Planet Earth Taken by Hayabusa-2
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Space Science in JAXA Planet Earth May 15, 2017 taken by Hayabusa-2 Saku Tsuneta, PhD JAXA Vice President Director General, Institute of Space and Astronautical Science 2017 IAA Planetary Defense Conference, May 15-19,1 Tokyo 1 Brief Introduction of Space Science in JAXA Introduction of ISAS and JAXA • As a national center of space science & engineering research, ISAS carries out development and in-orbit operation of space science missions with other directorates of JAXA. • ISAS is an integral part of JAXA, and has close collaboration with other directorates such as Research and Development and Human Spaceflight Technology Directorates. • As an inter-university research institute, these activities are intimately carried out with universities and research institutes inside and outside Japan. ISAS always seeks for international collaboration. • Space science missions are proposed by researchers, and incubated by ISAS. ISAS plays a strategic role for mission selection primarily based on the bottom-up process, considering strategy of JAXA and national space policy. 3 JAXA recent science missions HAYABUSA 2003-2010 AKARI(ASTRO-F)2006-2011 KAGUYA(SELENE)2007-2009 Asteroid Explorer Infrared Astronomy Lunar Exploration IKAROS 2010 HAYABUSA2 2014-2020 M-V Rocket Asteroid Explorer Solar Sail SUZAKU(ASTRO-E2)2005- AKATSUKI 2010- X-Ray Astronomy Venus Meteorogy ARASE 2016- HINODE(SOLAR-B)2006- Van Allen belt Solar Observation Hisaki 2013 4 Planetary atmosphere Close ties between space science and space technology Space Technology Divisions Space Flight Systems Technology driven Spacecraft Engineering Leads and creates space science programs Science driven Stimulates and encourages Space Science Divisions new technology development Space Astronomy Astrophysics Solar System Science 5 Interdisciplinary Space Science The First Interplanetary Micro-Spacecraft PROCYON Launched on Dec 3rd, 2014 Mission Demonstration of 50 kg-Class Deep Space Exploration Micro-Spacecraft Bus System Miniature Ion Thruster and Cold-Gas Thrusters System High-Effieciency GaN SSPA VLBI Navigation Technology Geocorona Observation Close Flyby Observation of Near Earth Asteroid Development The University of Tokyo and JAXA Spacecraft-System Weight 65 kg Size 550 mm×550 mm×670 mm Components Power SAP×4 Attitude RW×4, NSAS×5, FOG×3, STT×1 Communication XTRP (X-Band Transponder), GaN SSPA (Soid State Power Amplifier) VLBITX (Tone Signal Generator for VLBI Navigation) Propulsion Ion Thruster×1 (for Deep Space Maneuver) Cold-Gas Thruster×8 (for Reaction Control System and Trajectory Correction Maneuver) Mission Telescope×2 (for Asteroid Observation and Geocorona Observation) Achievements Demonstration of 50 kg-Class Deep Space Exploration Micro-Spacecraft Bus System Success Miniature Ion Thruster and Cold-Gas Thrusters System Success High-Effieciency GaN SSPA Success VLBI Navigation Technology Success Geocorona Observation Success Address : [email protected] (Ryu FUNASE) CG by Go MIyazaki Geocorona Observation Rikkyo U. PROCYON/LAICA • Neutral hydrogen geo- corona observed by Lyman Alpha Imaging CAmera (LAICA) onboard PROCYON at 15 million km (0.1 AU) from the Earth • 2-D image since 1972 ~400,000 km (Apollo 16) with wide FOV Geocoronal emission (in Rayleigh) on Jan 9, 2015 Apollo 16 [Carruthers et al., 1976] 7 Recent accomplishments HAYABUSA & IKAROS Led by JAXA Lunar & Planetary Exploration Program Group 8 Japan's Contribution to Spaceguard Asteroid missions • Hayabusa Explored a small S-type NEO (25143) Itokawa • Hayabusa2 Will explore a small C-type NEO (162173) Ryugu Observations • Bisei Spaceguard Center • Groundbased telescopes (Subaru etc) • APAON(Asia-Pacific Asteroid Observation Network) 9 Hayabusa changed concept of small NEOs before after Itokawa This is important The structure from the point of spaceguard of Itokawa is 0.535×0.294×0.209 km “Rubble Pile” 10 Hayabusa2-OSIRIS-REx falcon collaborationHayabusa 2 mission in operation hayabusa ISAS/JAXA HAYABUSA2 mission • Launched: 2014, arrival:2018, departure: 2019, return: 2020 • Earth swing-by completed in Dec 2015 on its way for arrival at Ryugu in 2018 NASA OSIRIS-Rex mission • Launch: 2016, arrival:2018, departure: 2021, return: 2023 • Target: BENNU Sample & return is regarded as a high-risk mission and the collaboration including sample-exchange serves as a means for insurance for both science teams. 1/5 11 Mission Scenario of Hayabusa2 Launch Arrival at Ryugu 03 Dec. 2015 03 Dec. 2014 June-July 2018 Sample analysis Earth swing-by Earth Return The spacecraft observes the asteroid, Nov.-Dec. 2020 releases the small rovers and the lander, and executes multiple samplings. 2019 Nov.