Lunar Daylight Exploration
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Spacecraft Deliberately Crashed on the Lunar Surface
A Summary of Human History on the Moon Only One of These Footprints is Protected The narrative of human history on the Moon represents the dawn of our evolution into a spacefaring species. The landing sites - hard, soft and crewed - are the ultimate example of universal human heritage; a true memorial to human ingenuity and accomplishment. They mark humankind’s greatest technological achievements, and they are the first archaeological sites with human activity that are not on Earth. We believe our cultural heritage in outer space, including our first Moonprints, deserves to be protected the same way we protect our first bipedal footsteps in Laetoli, Tanzania. Credit: John Reader/Science Photo Library Luna 2 is the first human-made object to impact our Moon. 2 September 1959: First Human Object Impacts the Moon On 12 September 1959, a rocket launched from Earth carrying a 390 kg spacecraft headed to the Moon. Luna 2 flew through space for more than 30 hours before releasing a bright orange cloud of sodium gas which both allowed scientists to track the spacecraft and provided data on the behavior of gas in space. On 14 September 1959, Luna 2 crash-landed on the Moon, as did part of the rocket that carried the spacecraft there. These were the first items humans placed on an extraterrestrial surface. Ever. Luna 2 carried a sphere, like the one pictured here, covered with medallions stamped with the emblem of the Soviet Union and the year. When Luna 2 impacted the Moon, the sphere was ejected and the medallions were scattered across the lunar Credit: Patrick Pelletier surface where they remain, undisturbed, to this day. -
FARSIDE Probe Study Final Report
Study Participants List, Disclaimers, and Acknowledgements Study Participants List Principal Authors Jack O. Burns, University of Colorado Boulder Gregg Hallinan, California Institute of Technology Co-Authors Jim Lux, NASA Jet Propulsion Laboratory, California Institute of Andres Romero-Wolf, NASA Jet Propulsion Laboratory, California Technology Institute of Technology Lawrence Teitelbaum, NASA Jet Propulsion Laboratory, California Tzu-Ching Chang, NASA Jet Propulsion Laboratory, California Institute of Technology Institute of Technology Jonathon Kocz, California Institute of Technology Judd Bowman, Arizona State University Robert MacDowall, NASA Goddard Space Flight Center Justin Kasper, University of Michigan Richard Bradley, National Radio Astronomy Observatory Marin Anderson, California Institute of Technology David Rapetti, University of Colorado Boulder Zhongwen Zhen, California Institute of Technology Wenbo Wu, California Institute of Technology Jonathan Pober, Brown University Steven Furlanetto, UCLA Jordan Mirocha, McGill University Alex Austin, NASA Jet Propulsion Laboratory, California Institute of Technology Disclaimers/Acknowledgements Part of this research was carried out at the Jet Propulsion Laboratory, California Institute of Technology, under a contract with the National Aeronautics and Space Administration. The cost information contained in this document is of a budgetary and planning nature and is intended for informational purposes only. It does not constitute a commitment on the part of JPL and/or Caltech © 2019. -
Rine and the Apennine Mountains. INSTITUTION National Aeronautics and Space Administration, Washington, D.C
DOCUMENT RESUME ED 053 930 SE 012 016 AUTHOR Simmons, Gene TITLE On the Moon with Apollo 15,A Guidebook to Hadley Rine and the Apennine Mountains. INSTITUTION National Aeronautics and Space Administration, Washington, D.C. PUB DATE Jun 71 NOTE 52p. AVAILABLE FROM Superintendent of Documents, U.S. Government Printing Office, Washington, D.C. 20402 (3300-0384 $0.50) EDRS PRICE EDRS Price MF-$0.65 HC-$3.29 DESCRIPTORS *Aerospace Technology, Geology, Reading Materials, Resource Materials IDENTIFIERS *Lunar Studies, Moon ABSTRACT The booklet, published before the Apollo 15 mission, gives a timeline for the mission; describes and illustrates the physiography of the landing site; and describes and illustrates each lunar surface scientific experiment. Separate timelines are included for all traverses (the traverses are the Moon walks and, for Apollo 15, the Moon rides in the Rover) with