The Global Exploration Roadmap
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国内外における今後の火星探査の動向調査 Research on Trend About
Eco-Engineering, 22(4), 185-191, 2010 内外の研究動向 国内外における今後の火星探査の動向調査 Research on Trend about Domestic and International Mars Exploration in the future 新井真由美* Mayumi Arai* 日本科学未来館 〒135-0064 東京都江東区青海2-3-6 National Museum of Emerging Science and Innovation 2-3-6, Aomi, Koto-ku, Tokyo 135-0064, Japan 月ごとにフォボスに接近し、高解像度ステレオカメラ 1 .国外における今後の火星探査 (HRSC)で、1 ピクセル 4.4 m という、これまでにない 2011 年以降打ち上げを予定している火星探査計画は、 ほどの高解像度でフォボス表面を撮影している。フォボ アメリカ航空宇宙局(NASA)が主体となる計画のほか、 スは、地球に対する月のように常に火星に同じ面を向け 欧州宇宙機関(ESA)、ロシア、中国の計画がある。こ て公転しているが、フライバイを行うことによってフォ れらの主な目的と特徴を述べる。 ボスの異なる面の観測が可能となる。これらのデータ 1.1 Phobos-Grunt は、Phobos-Grunt の着陸地点選出に用いられる予定であ Phobos-Grunt は、火星の衛星フォボスの表面サンプル る。現在、フォボスへのオペレーションと着陸が安全な を地球に持ち帰るロシアの計画である。Phobos-Grunt と 場所として、5 °S-5 °N, 230-235 °E が選ばれている(Zak, は、“フォボスの土壌”という意味である。2009 年に打 2010; Mars Express’s web site, 2010)。 ち上げが予定されていたが、2011 年に延期された。現 1.2 蛍火 1 号(Yinghuo-1) 時点での打ち上げウィンドウは、2011 年 12 月 25 日。 蛍火 1 号(インホワ・ワン)は、中国の航空宇宙産 2012 年 8 月から 9 月に火星軌道に入り、2013 年から 業が開発した中国初の小型の火星周回衛星で、Phobos- 火星軌道を周り、2013 年にフォボスに着地。そして、 Grunt に相乗りして 2011 年の打ち上げを予定している。 2014 年に地球に帰還予定である。フォボスは、直径が約 Yinghuo という名前は「蛍」を意味する。蛍火 1 号の 27 × 22 × 19 km の不整形な形をした炭素質の C 型小惑 大きさは、長さ 75 cm、幅 75 cm、高さ 60 cm で、質量 星で、密度が平均 1.85 g/cm3 と小さく、氷と岩石の混合 110 kg、太陽電池パネルを広げると 7.85 m。2012 年に 物から構成されていると考えられている。フォボスは、 Phobos-Grunt から分離され、火星の赤道軌道に投入され、 火星の重力に捕獲された小惑星であるという説のほか、 約 2 年間、火星上空のプラズマ環境と磁場の詳細な観測 火星に隕石が衝突した際に飛び散った岩石が集まって誕 などを行う予定である(Zak, 2010)。蛍火 1 号は、中国 生したという説、太陽系の惑星形成時の残余物が集まっ 初の惑星探査機で、有人探査の「神舟」シリーズ、月探 たという説が考えられているが、実際どのようなメカニ 査の「嫦娥」シリーズに継ぐ、第 3 の宇宙探査に位置づ ズムで火星の赤道面に捕獲され、進化してきたか未だ議 けられる。 -
Space Reporter's Handbook Mission Supplement
CBS News Space Reporter's Handbook - Mission Supplement Page 1 The CBS News Space Reporter's Handbook Mission Supplement Shuttle Mission STS-125: Hubble Space Telescope Servicing Mission 4 Written and Produced By William G. Harwood CBS News Space Analyst [email protected] CBS News 5/10/09 Page 2 CBS News Space Reporter's Handbook - Mission Supplement Revision History Editor's Note Mission-specific sections of the Space Reporter's Handbook are posted as flight data becomes available. Readers should check the CBS News "Space Place" web site in the weeks before a launch to download the latest edition: http://www.cbsnews.com/network/news/space/current.html DATE RELEASE NOTES 08/03/08 Initial STS-125 release 04/11/09 Updating to reflect may 12 launch; revised flight plan 04/15/09 Adding EVA breakdown; walkthrough 04/23/09 Updating for 5/11 launch target date 04/30/09 Adding STS-400 details from FRR briefing 05/04/09 Adding trajectory data; abort boundaries; STS-400 launch windows Introduction This document is an outgrowth of my original UPI Space Reporter's Handbook, prepared prior to STS-26 for United Press International and updated for several flights thereafter due to popular demand. The current version is prepared for CBS News. As with the original, the goal here is to provide useful information on U.S. and Russian space flights so reporters and producers will not be forced to rely on government or industry public affairs officers at times when it might be difficult to get timely responses. All of these data are available elsewhere, of course, but not necessarily in one place. -
MELOS Rover (Smaller Than MER) Engineering Primary Objectives Rough-Terrain Traversability • Design & Development of the Mobility System: I.E
MEPAG meeting 2015 Current plan of the MELOS, a proposed Japanese Mars mission Hirdy Miyamoto (University of Tokyo) on behalf of MELOS working group NOTE ADDED BY JPL WEBMASTER: This content has not been approved or adopted by, NASA, JPL, or the California Institute of Technology. This document is being made available for information purposes only, and any views and opinions expressed herein do not necessarily state or reflect those of NASA, JPL, or the California Institute of Technology. Background of the Japanese Mars program JAXA’s missions to solar system bodies NOZOMI Mars Mission (1998) (did not arrive at Mars) Hayabusa asteroid mission (2003) Kaguya lunar mission (2007) Akatsuki Venus mission (2011) Venus orbit insertion delayed until 2015 