-Dec. 2019 : Departure Sample will be obtained from the newly created Impactor collides crater New Experiment with the asteroid 12 Future Space Science in JAXA 13 Space Policy Commission under cabinet office intends to guarantee predetermined steady annual budget for space science and exploration to maintain its scientific activities 2010 2020 2030 Strategic Large Missions (300-350M$ class) for X-ray Recovery (2020) JAXA-led flagship science MMX(2024) mission with HIIA or H3 LiteBIRD, Solar-Sail (~2027) vehicle (3 in ten years) SPICA (~2028) Competitively-chosen Hisaki(2013) medium-sized focused ERG (2016) missions (<150M$ class) SLIM(2020) with Epsilon rocket DESTINY(2022) (every 2 year) #5(2024) BepiColombo (ESA, 2018) Missions of opportunity JUICE (ESA, 2022) for foreign agency-led WFIRST(NASA, ~2025) mission ATHENA(ESA, ~2028) (Notional) 14 Strategic L-class missions with HIIA/H3 #4 ESA-Led SPICA FY2028 Large-size #3 #2 Martian Moons Lite BIRD or eXplorer (MMX) Solar Power Sail Trojan asteroids FY2027 Strategic Large Missions FY2024 (300M$ class) for JAXA- led flagship science #1 X-ray astronomy mission with HIIA/H3 FY2020 Recovery mission vehicle (3 in ten years) 15 Competitive M-class AO for M-Class #5 missions with Epsilon soon announced #4 3200 Phaethon flyby (DESTINY) #3 Moon landing (SLIM) FY2022 #2 van Allen belt (ERG) FY2020 #1 Hisaki Competitively-chosen (UV planet) medium-sized focused FY2016 missions (<150M$ class) with Epsilon rocket (every 2 year) FY2013 16 MMX JAXA’s exploration of the two moons of Mars with sample return from Phobos JAXA’s mission to the Martian moons (MMX) will make close-up remote sensing and insitu observations of both moons, and return samples from Phobos. ISAS Minor Body Exploration Strategy Outside the snow line DESTINY+ Primordial asteroids HAYABUSA2 (under study) (Water in hydrated minerals) OSIRIS-Rex (NASA) Comet (water in the form of ice) Jupiter Trojans Dust ejecting bodies (Missing link between (Organic compound comets and asteroids) Transport via dust particles) Martian Moons ( ) Credit: ESA/ATG medialab Fossil of water delivery capsule ROSETTA (ESA) Solar Power Sail (under study) Martian Moons LUCY (NASA, selected) eXploration(MMX) The Rocky Planet Region 18 ISAS Planetary science 2020s SPICA(ESA-led) Lead sample & return Solar-power sail to Jupiter Trojan asteroids (JAXA-led) under assessment Martian Moons JUICE eXplorer(MMX) (ESA -led) (JAXA-led) Asteroid Sample Return BepiColombo Hayabusa, Hayabusa2 MMO(ESA-led) (JAXA-led) SLIM Moon landing (JAXA-led) 19 19 Foreign agency-led Large missions ? #3 Athena (ESA) #2 Jupiter Icy moons JUICE (ESA) FY2028 #1 Bepi-Colombo (ESA) FY2022 Missions of opportunity for foreign agency-led mission FY2018 20 ESA-JAXA SPICA Sensitivity Dramatic improvement Baseline specifications AKARI FIS-FTS Telescope : 2.5 m aperture 10-15 SOFIA cooled <8 K Core wavelength: 17–230 mm 2 - 10-16 Orbit : S-E L2 Halo Orbit Wm 2010's Launcher : JAXA H3 Vehicle Launch Year : 2027–2028 10-17 1hr) / - HERSCHEL σ AKARI IRC 10-18 Spitzer ×100 Improvement 10-19 R=300 ALMA SPICA/SAFARI Limiting Line Flux (5 Flux Line Limiting R=25000 2020's 10-20 JWST/MIRI SPICA R=3000 10 20 100 200 350 1000 Wavelength / µm 21 SPICA’s challenge to reveal the history of our solar system and its analogs Big Questions – When and how does gas evolve from primordial discs into emerging planetary systems? – How do ices and minerals evolve in the planet formation era, as seed for Solar Systems? • SPICA’s approaches – Detailed study of proto-planetary and debris discs in extra-solar systems to shed light on the history of our Solar System – Observations of planets and minor bodies in our own Solar System to characterize the early solar system and its evolution to the current system. 22 SPICA’s challenge to reveal the history of our own Solar System • Characterization of the early solar system: comets – SPICA will make systematic observations of the D/H ratio of comets, the most primitive bodies in the Solar System, and thereby quantify the original water characteristics in the early Solar System. • Evolution of the solar system: trans-Neptunian objects (TNOs) – SPICA will detect hundreds of the trans-Neptunian objects (TNOs), which are expected to bear an unaltered record of the formation and evolution of the outer Solar System, and infer their composition by measuring their sizes and albedos. • Evolution to planets: planetary atmospheres – SPICA will have resolution ten times better than those of previous exploration missions in the mid-infrared, which contains key features of critical molecules, and will reveal detailed composition and structure of planetary atmospheres. 23 ISAS Minor Body Exploration Strategy SPICA (revised) Infrared Astronomy Outer to main-belt asteroids Outside the snow line + Primordial asteroids HAYABUSA2 DESTINY (Water in hydrated minerals) OSIRIS-Rex (under