descriptions of activities at each traverse stop. Each member of the crew and the backup crew is identified. Also included is a bibliography of lunar literature and glossary of terms used in lunar studies. Photographs and diagrams are utilized throughout. Content is descriptive and informative but with a minimum of technical detail. (Author/PR) , ON THE MOON WITH APOLLO 15 A Guidebook to Hadley Rille and the Apennine Mountains U.S. DEPARTMENT OFHEALTH, EDUCATION,& WELFARE OFFICE OF EDUCATION THIS DOCUMENT HAS SEENREPRO- DUCED EXACTLY AS RECEIVEDFROM THE PERSON OR ORGANIZATIONORIG INATING IT. POINTS OF VIEWOR OPIN IONS STATED DO NOTNECESSARILY REPRESENT OFFICIAL OFFICEOF EDU CATION POSITION OR POLICY isr) 1..r1 w fl R CO iiii0OP" O NATIONAL AERONAUTICS AND SPACE ADMINISTRATION June 1971 1 \n ON THE MOON WITH APOLLO 15 A uidebook to Hadley Rille and the Apennine Mountains by Gene Simmons Chief Scientist Manned Spacecraft Center NATIONAL AERONAUTICS AND SPACE ADMINISTRATION June 1971 2 For sale by the Superintendent of Documents, U.S. -
NASA's Recommendations to Space-Faring Entities: How To
National Aeronautics and Space Administration NASA’s Recommendations to Space-Faring Entities: How to Protect and Preserve the Historic and Scientific Value of U.S. Government Lunar Artifacts Release: July 20, 2011 1 National Aeronautics and Space Administration Revision and History Page Status Revision No. Description Release Date Release Baseline Initial Release 07/20/2011 Update Rev A Updated with imagery from Apollo 10/28/2011 missions 12, 14-17. Added Appendix D: Available Photo Documentation of Apollo Hardware 2 National Aeronautics and Space Administration HUMAN EXPLORATION & OPERATIONS MISSION DIRECTORATE STRATEGIC ANALYSIS AND INTEGRATION DIVISION NASA HEADQUARTERS NASA’S RECOMMENDATIONS TO SPACE-FARING ENTITIES: HOW TO PROTECT AND PRESERVE HISTORIC AND SCIENTIFIC VALUE OF U.S. GOVERNMENT ARTIFACTS THIS DOCUMENT, DATED JULY 20, 2011, CONTAINS THE NASA RECOMMENDATIONS AND ASSOCIATED RATIONALE FOR SPACECRAFT PLANNING TO VISIT U.S. HERITAGE LUNAR SITES. ORGANIZATIONS WITH COMMENTS, QUESTIONS OR SUGGESTIONS CONCERNING THIS DOCUMENT SHOULD CONTACT NASA’S HUMAN EXPLORATION & OPERATIONS DIRECTORATE, STRATEGIC ANALYSIS & INTEGRATION DIVISION, NASA HEADQUARTERS, 202.358.1570. 3 National Aeronautics and Space Administration Table of Contents REVISION AND HISTORY PAGE 2 TABLE OF CONTENTS 4 SECTION A1 – PREFACE, AUTHORITY, AND DEFINITIONS 5 PREFACE 5 DEFINITIONS 7 A1-1 DISTURBANCE 7 A1-2 APPROACH PATH 7 A1-3 DESCENT/LANDING (D/L) BOUNDARY 7 A1-4 ARTIFACT BOUNDARY (AB) 8 A1-5 VISITING VEHICLE SURFACE MOBILITY BOUNDARY (VVSMB) 8 A1-6 OVERFLIGHT -
The Flexible Lunar Architecture for Exploration (FLARE) Designed for the Artemis-3 Moon 2024 Mission and Beyond
NASA/TP-2020-220517 The Flexible Lunar Architecture for Exploration (FLARE) Designed for the Artemis-3 Moon 2024 mission and beyond Dr. Michael E. Evans Planetary Scientist Astromaterials Research and Exploration Science (ARES) Division NASA Johnson Space Center [email protected] 281-483-3276 Mr. Lee D. Graham Senior Research Engineer Astromaterials Research and Exploration Science (ARES) Division NASA Johnson Space Center [email protected] 281-244-5192 National Aeronautics and Space Administration Johnson Space Center Houston, Texas 77058 April 2020 NASA STI Program Office ... in Profile Since its founding, NASA has been dedicated to the • CONFERENCE PUBLICATION. advancement of aeronautics and space science. The Collected papers from scientific and NASA scientific and technical information (STI) technical conferences, symposia, seminars, program plays a key part in helping NASA or other meetings sponsored or maintain this important role. co-sponsored by NASA. The NASA STI program operates under the • SPECIAL PUBLICATION. Scientific, auspices of the Agency Chief Information Officer. technical, or historical information from It collects, organizes, provides for archiving, and NASA programs, projects, and missions, disseminates NASA’s STI. The NASA STI often concerned with subjects having program provides access to the NTRS Registered substantial public interest. and its public interface, the NASA Technical Report Server, thus providing one of the largest • TECHNICAL TRANSLATION. collections of aeronautical and space science STI in English-language translations of foreign the world. Results are published in both non-NASA scientific and technical material pertinent to channels and by NASA in the NASA STI Report NASA’s mission. Series, which includes the following report types: Specialized services also include organizing • TECHNICAL PUBLICATION. -