Hayabusa 2 asteroid mission (2014) Successfully launched • MELOS working group@JAXA from 2008 MELOS used to stand for “Mars Explorations with Landers and Orbiters” Lander(s) and orbiters (meteorology and atmospheric escape) • MELOS is now down-scaled to be an EDL (+Rover) mission for an engineering demonstration • MELOS (Mars Exploration of Life-Organism Search) is one of 4 proposals for Announcement of Opportunity for medium- class missions, Feb. 2015, JAXA Proposed mission outline of MELOS Launch Aug. 2020 (Sep. 2022) Mars Arrival Feb. 2021 (Apr. 2023) Primary objective: Science objectives Engineering demonstration Current status/activity on Mars (Pin-point landing, long-range - Meteorology roving) - Geology - Biology Proposed landing scenario of MELOS Cruise module separation & entry Entry-Descent-Landing (EDL) module Guided flight 909kg (wet), 803kg (dry) Parachute deployment Interplanetary Cruise Module Atmospheric Entry Module Aeroshell Module Skycrane Powered Landing Module descent Rover Landing accuracy 20 x 14 km Rover touchdown MELOS Rover (smaller than MER) Engineering primary objectives Rough-terrain traversability • Design & development of the mobility system: i.e. -
Tventy Five Years with CANADARM
Canada celebrates Tventy five years with CANADARM -Canada’s ticket to the Space Shuttle and ISS Human participation is necessary in order to build large constructions in Like a space – that is a fact, to put it mildly human arm - but without the use of the right tools it will be impossible. With nerves When the plans for a shuttle of copper wiring, system first were introduced, a bones of graphite manipulator system was introduced as fibre, and electric a necessity, a robotic arm that could motors for muscles, deploy and retrieve space hardware Canadarm is like from the payload bay of the shuttle. the human arm. It Canadian industrial companies has rotating joints: accepted the challenge, and the two at the shoulder, manipulator system, Canadarm, made one at the elbow its space debut in November, 1981. and three at the The design and building of the Shuttle wrist. At 15 metres Remote Manipulator System also and weighing less marked the beginning of Canada’s than 480 kilograms, close collaboration with NASA in Canadarm can manned space flight. lift over 30,000 But the development did not kilograms in the stop there. A similar system for the weightlessness of Canadarm2 gives Canadian scientists space station was developed, and in space-or the mass of a fully loaded access to the Station’s laboratory April 2001, Space Shuttle Endeavour bus, using less electricity than a facilities to conduct experiments. delivered a package that was Canada’s teakettle. It also entitles key contribution to the International The brain of “In fact, the Station could Canada to send the system is a an astronaut to Space Station, the Canadarm 2. -
Comparison of the Orbital Properties of Jupiter Trojan Asteroids and Trojan Dust Xiaodong Liu and Jürgen Schmidt
A&A 614, A97 (2018) https://doi.org/10.1051/0004-6361/201832806 Astronomy & © ESO 2018 Astrophysics Comparison of the orbital properties of Jupiter Trojan asteroids and Trojan dust Xiaodong Liu and Jürgen Schmidt Astronomy Research Unit, University of Oulu, 90014 Oulu, Finland e-mail: [email protected] Received 10 February 2018 / Accepted 7 March 2018 ABSTRACT In a previous paper we simulated the orbital evolution of dust particles from the Jupiter Trojan asteroids ejected by the impacts of interplanetary particles, and evaluated their overall configuration in the form of dust arcs. Here we compare the orbital properties of these Trojan dust particles and the Trojan asteroids. Both Trojan asteroids and most of the dust particles are trapped in the Jupiter 1:1 resonance. However, for dust particles, this resonance is modified because of the presence of solar radiation pressure, which reduces the peak value of the semi-major axis distribution. We find also that some particles can be trapped in the Saturn 1:1 resonance and higher order resonances with Jupiter. The distributions of the eccentricity, the longitude of pericenter, and the inclination for Trojans and the dust are compared. For the Trojan asteroids, the peak in the longitude of pericenter distribution is about 60 degrees larger than the longitude of pericenter of Jupiter; in contrast, for Trojan dust this difference is smaller than 60 degrees, and it decreases with decreasing grain size. For the Trojan asteroids and most of the Trojan dust, the Tisserand parameter is distributed in the range of two to three. Key words. meteorites, meteors, meteoroids – planets and satellites: rings – minor planets, asteroids: general – zodiacal dust – celestial mechanics – solar wind 1. -
