Future Missions Related to the Determination of the Elemental and Isotopic Composition of Earth, Moon and the Terrestrial Planets
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The Surface Operations Framework – Transitioning from Early Analogue Experiments to Future Lunar Missions
THE SURFACE OPERATIONS FRAMEWORK – TRANSITIONING FROM EARLY ANALOGUE EXPERIMENTS TO FUTURE LUNAR MISSIONS Sebastian Martin(1), Toril Bye Rinnan(2), Mehran Sarkarati(3), Kim Nergaard(4) (1) ESA/ESOC, Robert-Bosch-Straße 5, 64293 Darmstadt, Germany, Email: [email protected] (2) Solenix Deutschland GmbH, Spreestraße 3, 64295 Darmstadt, Germany, Email: [email protected] (3) ESA/ESOC, Robert-Bosch-Straße 5, 64293 Darmstadt, Germany, Email: [email protected] (4) ESA/ESOC, Robert-Bosch-Straße 5, 64293 Darmstadt, Germany, Email: [email protected] ABSTRACT to assess the financial and technical feasibility of new mission concepts, technologies and studies before This paper provides an overview of a family of possibly advancing them to the next phases of activities performed within the European Space implementation of a mission. Operations Centre (ESOC) to prepare for future robotic As the result of one such concurrent design study in missions on the lunar surface and beyond. 2009, the METERON concept was created. METERON – the Multi-purpose End-To-End Robotics Operations Over the course of nearly a decade, ESOC has been Network – was initiated to prepare for future human and gradually building up expertise for future surface robotic exploration scenarios. These future scenarios operations activities. foresee robotic assets controlled on the surface of Moon This paper describes or Mars, with humans operating those assets from an - the activities and corresponding systems prepared orbiting vehicle or by Earth ground control. The benefit from the ground up before concrete missions were of near real-time remote asset operations is to reduce defined, human risks and cost by not having to land humans and - how we are now covering a range of activities return them from the surface, while still being able to where we have requirements from missions in the control robotic assets with short transmission delays definition phases while continuing to build on from an orbiter. -
ESA Strategy for Science at the Moon
ESA UNCLASSIFIED - Releasable to the Public ESA Strategy for Science at the Moon ESA UNCLASSIFIED - Releasable to the Public EXECUTIVE SUMMARY A new era of space exploration is beginning, with multiple international and private sector actors engaged and with the Moon as its cornerstone. This renaissance in lunar exploration will offer new opportunities for science across a multitude of disciplines from planetary geology to astronomy and astrobiology whilst preparing the knowledge humanity will need to explore further into the Solar System. Recent missions and new analyses of samples retrieved during Apollo have transformed our understanding of the Moon and the science that can be performed there. We now understand the scientific importance of further exploration of the Moon to understand the origins and evolution of Earth and the cosmic context of life’s emergence on Earth and our future in space. ESA’s priorities for scientific activities at the Moon in the next ten years are: • Analysis of new and diverse samples from the Moon. • Detection and characterisation of polar water ice and other lunar volatiles. • Deployment of geophysical instruments and the build up a global geophysical network. • Identification and characterisation of potential resources for future exploration. • Deployment long wavelength radio astronomy receivers on the lunar far side. • Characterisation of the dynamic dust, charge and plasma environment. • Characterisation of biological sensitivity to the lunar environment. ESA UNCLASSIFIED - Releasable to the Public -
Lunar Ionosphere Exploration Method Using Auroral Kilometric Radiation