The Moon Topic Read
The Moon The regular daily and monthly rhythms of Earth’s only natural satellite, the Moon, have guided timekeepers for thousands of years. Its influence on Earth’s cycles, notably tides, has been charted by many cultures in many ages. Earth's moon compared to Earth The Moon moderates Earth’s wobble on its axis, leading to a relatively stable climate over billions of years. From Earth, we always see the same face of the Moon because the Moon is spinning on its axis at the same speed that it is going around Earth (that is, it is in synchronous rotation with Earth). Lunar Terrain The light areas of the Moon are known as the highlands. The dark features, called maria (Latin for seas), are impact basins that were filled with lava between 4.2 and 1.2 billion years ago. These light and dark areas represent rocks of different composition and ages, which provide evidence for how the early crust may have crystallized from a lunar magma ocean. The craters themselves, which have been preserved for billions of years, provide an impact history for the Moon and other bodies in the inner solar system. Lunar Origins The leading theory of the Moon’s origin is that a Mars-sized body collided with Earth approximately 4.5 billion years ago, and the resulting debris from both Earth and the impactor accumulated to form our natural satellite. The newly formed Moon was in a molten state. Within about 100 million years, most of the global “magma ocean” had crystallized, with less-dense rocks floating upward and eventually forming the lunar crust. -
Planning for Sun-Synchronous Lunar Polar Roving
Planning for Sun-Synchronous Lunar Polar Roving Nathan D. Otten CMU-RI-TR-18-21 Submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy in Robotics. The Robotics Institute Carnegie Mellon University Pittsburgh, Pennsylvania 15213 May 2018 Thesis Committee: David Wettergreen, Co-chair William \Red" Whittaker, Co-chair Alonzo Kelly Anthony Colaprete, NASA Ames Paul Tompkins, SpaceX Copyright © 2018 by Nathan Otten. All rights reserved. Abstract Lunar polar resources can accelerate deep space exploration by resupplying mis- sions with oxygen, water, and propellent. Before lunar resupply can be established, the distribution and concentration of water ice and other volatiles abundant at the poles of the Moon must be verified and mapped. The need for affordable, scalable exploration of the lunar poles motivates the deployment of solar-powered rovers and planning strategies that sustain robotic missions beyond a single two-week period of lunar daylight. Reliance on solar power at the lunar poles gives rise to significant challenges| and opportunities|for individual rovers to achieve multi-lunar-day longevity. Solar- powered rovers require persistent sunlight for power and heat, lest they succumb to the cryogenic temperatures of lunar night. Although constrained by thermal conditions and available power, opportunistic polar rovers can maintain warmth and ample solar power for several months by following sun-synchronous routes. Strategic, informed route planning that exploits polar lighting enables sustained lunar polar roving and resource prospecting not possible by other means. This research develops polar roving strategies and applies global path planning methods to generate spatiotemporal routes that provide multiple lunar days of un- interrupted sunlight while satisfying constraints on rover speed, terrain slope, and direct-to-Earth communication. -
Midsize Lunar Rover Development and Testing