Preliminary Mission Analysis and Orbit Design for Next Mars Exploration
Trans. JSASS Aerospace Tech. Japan Vol. 8, No. ists27, pp. Tk_7-Tk_12, 2010 Topics Preliminary Mission Analysis and Orbit Design for Next Mars Exploration By Naoko OGAWA 1), Mutsuko Y. MORIMOTO1), Yuichi TSUDA1,2), Tetsuya YAMADA1,2), Kazuhisa FUJITA1,3), Tomohiro YAMAGUCHI4), Yasuhiro KAWAKATSU1,2), Takashi KUBOTA1,2) and Jun’ichiro KAWAGUCHI1,2) 1)JAXA Space Exploration Center, Japan Aerospace Exploration Agency, Sagamihara, Japan 2)Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara, Japan 3)Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency, Tokyo, Japan 4)The Graduate University for Advanced Studies, Sagamihara, Japan (Received July 21st, 2009) Japan has launched many interplanetary spacecraft for exploration of solar system bodies including Mars. Now we are planning the next Mars mission in the late 2010’s. This paper describes the preliminary mission analysis and orbit design for this plan. The combined exploration by several spacecraft requires complicated and careful consideration, different from those for single-probe missions. Mission plans to realize required configuration by a single launch and simple simulation results are reported. Key Words: Mars, Mission Analysis, Orbit Design, MELOS 1. Introduction 2.1.1. Meteorological orbiter for martian climate One orbiter of the two, called hereafter as the meteorological In 2008, Japan Aerospace Exploration Agency (JAXA) orbiter, aims understanding of the interaction between the has established a novel working group toward a novel Mars atmosphere and subsurface ice, and atmospheric dynamics. exploration program named MELOS, an acronym for “Mars Global, high-resolution and continuous mapping of water vapor, Exploration with Lander-Orbiter Synergy”1). As its name clouds, dusts and atmospheric temperature will be performed indicates, this is an ambitious mission composed of several with imaging cameras from the apoapsis of its highly elliptic landers and orbiters, schematically illustrated in Fig. -
The Impact of Human Factors on Future Long Duration Human Space Exploration Missions En Route to Mars
Open Archive TOULOUSE Archive Ouverte ( OATAO ) OATAO is an open access repository that collects the work of Toulouse researchers and makes it freely available over the web where possible. This is an author-deposited version published in : http://oatao.univ-toulouse.fr/ Eprints ID : 13827 To cite this version : Ferraioli, Giuseppe and Causse, Mickael and Lizy-Destrez, Stéphanie and Gourinat, Yves Habitability of manned vehicules : the impact of human factors on future long duration human space exploration missions en route to Mars. (2015) In: 64th International Astronautical Congress, Beijing, China, September 23-27, 2013, 2013 - 2013 (Beijing, China). Any correspondance concerning this service should be sent to the repository administrator: [email protected] HABITABILITY OF MANNED VEHICLES: THE IMPACT OF HUMAN FACTORS ON FUTURE LONG DURATION HUMAN SPACE EXPLORATION MISSIONS EN ROUTE TO MARS Giuseppe Ferraioli ISAE - Institut Sup´erieurde l'A´eronautiqueet de l'Espace, Italy, [email protected] Dr. Mickael Causse ISAE, France, [email protected] Mrs. St´ephanie Lizy-Destrez ISAE, France, [email protected] Prof. Yves Gourinat ISAE, France, [email protected] August 3, 2013 Abstract Placing humans in space for a long duration mission beyond Earth's neighborhood implies the design of a highly complex system to travel, live and work safely in the hostile environment of deep space. In order to identify all the constraints from both engineering and human sides, a meticulous system engineering approach has to be followed and the human sciences, including incorporation of ideas from artists, ergonomists and psychologists, have to be integrated in the very early stages of the mission design. -
