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A Review of Possible Planetary Atmospheres in the TRAPPIST-1 System
Space Sci Rev (2020) 216:100 https://doi.org/10.1007/s11214-020-00719-1 A Review of Possible Planetary Atmospheres in the TRAPPIST-1 System Martin Turbet1 · Emeline Bolmont1 · Vincent Bourrier1 · Brice-Olivier Demory2 · Jérémy Leconte3 · James Owen4 · Eric T. Wolf5 Received: 14 January 2020 / Accepted: 4 July 2020 / Published online: 23 July 2020 © The Author(s) 2020 Abstract TRAPPIST-1 is a fantastic nearby (∼39.14 light years) planetary system made of at least seven transiting terrestrial-size, terrestrial-mass planets all receiving a moderate amount of irradiation. To date, this is the most observationally favourable system of po- tentially habitable planets known to exist. Since the announcement of the discovery of the TRAPPIST-1 planetary system in 2016, a growing number of techniques and approaches have been used and proposed to characterize its true nature. Here we have compiled a state- of-the-art overview of all the observational and theoretical constraints that have been ob- tained so far using these techniques and approaches. The goal is to get a better understanding of whether or not TRAPPIST-1 planets can have atmospheres, and if so, what they are made of. For this, we surveyed the literature on TRAPPIST-1 about topics as broad as irradiation environment, planet formation and migration, orbital stability, effects of tides and Transit Timing Variations, transit observations, stellar contamination, density measurements, and numerical climate and escape models. Each of these topics adds a brick to our understand- ing of the likely—or on the contrary unlikely—atmospheres of the seven known planets of the system. -
Temperature Control for the Primary Mirror of Subaru Telescope Using the Data from 'Forecast for Mauna Kea Observatories'
Publ. Natl. Astron. Obs. Japan Vol. 7. 25–31 (2003) Temperature Control for the Primary Mirror of Subaru Telescope using the Data from ‘Forecast for Mauna Kea Observatories’ ∗ Akihiko MIYASHITA, Ryusuke OGASAWARA ,GeorgeMACARAYA†, and Noboru ITOH† (Received March 28, 2003) Abstract Based on the successful numerical weather forecasting performed by collaboration between the Mauna Kea Weather Center and Subaru Telescope, we developed a temperature control system for the primary mirror of the Subaru Telescope. Temperature forecast is accurate 80% in 2 degrees. After the start of operation, the temperature of the primary mirror controlled below 1 degree centigrade compared by the ambient night air temperature in over 70% probability. The effect of the temperature control for the improvement of the seeing of Subaru telescope seems to be moderately effective. The median of the seeing size of Subaru Telescope on May 2000 to March 2003 is 0.655 arcsec FWHM. We need further investigation as to whether the improvement is the result of our successful temperature control system of the primary mirror or the effect of the annual variation of seeing itself. Thus, we need a longer period of data for verification of the effectiveness of the temperature control. Key words: Subaru Telescope, Weather forecast, Seeing, Primary mirror, Temperature control. the actual night-time temperature over the entire night. 1. Introduction The predicted temperature by Mauna Kea Weather Center In order to obtain high quality images from optical- is used as a target temperature of the air-conditioning systems. infrared telescope, the heat generated by the instruments and After a preliminary test run of our method, it was found to equipment need to be removed. -
Presentation71.Pdf
