Tianwen-1: China's Mars Mission
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INPE) MCTI Çp ' Acordo Operação Técnica COPERNICUS Entre ESA,AEB E INPE (0026237) SEI 01350.001611/2018-03 / Pg
ORIGINAL N° 1 Copernicus Space Component Technical Operating Arrangement ESA - Brazilian Space Agency and INPE (INPE) MCTI çp ' Acordo Operação Técnica COPERNICUS entre ESA,AEB E INPE (0026237) SEI 01350.001611/2018-03 / pg. 1 Table of Contents 1 INTRODUCTION....................................................................................... 4 1.1 Background....................................................................................................................... 4 1.2 Purpose and objectives ..................................................................................................... 4 1.3 Scope................................................................................................................................. 6 1.4 References......................................................................................................................... 6 2 EUROPEAN ACCESS TO BRAZILIAN EO MISSIONS AND CALIBRATION DATA AND PARTNER IN-SITU DATA ............................................................. 7 3 ARRANGEMENT OF TECHNICAL INTERFACES ....................................... 8 3.1 Technical Arrangement Types.......................................................................................... 8 4 INTERNATIONALARCHIVING AND DISSEMINATION CENTRES, MIRRORSITE ................................................................................................ 9 4.1 Invohred Entities............................................................................................................... 9 4.2 INPE Activity -
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. -
Mars 2020 Radiological Contingency Planning
National Aeronautics and Space Administration Mars 2020 Radiological Contingency Planning NASA plans to launch the Mars 2020 rover, produce the rover’s onboard power and to Perseverance, in summer 2020 on a mission warm its internal systems during the frigid to seek signs of habitable conditions in Mars’ Martian night. ancient past and search for signs of past microbial life. The mission will lift off from Cape NASA prepares contingency response plans Canaveral Air Force Station in Florida aboard a for every launch that it conducts. Ensuring the United Launch Alliance Atlas V launch vehicle safety of launch-site workers and the public in between mid-July and August 2020. the communities surrounding the launch area is the primary consideration in this planning. The Mars 2020 rover design is based on NASA’s Curiosity rover, which landed on Mars in 2012 This contingency planning task takes on an and greatly increased our knowledge of the added dimension when the payload being Red Planet. The Mars 2020 rover is equipped launched into space contains nuclear material. to study its landing site in detail and collect and The primary goal of radiological contingency store the most promising samples of rock and planning is to enable an efficient response in soil on the surface of Mars. the event of an accident. This planning is based on the fundamental principles of advance The system that provides electrical power for preparation (including rehearsals of simulated Mars 2020 and its scientific equipment is the launch accident responses), the timely availability same as for the Curiosity rover: a Multi- of technically accurate and reliable information, Mission Radioisotope Thermoelectric Generator and prompt external communication with the (MMRTG). -
Mars Helicopter/Ingenuity
National Aeronautics and Space Administration Mars Helicopter/Ingenuity When NASA’s Perseverance rover lands on February 18, 2021, it will be carrying a passenger onboard: the first helicopter ever designed to fly in the thin Martian air. The Mars Helicopter, Ingenuity, is a small, or as full standalone science craft carrying autonomous aircraft that will be carried to instrument payloads. Taking to the air would the surface of the Red Planet attached to the give scientists a new perspective on a region’s belly of the Perseverance rover. Its mission geology and even allow them to peer into is experimental in nature and completely areas that are too steep or slippery to send independent of the rover’s science mission. a rover. In the distant future, they might even In the months after landing, the helicopter help astronauts explore Mars. will be placed on the surface to test – for the first time ever – powered flight in the thin The project is solely a demonstration of Martian air. Its performance during these technology; it is not designed to support the experimental test flights will help inform Mars 2020/Perseverance mission, which decisions relating to considering small is searching for signs of ancient life and helicopters for future Mars missions, where collecting samples of rock and sediment in they could perform in a support role as tubes for potential return to Earth by later robotic scouts, surveying terrain from above, missions. This illustration shows the Mars Helicopter Ingenuity on the surface of Mars. Key Objectives Key Features • Prove powered flight in the thin atmosphere of • Weighs 4 pounds (1.8 kg) Mars. -