Np-2015-03-011-Jsc-Expedition-43
National Aeronautics and Space Administration International Space Station [MISSION SUMMARY] began March 11, 2015 and ends May 13, 2015. This expedition will include the EXPEDITION 43 beginning of research projects focusing on the One-Year mission, which includes medical, psychological and biomedical studies with NASA Astronaut Scott Kelly and Roscosmos Cosmonaut Mikhail Kornienko who will spend a year in space. Expedition 43 also will include astrophysics research, physical science investigations and technology demonstrations. There are no spacewalks planned during Expedition 43. THE CREW: Soyuz TMA-15M • Launch: Nov. 23, 2014 • Landing: May 13, 2015 Soyuz TMA-16M • March 27, 2015 • Landing: September 11, 2015 Note: Kelly and Kornienko will remain onboard until March 2016 Terry Virts (NASA) – Commander Gennady Padalka (Roscosmos) – Flight Engineer (Verts) (Puh-DOLL-kuh) Born: Baltimore Born: Krasnodar, Russia Interests: Astronomy, baseball, coaching youth sports Interests: Diving, parachute sport and theater Spaceflights: STS-130 Spaceflights: Soyuz-TM-28/Mir Exp. 26, ISS Exps. 9, 19 Bio: http://go.nasa.gov/w1eH1s and 20 Twitter: @AstroTerry Bio: http://go.nasa.gov/1u1HVm6 Anton Shkaplerov (Roscosmos) – Flight Engineer Scott Kelly (NASA) – Flight Engineer (SHKAP-luh-roff) Born: Sevastopol, Crimean Peninsula Born: Orange, New Jersey Interests: Fishing, golf, sports, travel Interests: Racquetball, running, water sports and Spaceflights: Exps. 29 and 30 weight lifting Bio: http://go.nasa.gov/1Dmd1Yd Spaceflights: STS-103, STS-118, Exps. 25 and 26 Twitter: @AntonAstrey Bio: http://go.nasa.gov/SbcMZD Twitter: @StationCDRKelly Instagram: stationcdrkelly Samantha Cristoforetti (ESA) – Flight Engineer Mikhail Kornienko (Roscosmos) – Flight Engineer (Cris-ta-four-REHT-ee) (Kor-knee-EHN-koh) Born: Milan, Italy Born: Syzran, Russia Interests: Hiking, reading, scuba diving, travel, yoga Interests: Mountaineering Spaceflights: Exps. -
Habitation Module 26 July 2016 – NASA Advisory Council, Human Exploration and Operations Committee
National Aeronautics and Space Administration Habitation Module 26 July 2016 – NASA Advisory Council, Human Exploration and Operations Committee Jason Crusan | Advanced Exploration Systems Director | NASA Headquarters 2 Human Exploration of Mars Is Hard Common Capability Needs Identified from Multiple Studies Days Reliable In-Space 800-1,100 44 min Transportation Total me crew is Maximum two- away from Earth – way communicaon for orbit missions all in 2me delay – 300 KW Micro-g and Radia2on Autonomous Opera2ons Total connuous transportaon power 130 t Heavy-LiA Mass 20-30 t Long Surface Stay Multiple Ability to 500 Days Launches per land large mission payloads Surface Operations Dust Toxicity and 100 km 11.2 km/s Long Range Explora2on Earth Entry Speed 20 t Oxygen produced for ascent to orbit - ISRU 3 The Habitation Development Challenge HABITATATION CAPABILITY Days 800-1,100 Habitation Systems – Total me crew is AES/ISS/STMD away from Earth – • Environmental Control & Life Support for orbit missions all in • Autonomous Systems Micro-g and Radia2on Integrated • EVA testing on ISS • Fire Safety • Radiation Protection Habitation Systems - Crew Health – HRP Long Surface Stay • Human Research 500 Days • Human Performance • Exercise PROVING GROUND Validation in cislunar space • Nutrition Habitation Capability– NextSTEP BAA / Int. Partners • Studies and ground prototypes of pressurized volumes 4 Specific Habitation Systems Objectives TODAY FUTURE Habitation The systems, tools, and protec:ons that allow Systems Elements humans to live and work -
Commercial Orbital Transportation Services