The KiboCUBE Programme December 14, 2017 United Nations / South Africa Symposium on Basic Space Technology “Small satellite missions for scientific and technological advancement” Masanobu TSUJI Japan Aerospace Exploration Agency (JAXA) 1 Credit : JAXA/NASA ISS: Japan’s Capabilities and Contributions ISS Kibo (International Space Station) (Japanese Experiment Module) HTV (H-II Transfer Vehicle) ▪ ISS is a huge manned construction located about 400km above the Earth. ▪ 15 countries participate in the ISS program ▪ Japan strives to make concrete international contributions through extensive utilization of Kibo and HTV. H-IIB Credit : JAXA/NASA 2 ISS: Japan’s Capabilities and Contributions Kibo: Japanese Experiment Module Kibo has a unique Exposed Facility (EF) with an Airlock (AL) and a Remote Manipulator System (JEMRMS), and has a high capacity to exchange experimental equipment. Robotic Arm (JEM-Remote Manipulator System) Airlock Credit : JAXA/NASA 3 “Kibo” is Unique! – Exposed Facility Small Satellite Deployment platform using J-SSOD AtIn present,recent years, satellite a growing deployers numberother ofthan universities J-SSOD andthat companiesuse Kibo include around the world have beenthe NanoRacks developing CubeSat the DeployerMicro/Nano (NRCSD)-satellite and (under 100kg, mainlyCyclops CubeSat). (Space Station Integrated Kinetic Launcher for Orbital Payload Systems). Credit : JAXA/NASA J-SSOD#2 NRCSD#1 Cyclops#1 J-SSOD Microsat#1 J-SSOD#1 J-SSOD Upgrade#1 4 Ref: Prof. 2017 Nano/Microsatellite Market Forecast (SpaceWorks Enterprises -
Highlights in Space 2010
International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no. -
Subaru Telescope: Current Instruments and Plans for Near-Future
Subaru Telescope: Current Instruments and Plans for Near-Future Ikuru Iwata (Subaru Telescope, NAOJ) New Development Group Scientist Photo by Enrico Sacchetti Current Subaru Instruments Primary Suprime-Cam FMOS NsOpt HDS NsIR AO188 IRCS CsOpt HiCIAO FOCAS SCExAO Kyoto 3DII CsIR MOIRCS COMICS Optical Instruments • FOCAS: Imaging, Multi-Object Spectroscopy, Polarization • FOV: 6’Φ, 0.10”/pix, R=250 - 7,500 (0.4” slit) • HDS: High-Dispersion Spectrograph • R=100,000 (0.38” slit), 0.14”/pix • Image Slicer: 0.3” x 5 opened in S11B • Suprime-Cam: Wide-Field Imaging • FOV: 34’ x 27’, 0.20”/pix • Kyoto 3D II: Three-Dimensional Spectroscopy • Fabry-Perot: FOV: 1.9‘x1.9’, 0.056”/pix, IFS: FOV: 3.4”x3.4”, 0.094”/pix Infrared Instruments • COMICS: Mid-IR Imaging and Spectroscopy • λ=8 - 25μm, FOV: 42”x32”, 0.13”/pix • FMOS: Near-IR Fiber Multi-Object Spectroscopy • 400 fibers, λ=0.9 - 1.8μm, FOV: 30’Φ, R= 500 & 2,200 • IRCS: Near-IR Imaging and Spectroscopy with AO • λ=0.9-5.5μm, FOV: 21” (20mas/pix), 54” (52mas/pix), R: 100-2,000 (grism), ~20,000 (echelle) • MOIRCS: Near-IR Wide-field Imaging and MOS • λ=0.9-2.5μm, FOV: 4’x7’, 0.12”/pix • AO188 / LGS: Adaptive Optics System with Laser Guide Star • HiCIAO: High-Contrast Coronagraph • λ=0.85-2.5μm, FOV: 20”x10” (DI, PDI), 5”x5” (SDI), 1e-5.5 contrast at r=1” Slide by H. Takami Two Outstanding Features among 8-10m Telescopes 1. Prime Focus 2. Good Image Quality Prime Focus Capability of Wide-Field Imaging and Spectroscopy Suprime-Cam FMOS • Fiber Multi-Object Spectrograph • 400 Fibers over 30’ Φ Field-of-View • 0.9 - 1.8 μm • OH Suppression with Mask Mirror FMOS Slide by N. -
Kibo HANDBOOK
Kibo HANDBOOK September 2007 Japan Aerospace Exploration Agency (JAXA) Human Space Systems and Utilization Program Group Kibo HANDBOOK Contents 1. Background on Development of Kibo ............................................1-1 1.1 Summary ........................................................................................................................... 1-2 1.2 International Space Station (ISS) Program ........................................................................ 1-2 1.2.1 Outline.........................................................................................................................1-2 1.3 Background of Kibo Development...................................................................................... 