Earth Planets Space, 63, 47–56, 2011 Lunar ionosphere exploration method using auroral kilometric radiation Yoshitaka Goto1, Takamasa Fujimoto1, Yoshiya Kasahara1, Atsushi Kumamoto2, and Takayuki Ono2 1Kanazawa University, Kanazawa, Japan 2Tohoku University, Sendai, Japan (Received June 3, 2009; Revised November 10, 2010; Accepted January 14, 2011; Online published February 21, 2011) The evidence of a lunar ionosphere provided by radio occultation experiments performed by the Soviet spacecraft Luna 19 and 22 has been controversial for the past three decades because the observed large density is difficult to explain theoretically without magnetic shielding from the solar wind. The KAGUYA mission provided an opportunity to investigate the lunar ionosphere with another method. The natural plasma wave receiver (NPW) and waveform capture (WFC) instruments, which are subsystems of the lunar radar sounder (LRS) on board the lunar orbiter KAGUYA, frequently observe auroral kilometric radiation (AKR) propagating from the Earth. The dynamic spectra of the AKR sometimes exhibit a clear interference pattern that is caused by phase differences between direct waves and waves reflected on a lunar surface or a lunar ionosphere if it exists. It was hypothesized that the electron density profiles above the lunar surface could be evaluated by comparing the observed interference pattern with the theoretical interference patterns constructed from the profiles with ray tracing. This method provides a new approach to examining the lunar ionosphere that does not involve the conventional radio occultation technique. Key words: KAGUYA, lunar ionosphere, auroral kilometric radiation. 1. Introduction 2001; Kurata et al., 2005). The dense plasma layers may The lunar atmosphere is extremely tenuous compared to be maintained by these strong fields. -
Appendix 1: Venus Missions
Appendix 1: Venus Missions Sputnik 7 (USSR) Launch 02/04/1961 First attempted Venus atmosphere craft; upper stage failed to leave Earth orbit Venera 1 (USSR) Launch 02/12/1961 First attempted flyby; contact lost en route Mariner 1 (US) Launch 07/22/1961 Attempted flyby; launch failure Sputnik 19 (USSR) Launch 08/25/1962 Attempted flyby, stranded in Earth orbit Mariner 2 (US) Launch 08/27/1962 First successful Venus flyby Sputnik 20 (USSR) Launch 09/01/1962 Attempted flyby, upper stage failure Sputnik 21 (USSR) Launch 09/12/1962 Attempted flyby, upper stage failure Cosmos 21 (USSR) Launch 11/11/1963 Possible Venera engineering test flight or attempted flyby Venera 1964A (USSR) Launch 02/19/1964 Attempted flyby, launch failure Venera 1964B (USSR) Launch 03/01/1964 Attempted flyby, launch failure Cosmos 27 (USSR) Launch 03/27/1964 Attempted flyby, upper stage failure Zond 1 (USSR) Launch 04/02/1964 Venus flyby, contact lost May 14; flyby July 14 Venera 2 (USSR) Launch 11/12/1965 Venus flyby, contact lost en route Venera 3 (USSR) Launch 11/16/1965 Venus lander, contact lost en route, first Venus impact March 1, 1966 Cosmos 96 (USSR) Launch 11/23/1965 Possible attempted landing, craft fragmented in Earth orbit Venera 1965A (USSR) Launch 11/23/1965 Flyby attempt (launch failure) Venera 4 (USSR) Launch 06/12/1967 Successful atmospheric probe, arrived at Venus 10/18/1967 Mariner 5 (US) Launch 06/14/1967 Successful flyby 10/19/1967 Cosmos 167 (USSR) Launch 06/17/1967 Attempted atmospheric probe, stranded in Earth orbit Venera 5 (USSR) Launch 01/05/1969 Returned atmospheric data for 53 min on 05/16/1969 M. -
An Overview of Hayabusa2 Mission and Asteroid 162173 Ryugu
Asteroid Science 2019 (LPI Contrib. No. 2189) 2086.pdf AN OVERVIEW OF HAYABUSA2 MISSION AND ASTEROID 162173 RYUGU. S. Watanabe1,2, M. Hira- bayashi3, N. Hirata4, N. Hirata5, M. Yoshikawa2, S. Tanaka2, S. Sugita6, K. Kitazato4, T. Okada2, N. Namiki7, S. Tachibana6,2, M. Arakawa5, H. Ikeda8, T. Morota6,1, K. Sugiura9,1, H. Kobayashi1, T. Saiki2, Y. Tsuda2, and Haya- busa2 Joint Science Team10, 1Nagoya University, Nagoya 464-8601, Japan ([email protected]), 2Institute of Space and Astronautical Science, JAXA, Japan, 3Auburn University, U.S.A., 4University of Aizu, Japan, 5Kobe University, Japan, 6University of Tokyo, Japan, 7National Astronomical Observatory of Japan, Japan, 8Research and Development Directorate, JAXA, Japan, 9Tokyo Institute of Technology, Japan, 10Hayabusa2 Project Summary: The Hayabusa2 mission reveals the na- Combined with the rotational motion of the asteroid, ture of a carbonaceous asteroid through a combination global surveys of Ryugu were conducted several times of remote-sensing observations, in situ surface meas- from ~20 km above the sub-Earth point (SEP), includ- urements by rovers and a lander, an active impact ex- ing global mapping from ONC-T (Fig. 1) and TIR, and periment, and analyses of samples returned to Earth. scan mapping from NIRS3 and LIDAR. Descent ob- Introduction: Asteroids are fossils of planetesi- servations covering the equatorial zone were performed mals, building blocks of planetary formation. In partic- from 3-7 km altitudes above SEP. Off-SEP observa- ular carbonaceous asteroids (or C-complex asteroids) tions of the polar regions were also conducted. Based are expected to have keys identifying the material mix- on these observations, we constructed two types of the ing in the early Solar System and deciphering the global shape models (using the Structure-from-Motion origin of water and organic materials on Earth [1]. -