National Aeronautics and Space Administration Commercial Orbital Transportation Services A New Era in Spaceflight NASA/SP-2014-617 Commercial Orbital Transportation Services A New Era in Spaceflight On the cover: Background photo: The terminator—the line separating the sunlit side of Earth from the side in darkness—marks the changeover between day and night on the ground. By establishing government-industry partnerships, the Commercial Orbital Transportation Services (COTS) program marked a change from the traditional way NASA had worked. Inset photos, right: The COTS program supported two U.S. companies in their efforts to design and build transportation systems to carry cargo to low-Earth orbit. (Top photo—Credit: SpaceX) SpaceX launched its Falcon 9 rocket on May 22, 2012, from Cape Canaveral, Florida. (Second photo) Three days later, the company successfully completed the mission that sent its Dragon spacecraft to the Station. (Third photo—Credit: NASA/Bill Ingalls) Orbital Sciences Corp. sent its Antares rocket on its test flight on April 21, 2013, from a new launchpad on Virginia’s eastern shore. Later that year, the second Antares lifted off with Orbital’s cargo capsule, (Fourth photo) the Cygnus, that berthed with the ISS on September 29, 2013. Both companies successfully proved the capability to deliver cargo to the International Space Station by U.S. commercial companies and began a new era of spaceflight. ISS photo, center left: Benefiting from the success of the partnerships is the International Space Station, pictured as seen by the last Space Shuttle crew that visited the orbiting laboratory (July 19, 2011). More photos of the ISS are featured on the first pages of each chapter. -
NASA's Lunar Orbital Platform-Gatway
The Space Congress® Proceedings 2018 (45th) The Next Great Steps Feb 28th, 9:00 AM NASA's Lunar Orbital Platform-Gatway Tracy Gill NASA/KSC Technology Strategy Manager Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Gill, Tracy, "NASA's Lunar Orbital Platform-Gatway" (2018). The Space Congress® Proceedings. 17. https://commons.erau.edu/space-congress-proceedings/proceedings-2018-45th/presentations/17 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. National Aeronautics and Space Administration NASA’s Lunar Orbital Platform- Gateway Tracy Gill NASA/Kennedy Space Center Exploration Research & Technology Programs February 28, 2018 45th Space Congress Space Policy Directive-1 “Lead an innovative and sustainable program of exploration with commercial and international partners to enable human expansion across the solar system and to bring back to Earth new knowledge and opportunities. Beginning with missions beyond low-Earth orbit, the United States will lead the return of humans to the Moon for long-term exploration and utilization, followed by human missions to Mars and other destinations.” 2 LUNAR EXPLORATION CAMPAIGN 3 4 STRATEGIC PRINCIPLES FOR SUSTAINABLE EXPLORATION • FISCAL REALISM • ECONOMIC OPPORTUNITY Implementable in the near-term with the buying -
Workstation Designs for a Cis-Lunar Deep Space Habitat
Workstation Designs for a Cis-lunar Deep Space Habitat A. Scott Howe, PhD1 Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, California 91109 Using the International Standard Payload Rack (ISPR) system, a suite of workstations required for deep space missions have been proposed to fill out habitation functions in an International Space Station (ISS) derived Cis-lunar Deep Space Habitat. This paper introduces the functional layout of the Cis-lunar habitat design, and describes conceptual designs for modular deployable work surfaces, General Maintenance Workstation (GMWS), In-Space Manufacturing Workstation (ISMW), Intra-Vehicular Activity Telerobotics Work Station (IVA-TRWS), and Galley / Wardroom. Nomenclature AES = NASA Advanced Exploration Systems project ATHLETE = All-Terrain Hex-Limbed Extra-Terrestrial Explorer robotic mobility system CTB = Cargo Transfer Bag D-RATS = NASA Desert Research and Technology Studies DSH = Deep Space Habitat EAM = Exploration Augmentation Module EXPRESS = EXpedite the PRocessing of Experiments for Space Station GMWS = General Maintenance Work Station HDU = Habitat Demonstration Unit HERA = Human Exploration Research Analog ISMW = In-Space Manufacturing Work Station ISPR = International Standard Payload Rack ISIS = International Subrack Interface Standard ISS = International Space Station IVA = Intravehicular Activity MPCV = Multi-Purpose Crew Vehicle MPLM = Multi-Purpose Logistics Module PLSS = Personal Life Support System RAF = Random Access Frames TRWS = Telerobotics