1-4 2. Kibo Elements...................................................................................2-1 2.1 Kibo Elements.................................................................................................................... 2-2 2.1.1 Pressurized Module (PM)............................................................................................ 2-3 2.1.2 Experiment Logistics Module - Pressurized Section (ELM-PS)................................... 2-4 2.1.3 Exposed Facility (EF) .................................................................................................. 2-5 2.1.4 Experiment Logistics Module - Exposed Section (ELM-ES)........................................ 2-6 2.1.5 JEM Remote Manipulator System (JEMRMS)............................................................ -
Securing Japan an Assessment of Japan´S Strategy for Space
Full Report Securing Japan An assessment of Japan´s strategy for space Report: Title: “ESPI Report 74 - Securing Japan - Full Report” Published: July 2020 ISSN: 2218-0931 (print) • 2076-6688 (online) Editor and publisher: European Space Policy Institute (ESPI) Schwarzenbergplatz 6 • 1030 Vienna • Austria Phone: +43 1 718 11 18 -0 E-Mail: [email protected] Website: www.espi.or.at Rights reserved - No part of this report may be reproduced or transmitted in any form or for any purpose without permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “ESPI Report 74 - Securing Japan - Full Report, July 2020. All rights reserved” and sample transmission to ESPI before publishing. ESPI is not responsible for any losses, injury or damage caused to any person or property (including under contract, by negligence, product liability or otherwise) whether they may be direct or indirect, special, incidental or consequential, resulting from the information contained in this publication. Design: copylot.at Cover page picture credit: European Space Agency (ESA) TABLE OF CONTENT 1 INTRODUCTION ............................................................................................................................. 1 1.1 Background and rationales ............................................................................................................. 1 1.2 Objectives of the Study ................................................................................................................... 2 1.3 Methodology -
The MAXI Mission on the ISS: Science and Instruments for Monitoring All
PASJ: Publ. Astron. Soc. Japan , 1–??, c 2018. Astronomical Society of Japan. The MAXI Mission on the ISS: Science and Instruments for Monitoring All Sky X-Ray Images Masaru Matsuoka, 1 Kazuyoshi Kawasaki, 1 Shiro Ueno, 1 Hiroshi Tomida, 1 Mitsuhiro Kohama, 1,2 Motoko Suzuki, 1 Yasuki Adachi, 1 Masaki Ishikawa, 1 Tatehiro Mihara, 2 Mutsumi Sugizaki, 2 Naoki Isobe, 2 Yujin Nakagawa, 2 Hiroshi Tsunemi, 3 Emi Miyata, 3 Nobuyuki Kawai, 4 Jun Kataoka, 4∗ Mikio Morii, 4 Atsumasa Yoshida, 5 Hitoshi Negoro, 6 Motoki Nakajima, 6 Yoshihiro Ueda, 7 Hirotaka Chujo, 2 Kazutaka Yamaoka, 5 Osamu Yamazaki, 5 Satoshi Nakahira, 5 Tetsuya You, 5 Ryoji Ishiwata, 6 Sho Miyoshi, 6 Satoshi Eguchi, 7 Kazuo Hiroi, 7 Haruyoshi Katayama, 8 and Ken Ebisawa, 9 1ISS Science Project Office, ISAS, JAXA, 2-1-1 Sengen, Tsukuba, Ibaraki 305-8505 (MM) [email protected] 2Cosmic Radiation Laboratory, RIKEN, 2-1 Hirosawa, Wako, Saitama 351–198 3Department of Earth and Space Science, Osaka University , 1-1 Machikaneyama, Toyonaka, Osaka 560-0043 4Department of Physics, Tokyo Institute of Technology, 2-12-1 Ookayama, Meguro-ku, Tokyo 152-8551 5Department of Physics and Mathematics, Aoyama Gakuin University, 5-10-1 Fuchinobe, Sagamihara, Kanagawa 229-8558 6Department of Physics, Nihon University, 1-8-14, Kanda-Surugadai, Chiyoda-ku, Tokyo 101-8308 7Department of Astronomy, Kyoto University, Oiwake-cho, Sakyo-ku, Kyoto 606-8502 8Earth Observation Research Center, JAXA, 2-1-1 Sengen, Tsukuba, Ibaraki 305-8505 9ISAS, JAXA, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 229-8510 (Received 2009 March 9; accepted 2009 May 28) Abstract The Monitor of All Sky X-ray Image (MAXI) mission is the first astronomical payload to be installed on the Japanese Experiment Module - Exposed Facility (JEM-EF or Kibo-EF) on the International Space Station (ISS). -