Global Exploration Roadmap
The Global Exploration Roadmap January 2018 What is New in The Global Exploration Roadmap? This new edition of the Global Exploration robotic space exploration. Refinements in important role in sustainable human space Roadmap reaffirms the interest of 14 space this edition include: exploration. Initially, it supports human and agencies to expand human presence into the robotic lunar exploration in a manner which Solar System, with the surface of Mars as • A summary of the benefits stemming from creates opportunities for multiple sectors to a common driving goal. It reflects a coordi- space exploration. Numerous benefits will advance key goals. nated international effort to prepare for space come from this exciting endeavour. It is • The recognition of the growing private exploration missions beginning with the Inter- important that mission objectives reflect this sector interest in space exploration. national Space Station (ISS) and continuing priority when planning exploration missions. Interest from the private sector is already to the lunar vicinity, the lunar surface, then • The important role of science and knowl- transforming the future of low Earth orbit, on to Mars. The expanded group of agencies edge gain. Open interaction with the creating new opportunities as space agen- demonstrates the growing interest in space international science community helped cies look to expand human presence into exploration and the importance of coopera- identify specific scientific opportunities the Solar System. Growing capability and tion to realise individual and common goals created by the presence of humans and interest from the private sector indicate and objectives. their infrastructure as they explore the Solar a future for collaboration not only among System. -
Arecibo Radar Observations of 14 High-Priority Near-Earth Asteroids in CY2020 and January 2021 Patrick A
Arecibo Radar Observations of 14 High-Priority Near-Earth Asteroids in CY2020 and January 2021 Patrick A. Taylor (LPI, USRA), Anne K. Virkki, Flaviane C.F. Venditti, Sean E. Marshall, Dylan C. Hickson, Luisa F. Zambrano-Marin (Arecibo Observatory, UCF), Edgard G. Rivera-Valent´ın, Sriram S. Bhiravarasu, Betzaida Aponte-Hernandez (LPI, USRA), Michael C. Nolan, Ellen S. Howell (U. Arizona), Tracy M. Becker (SwRI), Jon D. Giorgini, Lance A. M. Benner, Marina Brozovic, Shantanu P. Naidu (JPL), Michael W. Busch (SETI), Jean-Luc Margot, Sanjana Prabhu Desai (UCLA), Agata Rozek˙ (U. Kent), Mary L. Hinkle (UCF), Michael K. Shepard (Bloomsburg U.), and Christopher Magri (U. Maine) Summary We propose the continuation of the long-running project R3037 to physically and dynamically characterize the population of near-Earth asteroids with the Arecibo S-band (2380 MHz; 12.6 cm) planetary radar system. The objectives of project R3037 are to: (1) collect high-resolution radar images of and (2) report ultra-precise radar astrometry for the strongest predicted radar targets for the 2020 calendar year plus early January 2021. Such images will be used for three-dimensional shape modeling as the data sets allow. These observations will be carried out as part of the NASA- funded Arecibo planetary radar program, Grant No. 80NSSC19K0523, to PI Anne Virkki (Arecibo Observatory, University of Central Florida) with Patrick Taylor as Institutional PI at the Lunar and Planetary Institute (Universities Space Research Association). Background Radar is arguably the most powerful Earth-based technique for post-discovery physical and dynamical characterization of near-Earth asteroids (NEAs) and plays a crucial role in the nation’s planetary defense initiatives led through the NASA Planetary Defense Coordination Office. -
AAS SFMC Manuscript Format Template