Midsize Lunar Rover Development and Testing P. Visscher*, D. Woolley** *Program Manager, Ontario Drive and Gear, Canada e-mail: [email protected] **Project Design Engineer, Ontario Drive and Gear, Canada e-mail: [email protected] Abstract 2 Design and Development The Canadian Space Agency has been funding the design and development of numerous rover prototypes Mid-size utility rovers associated with in-situ since 2008. A credible candidate for a Canadian lunar resource utilization (ISRU), must have the ability to flight-program is an evolving class of rovers (known climb steep slopes and traverse rough terrain, whilst internally at Ontario Drive & Gear as “J-class rovers”, which includes the Juno 1, Juno II, and Artemis Jr. transporting large payloads or native material. The rovers must also be able to operate for extended periods rovers. of time while exposed to the native environmental Compared to previous or in-service Mars rovers, extremes. In recent times of fiscal restraint and J-class rovers also share common design attributes which cross-border collaboration, it is also imperative that a include increased ruggedness, reduced parts-count and an emphasis in reducing the effort expelled to integrate mid-size utility rover be adaptable and highly reliable, payloads, sensors and thermal subsystems. Since 2010, ultimately to achieve mission success and maintain public engagement. J-class rovers have undergone significant laboratory and Arguably, one method to meet these mission goals analogue field testing and subsequent continued and that exemplified by the J-class mid-size utility rovers, development of several key rover sub-systems such as the chassis, drivetrain, suspension and traction involves initially marrying terrestrial design convergence subsystems. -
Energetic Efficiency Evaluation of the Lunar Roving Vehicles Using Computer Simulation
TEM Journal. Volume 7, Issue 4, Pages 937-943, ISSN 2217-8309, DOI: 10.18421/TEM74-35, November 2018. Energetic Efficiency Evaluation of the Lunar Roving Vehicles Using Computer Simulation Calin Doru Iclodean 1, Calin Dan Iclodean 2 1Technical University of Cluj-Napoca, Romania 2 Estaca Ecole d’Ingénieurs, Saint-Quentin-e n-Yvelines, France Abstract – This paper studies the energetic 1. Introduction performance of a Lunar Roving Vehicle using computer simulation with the AVL Cruise software. The Moon is the celestial body which has The simulation tasks include an energy consumption fascinated mankind during millennia. Since ancient calculation over the determined extra vehicular times, people have tried to uncover the Moon’s activity and based on the simulation results, a mysteries, and many dreamt of treading the lunar comparative analysis is performed between the AVL grounds long before the emergence of the modern Cruise simulation results and the NASA recordings of technology that made this journey possible. This the energy balance resulting from computer technology has come to fruition in the years 1950- simulations made in 1971, as well as the real results recorded by the crew of astronauts during the Apollo 1970 with the Russians space exploration missions 15 mission. The purpose of this paper is to design a (launch of the first Earth orbiting satellite Sputnik virtual Lunar Roving Vehicle and to simulate its and the first manned space capsule Vostok with operation in the lunar environment. The architecture Russian astronaut Yuri Gagarin [1]) and the of the Lunar Roving Vehicle will be based on the American Apollo program (Apollo 11 Moon landing original NASA LRV design, but using current and Neil Armstrong’s first steps on the Moon [2]). -
Llie LUNAR ROVING VEHICLE-N 9 3 HISTORICAL PERSPECTIVE
PRECEDING PAGE flt.ANK i'JOT F!LMED 619 lliE LUNAR ROVING VEHICLE-N 9 3 -14008 HISTORICAL PERSPECTIVE Saverio F. Morea Research and Technology Office NASA Marshall Space Right Center Huntsville AL 35812 As NASA proceeds with its studies, planning, arui technology efforts in preparing for the early twenty .first century, it seems appropriate to reexamine past programs for potential applicability in meeting futun! national space science and exploration goals arui objectives. Both the National Commission on Space ( NCOS) study and NASAs "Sally Ride study" suggest futun! programs inoolving n!turning to the Moon and establishing mans permanent pn!sence then!, arui/or visiting the planet Mars in lxith the unmanned and manned mode. Regardless of when and which of these new lxJ/d initiatives is selected as our next national space goal, implementing these potentially neu• national thrusts in space u>ill undoubtedly n!quin! the use of both manned and remotely controlled roving vehicles. 7berefore, the purpose of this paper is to raise the consdousness ler>el of the current space exploration planners to what, in the early 1970s, was a highly successful roving l>ehicle. During the Apollo program, the l!(!bicle known as the Lunar Rolling Vehicle ( LRV) was designed for canying two astronauts, their t<XJls, and the equipment needed for rndimentary exploration of the Moon. This paper contains a discussion of the vehicle, its characteristics, arui its use on the Moon. Conceivably, the LRV has the potential to meet some futun! n!quin!ments, either with n!latit>ely low cost modifications or 1>ia an er10lutionary route. -