Japan's Technical Prowess International Cooperation
Japan Aerospace Exploration Agency April 2016 No. 10 Special Features Japan’s Technical Prowess Technical excellence and team spirit are manifested in such activities as the space station capture of the HTV5 spacecraft, development of the H3 Launch Vehicle, and reduction of sonic boom in supersonic transport International Cooperation JAXA plays a central role in international society and contributes through diverse joint programs, including planetary exploration, and the utilization of Earth observation satellites in the environmental and disaster management fields Japan’s Technical Prowess Contents No. 10 Japan Aerospace Exploration Agency Special Feature 1: Japan’s Technical Prowess 1−3 Welcome to JAXA TODAY Activities of “Team Japan” Connecting the Earth and Space The Japan Aerospace Exploration Agency (JAXA) is positioned as We review some of the activities of “Team the pivotal organization supporting the Japanese government’s Japan,” including the successful capture of H-II Transfer Vehicle 5 (HTV5), which brought overall space development and utilization program with world- together JAXA, NASA and the International Space Station (ISS). leading technology. JAXA undertakes a full spectrum of activities, from basic research through development and utilization. 4–7 In 2013, to coincide with the 10th anniversary of its estab- 2020: The H3 Launch Vehicle Vision JAXA is currently pursuing the development lishment, JAXA defined its management philosophy as “utilizing of the H3 Launch Vehicle, which is expected space and the sky to achieve a safe and affluent society” and to become the backbone of Japan’s space development program and build strong adopted the new corporate slogan “Explore to Realize.” Under- international competitiveness. -
External Multipurpose Facilities
External Multipurpose Facilities This section gives an overview of existing External Facilities that are mul- tidisciplinary in nature, providing access to multiple sites that are exposed to the space environment and which include structural attachment points and utility interface. Exposed Experiment Handrail Attachment Mechanism (ExHAM) [JAXA] enables space investigations in an exposed environment by provid- ing attachment onto the JEM Kibo’s Exposed Facility, taking advantage of Kibo’s unique function having both airlock and robotic arm among mod- ules on the ISS. ExHAM is a cuboid mechanism equipped with a grapple fixture for the Kibo’s robotic arm, JEM Remote Manipulator System (JEMRMS) Small Fine Arm (SFA). The number of loadable investigation samples is 7 on the upper surface and 13 on the side surfaces. External Multipurpose Facilities View of the JEM Exposed Facility. The Hyperspectral Imager for the Coastal Ocean (HICO)/Remote Atmospheric and Ionospheric Detection System (RAIDS) Experiment Payload (HREP), NanoRacks External Platform (NREP), ExHAM, and Space Environment Data Acquisition equipment - Attached Payload (SEDA-AP) are in view. (ISS048E057068). 36 37 Expedite the Processing of Experiments to the Space Station Columbus-External Payload Facility (Columbus-EPF) [ESA] provides (EXPRESS) Logistics Carrier (ELC) [NASA] is a pallet designed to sup- 4 powered external attachment site locations for scientific payloads or port external research hardware and store external spares (called Orbital facilities, and has to date been used by ESA and NASA. Each of the 4 Replacement Units) needed over the life of the ISS. Currently, 4 ELCs attachment sites may hold a mass of up to 290 kg, and are provided utility are mounted to ISS trusses, providing unique vantage points for space, connections for power and data. -