(Preprint) AAS 18-344 REFINED MISSION ANALYSIS FOR HERACLES – A ROBOTIC LUNAR SURFACE SAMPLE RETURN MISSION UTILIZING HUMAN INFRASTRUCTURE Dr.-Ing. Florian Renk,* Dr. rer. nat. Markus Landgraf,† and Lorenzo Bucci‡ In the frame of the International Space Exploration Coordination Working Group the European Space Agency is participating in the planning of future ex- ploration architectures. The mission concept for the robotic lander mission (Human Enhanced Robotic Architecture and Capability for Lunar Exploration and Science – HERACLES) has matured meanwhile. The mission aims for a human assisted sample return from the lunar surface, while at the same time providing a qualification opportunity for technologies required for a crewed lu- nar lander. Human spaceflight rating is required for parts of the mission, since the sample return shall not be via a direct return trajectory, but the samples shall be transported via Orion, and thus docking of the robotic lander to the LOP-G will be required. This paper shall provide an update on the current mission de- sign as agreed between the international partners and the associated mission analysis as all the intermediate and final orbits have been selected for the base- line. The implications of the design decision as well as some alternatives that can serve as a backup scenario will be presented as well. The paper will first present the baseline mission sequence and will then focus on aspects of particu- lar interest as e.g. the strong limitation in the launch window design and the ren- dezvous and docking strategy. INTRODUCTION HERACLES is intended as a human-robotic architecture in the frame of preparations for hu- man exploration activities on the lunar surface. -
Arxiv:1912.04482V1 [Physics.Space-Ph] 10 Dec 2019
manuscript submitted to Radio Science Measuring the Earth's Synchrotron Emission from Radiation Belts with a Lunar Near Side Radio Array Alexander Hegedus1, Quentin Nenon2, Antoine Brunet3, Justin Kasper1, Ang´elicaSicard3, Baptiste Cecconi4, Robert MacDowall5, Daniel Baker6 1University of Michigan, Department of Climate and Space Sciences and Engineering, Ann Arbor, Michigan, USA 2Space Sciences Laboratory, University of California, Berkeley, CA, USA 3ONERA / DPHY, Universit´ede Toulouse, F-31055 Toulouse France 4LESIA, Observatoire de Paris, Universit PSL, CNRS, Sorbonne Universit, Univ. de Paris, Meudon, France 5NASA Goddard Space Flight Center, Greenbelt, MD, USA 6University of Colorado Boulder, Laboratory for Atmospheric and Space Physics, Boulder, Colorado, USA Key Points: • Synchrotron emission between 500-1000 kHz has a total flux density of 1.4-2 Jy at lunar distances • A 10 km radio array with 16000 elements could detect the emission in 12-24 hours with moderate noise • Changing electron density can make detections 10x faster at lunar night, 10x slower at lunar noon arXiv:1912.04482v1 [physics.space-ph] 10 Dec 2019 Corresponding author: Alexander Hegedus, [email protected] {1{ manuscript submitted to Radio Science Abstract The high kinetic energy electrons that populate the Earth's radiation belts emit synchrotron emissions because of their interaction with the planetary magnetic field. A lunar near side array would be uniquely positioned to image this emission and provide a near real time measure of how the Earth's radiation belts are responding to the current solar in- put. The Salammb^ocode is a physical model of the dynamics of the three-dimensional phase-space electron densities in the radiation belts, allowing the prediction of 1 keV to 100 MeV electron distributions trapped in the belts. -
Thermal Inertia of Asteroid Ryugu Using Dawn-Side Thermal Images by TIR on Hayabusa2
EPSC Abstracts Vol. 13, EPSC-DPS2019-268-1, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. Thermal inertia of asteroid Ryugu using dawn-side thermal images by TIR on Hayabusa2 Tatsuaki Okada (1,2), Tetsuya Fukuhara (3), Satoshi Tanaka (1), Makoto Taguchi (3), Takehiko Arai (4), Naoya Sakatani (1), Yuri Shimaki (1), Hiroki Senshu (5), Hirohide Demura (6), Yoshiko Ogawa (6), Kentaro Suko (6), Tomohiko Sekiguchi (7), Toru Kouyama (8), Jorn Helbert (9), Thomas G. Mueller (10), Axel Hagermann (11), Jens Biele (12), Matthias Grott (9), Maximilian Hamm (9), Marco Delbo (13), and Hayabusa2 TIR Team (1) Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara, Japan, (2) University of Tokyo, Japan, (3) Rikkyo University, Tokyo, Japan, (4) Ashikaga University, Japan, (5) Chiba Institute of Technology, Narashino, Japan, (6) University of Aizu, Aizu-Wakamatsu, Japan, (7) Hokkaido University of Education, Asahikawa, Japan, (8) National Institute of Advanced Industrial