Unique Abilities of Hopper Spacecraft to Enable National Objectives for Solar System Exploration
UNIQUE ABILITIES OF HOPPER SPACECRAFT TO ENABLE NATIONAL OBJECTIVES FOR SOLAR SYSTEM EXPLORATION EPHRAIM ROBERT LANFORD B.S. Engineering Harvey Mudd College, 2006 Submitted to the Engineering Systems Division and the Department of Aeronautics and Astronautics in partial fulfillment of the requirements for the degrees of MASTER OF SCIENCE IN TECHNOLOGY AND POLICY and MASTER OF SCIENCE IN AERONAUTICS AND ASTRONAUTICS at the MASSACHUSETTS INSTITUTE OF TECHNOLOGY February 2011 © 2011 Massachusetts Institute of Technology. All rights reserved. Signature of author: Technology and Policy Program Department of Aeronautics and Astronautics January 27, 2011 Certified by: Jeffrey A. Hoffman Professor of the Practice of Aeronautics and Astronautics Thesis Supervisor Certified by: John Danis Group Leader, Mission Architectures and Applications Charles Stark Draper Laboratory Accepted by: Dava J. Newman Professor of Aeronautics and Astronautics & Engineering Systems, MacVicar Faculty Fellow Director of Technology and Policy Program Accepted by: Eytan H. Modiano Associate Professor of Aeronautics and Astronautics Chair, Graduate Program Committee, Department of Aeronautics and Astronautics 2 UNIQUE ABILITIES OF HOPPER SPACECRAFT TO ENABLE NATIONAL OBJECTIVES FOR SOLAR SYSTEM EXPLORATION Ephraim Robert Lanford B.S. Engineering Harvey Mudd College, 2006 Submitted to the Engineering Systems Division and the Department of Aeronautics and Astronautics on January 27, 2011 in partial fulfillment of the requirements for the degrees of Master of Science in Technology and Policy and Master of Science in Aeronautics and Astronautics at the Massachusetts Institute of Technology ABSTRACT In comparison with conventional and other conceived approaches, hopper spacecraft offer unique advantages in exploring Solar System objects beyond Earth. The present work began with a survey – based on documents from the White House, Congress, NASA, and the international planetary science community – of exploration plans and objectives in the United States. -
4. Lunar Architecture
4. Lunar Architecture 4.1 Summary and Recommendations As defined by the Exploration Systems Architecture Study (ESAS), the lunar architecture is a combination of the lunar “mission mode,” the assignment of functionality to flight elements, and the definition of the activities to be performed on the lunar surface. The trade space for the lunar “mission mode,” or approach to performing the crewed lunar missions, was limited to the cislunar space and Earth-orbital staging locations, the lunar surface activities duration and location, and the lunar abort/return strategies. The lunar mission mode analysis is detailed in Section 4.2, Lunar Mission Mode. Surface activities, including those performed on sortie- and outpost-duration missions, are detailed in Section 4.3, Lunar Surface Activities, along with a discussion of the deployment of the outpost itself. The mission mode analysis was built around a matrix of lunar- and Earth-staging nodes. Lunar-staging locations initially considered included the Earth-Moon L1 libration point, Low Lunar Orbit (LLO), and the lunar surface. Earth-orbital staging locations considered included due-east Low Earth Orbits (LEOs), higher-inclination International Space Station (ISS) orbits, and raised apogee High Earth Orbits (HEOs). Cases that lack staging nodes (i.e., “direct” missions) in space and at Earth were also considered. This study addressed lunar surface duration and location variables (including latitude, longi- tude, and surface stay-time) and made an effort to preserve the option for full global landing site access. Abort strategies were also considered from the lunar vicinity. “Anytime return” from the lunar surface is a desirable option that was analyzed along with options for orbital and surface loiter.