JAXA's Examples of International Mechanisms for Cooperation in The
JAXA’s examples of International Mechanisms for Cooperation in the Peaceful Exploration and Use of Outer Space Japan Aerospace Exploration Agency (JAXA) UNCOPUOS, Legal Subcommittee 54 th Session Vienna, 20 April 2015 Contents 1. “Hayabusa2” Project 2. Sentinel Asia 3. Cooperation on the high-quality protein crystal growth experiment on board the Japanese Experiment Module “KIBO” 4. Cooperative project between JAXA and the Asian Development Bank (ADB) 1 1. “Hayabusa2” Project 2 2 Mission Outline Asteroid (1999JU3) Arrival Earth Swing-by June. 2018 Dec. 2015 impactor Launch •asteroid remote sensing release Dec, 2014 •small rovers and lander release crater •multiple samplings forming Departure Earth Return Dec. 2019 Dec. 2020 sampling from artificial crater 3 3 JAXA-NASA Cooperation • NASA provides support for Hayabusa2 including the NASA Deep Space Network which enables advanced and reliable mission operations. • Asteroid sample exchange and joint participation during key mission phases with NASA’ s asteroid explorer OSIRIS-REx , JAXA and NASA will mutually maximize their missions’ results. 4 4 Japan-US Cooperative Framework Hayabusa-2 Cooperation Exchange of Exchange of Notes (E/N) Notes (E/N) Government of Cross-Waiver concerning the for revision of Agreement US - Japan cooperation Annex of (1995) on Hayabusa2 Cross-Waiver Project Agreement Annex MOU for Cooperation on NASA – JAXA the Hayabusa2 Mission and the OSIRIS-REx Mission Diet Approval Treaty Administrative Arrangement Implementing Arrangement 5 Characteristics • In the case of long-term projects with huge costs and unpredictable R&D risks, there may be some risks of cancelation of project, owing to domestic political change, budgetary problems, technical difficulties, and so on. -
The Mauna Kea Observatories Near-Infrared Filter Set. II. Specifications for a New JHKL!
Publications of the Astronomical Society of the Pacific, 114:180–186, 2002 February ᭧ 2002. The Astronomical Society of the Pacific. All rights reserved. Printed in U.S.A. The Mauna Kea Observatories Near-Infrared Filter Set. II. Specifications for a New JHKLЈMЈ Filter Set for Infrared Astronomy A. T. Tokunaga Institute for Astronomy, University of Hawaii, 2680 Woodlawn Drive, Honolulu, HI 96822; [email protected] D. A. Simons Gemini Observatory, Northern Operations Center, 670 North A‘ohoku Place, Hilo, HI 96720; [email protected] and W. D. Vacca Max-Planck-Institut fu¨r extraterrestrische Physik, Postfach 1312, D-85741 Garching, Germany; [email protected] Received 2001 July 28; accepted 2001 October 17 ABSTRACT. We present a description of a new 1–5 mm filter set similar to the long-used JHKLM filter set derived from that of Johnson. The new Mauna Kea Observatories Near-Infrared filter set is designed to reduce background noise, improve photometric transformations from observatory to observatory, provide greater accuracy in extrapolating to zero air mass, and reduce the color dependence in the extinction coefficient in photometric reductions. We have also taken into account the requirements of adaptive optics in setting the flatness specification of the filters. A complete technical description is presented to facilitate the production of similar filters in the future. 1. INTRODUCTION baru Telescopes, all of the optical/infrared observatories at Mauna Kea are currently using these filters (NASA Infrared The rationale for a new set of infrared filters was presented Telescope Facility, United Kingdom Infrared Telescope, Canada- by Simons & Tokunaga (2002, hereafter Paper I).