Science and Technology, Tokyo, Japan, (9) German Aerospace Centre, Berlin, Germany, (10) Max-Planck Institute for Extraterrestrial Physics, Garching, Germany, (11) University of Stirling, UK, (12) German Aerospace Centre, Cologne, Germany, (13) Code d’Azur Observatory, Nice, France. Abstract 30 % porosity. The surface features imaged by MasCAM on MASCOT indicated the very fluffy A thermal inertia map of the C-type Near-Earth surface [5]. This time the temperature at the night asteroid 162173 Ryugu has been derived using the side area observed by TIR was applied improve the one-rotation global thermal image sets observed from estimate of the global thermal inertia of Ryugu. -
Apollo Over the Moon: a View from Orbit (Nasa Sp-362)
chl APOLLO OVER THE MOON: A VIEW FROM ORBIT (NASA SP-362) Chapter 1 - Introduction Harold Masursky, Farouk El-Baz, Frederick J. Doyle, and Leon J. Kosofsky [For a high resolution picture- click here] Objectives [1] Photography of the lunar surface was considered an important goal of the Apollo program by the National Aeronautics and Space Administration. The important objectives of Apollo photography were (1) to gather data pertaining to the topography and specific landmarks along the approach paths to the early Apollo landing sites; (2) to obtain high-resolution photographs of the landing sites and surrounding areas to plan lunar surface exploration, and to provide a basis for extrapolating the concentrated observations at the landing sites to nearby areas; and (3) to obtain photographs suitable for regional studies of the lunar geologic environment and the processes that act upon it. Through study of the photographs and all other arrays of information gathered by the Apollo and earlier lunar programs, we may develop an understanding of the evolution of the lunar crust. In this introductory chapter we describe how the Apollo photographic systems were selected and used; how the photographic mission plans were formulated and conducted; how part of the great mass of data is being analyzed and published; and, finally, we describe some of the scientific results. Historically most lunar atlases have used photointerpretive techniques to discuss the possible origins of the Moon's crust and its surface features. The ideas presented in this volume also rely on photointerpretation. However, many ideas are substantiated or expanded by information obtained from the huge arrays of supporting data gathered by Earth-based and orbital sensors, from experiments deployed on the lunar surface, and from studies made of the returned samples. -
Planetary Exploration : Progress and Promise
PLANET ARY EXPLORATION PROGRESS AND PROMISE CONTENTS: NASA PLANETARY EXPLORATION PLANS: SIGNIFICANT EVENTS PLANETARY EXPLORATION PROGRESS-1978 NASA SPACE SCIENCE PROGRAM FUNDING: 5 -YEAR PLAN NASA OSS 5-YEAR PLAN: PLANETARY PROGRAM FUNDING REFERENCE COP'I PLEASE DO NOT REMOVE compiled by Dr. Leonard Srnka, Staff Scientist Lunar and Planetary Institute 3303 NASA Road One Houston, Texas 77058 Lunar and Planetary Institute Contribution No. 297 (June 1978 update> NASA PLANETARY EXPLORATION PLANS SIGNIFICANT EVENTS MISSION EVENTS PIONEER VENUS ORBITER ORBIT INSERTION, DECEMBER 1978 PIONEER VENUS MULTIPROBE VENUS ENCOUNTER/ENTRY, DECEMBER 1978 PIONEER 11 SATURN ENCOUNTER, SEPTEMBER 1979 VOYAGER 1 JUPITER ENCOUNTER, MARCH 1979 SATURN ENCOUNTER, NOVEMBER 1980 VOYAGER 2 JUPITER ENCOUNTER, JULY 1979 SATURN ENCOUNTER, AUGUST 1981 URANUS ENCOUNTER, JANUARY 1986 SOLAR MAXIMUM MISSION LAUNCH, OCTOBER 1979 VENUS ORBITAL IMAGING RADAR VENUS ENCOUNTER, SPRING 1985 SOLAR POLAR MISSION JUPITER ENCOUNTER, 1984 SOLAR POLES PASSAGE, 1986 GALILEO MISSION MARS FLYBY, APRIL 1982 JUPITER ENCOUNTER (ORBIT INSERTION/ PROBE ENTRY), 1985 COMET HALLEYlTEMPEL, . 2'J MISSION• HALLEY ENCOUNTER, NOVEMBER 1985 TEMPEL 2 ENCOUNTER, JULY 1988 or COMET ENCKE RENDEZVOUS ENCKE ENCOUNTER, 1987 MARS GEOCHEMICAL ORBITER MARS ENCOUNTER, 1987 MARS SAMPLE RETURN MARS ENCOUNTER, 1989 EARTH RETURN, 1991 SATURN ORBITER DUAL PROBE SATURN ENCOUNTER, 1992 from NASA Headquarters 5-year plan May 1978 PLANETARY EXPLORATION -- PROGRESS AND PROMISE CONTENT S: Planetary exploration progress - 1977 fig. 1 The future fig. 2 Inner planets plan fig. 3 Outer planets plan fig. 4 Small bodies plan fig. 5 compiled by Dr. Leonard Srnka, Staff Scientist LUNAR SCIENCE INSTITUTE 3303 NASA Road One Houston, TX 77058 September 1977 LUNAR SCIENCE INSTITUTE CONTRIBUTION No.