created the first surface temperature map of the south polar region of the moon using date taken between September and October, 2009 when south polar temperatures were close to their annual maximum values. The colorized map shows the locations of several intensely cold impact craters that are potential cold traps for water ice as well as a range of other icy compounds commonly observed in comets. The approximate maximum temperatures at which these compounds would be frozen in place for more than a billion years is shown on the scale to the right. The LCROSS spacecraft was targeted to impact one of the coldest of these craters, and many of these compounds were observed in the ejecta plume. (Courtesy: UCLA/NASA/JPL) Problem 1 - The width of this map is 500 km. What are the diameters of Crater A (Shackleton) and Crater B (Amundsen) in kilometers? Problem 2 - In which colored areas might an astronaut expect to find conditions cold enough to recover all of the elements and molecules indicated in the vertical temperature scale to the right? Problem 3 - The Shackleton Crater (Crater A) is cold enough to trap water and methanol. From Problem 1, and assuming that the thickness of the water deposit is 100 meters, and occupies 10% of the volume of the circular crater, how many cubic meters of water-ice might be present? Space Math http://spacemath.gsfc.nasa.gov Answer Key 42 Problem 1 - The width of this map is 500 km. -
Technology Today Spring 2013
Spring 2012 TECHNOLOGY® today Southwest Research Institute® San Antonio, Texas Spring 2012 • Volume 33, No. 1 TECHNOLOGY today COVER Director of Communications Craig Witherow Editor Joe Fohn TECHNOLOGY Assistant Editor today Deborah Deffenbaugh D018005-5651 Contributing Editors Tracey Whelan Editorial Assistant Kasey Chenault Design Scott Funk Photography Larry Walther Illustrations Andrew Blanchard, Frank Tapia Circulation Southwest Research Institute San Antonio, Texas Gina Monreal About the cover Full-scale fire tests were performed on upholstered furniture Technology Today (ISSN 1528-431X) is published three times as part of a project to reduce uncertainty in determining the each year and distributed free of charge. The publication cause of fires. discusses some of the more than 1,000 research and develop- ment projects under way at Southwest Research Institute. The materials in Technology Today may be used for educational and informational purposes by the public and the media. Credit to Southwest Research Institute should be given. This authorization does not extend to property rights such as patents. Commercial and promotional use of the contents in Technology Today without the express written consent of Southwest Research Institute is prohibited. The information published in Technology Today does not necessarily reflect the position or policy of Southwest Research Institute or its clients, and no endorsements should be made or inferred. Address correspondence to the editor, Department of Communications, Southwest Research Institute, P.O. Drawer 28510, San Antonio, Texas 78228-0510, or e-mail [email protected]. To be placed on the mailing list or to make address changes, call (210) 522-2257 or fax (210) 522-3547, or visit update.swri.org. -
Sampling the SPA Basin Some Considerations Based on the Apollo Experience
Sampling the SPA Basin Some Considerations Based on the Apollo Experience Paul D. Spudis Applied Physics Laboratory Workshop on Science Associated with the Lunar Exploration Architecture February 27- March 2, 2007 How do you best sample the Moon? Samples without context have limited value Bulk planet properties, inventory of compositions Context requires either geologic field work or a simple regional setting Robotic missions tend to provide less context than human field study cf. Luna 20 and Apollo 16 Types of Exploratory Targets Reconnaissance Geologically simple sites where a “grab sample” of rocks and regolith can address and solve scientific issues Example: youngest mare lava flow, impact melt floor of fresh crater, regional pyroclastics Field Study Complex, multi-unit sites having a protracted evolution. Require human interaction, sampling, mapping, re-visiting field sites Examples: basin ejecta blanket, Aristarchus plateau, crater central peaks See Ryder et al., 1989, EOS, v. 70, n. 47, p. 1495; 1505-1520 Apollo Highlands Sampling Apollo 14 – Fra Mauro Sent to sample Fra Mauro Fm (Imbrium ejecta) Returned complex breccias; basaltic, KREEP-rich Which samples are Imbrium basin primary ejecta? Apollo 15 – Hadley-Apennines Sample front (deep Imbrium rim material) Anorthosite, KREEP basalts, mafic impact melts Which samples represent Imbrium basin melt? Apollo 16 – Descartes Sent to sample highland volcanic rocks Anorthositic debris, breccias, some mafic melts (VHA) Basin-related? If so, which ones? Apollo 17 – Taurus-Littrow Sample