Build Your Own Mars Helicopter
Aeronautics Research Mission Directorate Build Your Own Mars Helicopter Suggested Grades: 3-8 Activity Overview Time: 30 minutes NASA is sending a helicopter to Mars! This helicopter Materials is called Ingenuity and is designed to test whether or not • 1 Large marshmallow flight is a good way to study distant bodies in space. • 4 Small marshmallows • 5 Toothpicks We have sent spacecraft to other planets, but this is the • Cardstock (to print out the last first aircraft that will fly on another world. In this page of this document) activity, you will learn about this amazing feat of engineering as you build your own Mars helicopter • Scissors model. Steps 1. The large marshmallow will represent Ingenuity’s fuselage. Ingenuity is fairly small, about 19 inches tall and weighing about 4 pounds, and the fuselage is about the size of a softball. The fuselage contains batteries, sensors, and cameras to power and control Ingenuity’s flight. It is insulated and has heaters to protect the equipment in the cold Martian environment where it can reach -130 oC at night. 2. Insert the four toothpicks into the marshmallow so they come out at angles as shown in Figure 1. The toothpicks represent the four hollow carbon-fiber legs on Ingenuity. Ingenuity’s legs are designed to be lightweight while still supporting the helicopter when it’s on the Martian surface. To take up less space, Ingenuity’s legs are folded while it’s being carried to Mars. / Figure 1. Insert the four toothpicks into the marshmallow to represent Ingenuity's legs. 3. -
Exploration of Mars by the European Space Agency 1
Exploration of Mars by the European Space Agency Alejandro Cardesín ESA Science Operations Mars Express, ExoMars 2016 IAC Winter School, November 20161 Credit: MEX/HRSC History of Missions to Mars Mars Exploration nowadays… 2000‐2010 2011 2013/14 2016 2018 2020 future … Mars Express MAVEN (ESA) TGO Future ESA (ESA- Studies… RUSSIA) Odyssey MRO Mars Phobos- Sample Grunt Return? (RUSSIA) MOM Schiaparelli ExoMars 2020 Phoenix (ESA-RUSSIA) Opportunity MSL Curiosity Mars Insight 2020 Spirit The data/information contained herein has been reviewed and approved for release by JPL Export Administration on the basis that this document contains no export‐controlled information. Mars Express 2003-2016 … First European Mission to orbit another Planet! First mission of the “Rosetta family” Up and running since 2003 Credit: MEX/HRSC First European Mission to orbit another Planet First European attempt to land on another Planet Original mission concept Credit: MEX/HRSC December 2003: Mars Express Lander Release and Orbit Insertion Collission trajectory Bye bye Beagle 2! Last picture Lander after release, release taken by VMC camera Insertion 19/12/2003 8:33 trajectory Credit: MEX/HRSC Beagle 2 was found in January 2015 ! Only 6km away from landing site OK Open petals indicate soft landing OK Antenna remained covered Lessons learned: comms at all time! Credit: MEX/HRSC Mars Express: so many missions at once Mars Mission Phobos Mission Relay Mission Credit: MEX/HRSC Mars Express science investigations Martian Moons: Phobos & Deimos: Ionosphere, surface, -
JAXA's Space Exploration Activities
JAXA’s Space Exploration Activities Jun Gomi, Deputy Director General, JAXA Hayabusa 2 ✓ Asteroid Explorer of the C-type asteroid ✓ Launched in December, 2014 ✓ Reached target asteroid “Ryugu” in 2018 ✓ First successful touchdown to Ryugu on February 22, 2019 ✓ Return to Earth in 2020 (162173) Ryugu 2 Hayabusa 2 (c) JAXA, University of Tokyo, Kochi University, Rikkyo University, (c) JAXA, University of Tokyo, Kochi University, Rikkyo University, Nagoya University, Chiba Institute of Technology, Meiji University, Nagoya University, Chiba Institute of Technology, Meiji University, University of Aizu and AIST. University of Aizu, AIST Asteroid Ryugu photographed from a Asteroid Ryugu from an altitude of 6km. distance of about 20 km. The image Image was captured with the Optical was taken on June 30, 2018. Navigation Camera on July 20, 2018. Hayabusa 2 4 JAXA’s Plan for Space Exploration International • Utilization of ISS/Kibo • Cis-Lunar Platform (Gateway) Cooperation • Lunar exploration and beyond Industry & • JAXA Space Exploration Innovation Academia Hub Partnerships • Science Community discussions JAXA’s Overall Scenario for International Space Exploration Mars, others ★ Initial Exploration ★ Full Fledge Exploration MMX: JFY2024 • Science and search for life • Utilization feasibility exam. Kaguya Moon ©JAXA ©JAXA ©JAXA ©JAXA ©JAXA Full-fledged Exploration & SLIM Traversing exploration(2023- ) Sample Return(2026- ) Utilization (JFY2021) • Science exploration • S/R from far side • Cooperative science/resource • Water prospecting • Technology demo for human mission exploration by robotic and human HTV-X der.(2026- ) • Small probe deploy, data relay etc. Gateway Phase 1 Gateway (2022-) Phase 2 • Support for Lunar science Earth • Science using deep space Promote Commercialization International Space Station 6 SLIM (Smart Lander for Investigating Moon) ✓ Demonstrate pin-point landing on the moon. -
Concept for a Crewed Lunar Lander Operating from the Lunar Orbiting Platform-Gateway
69th International Astronautical Congress (IAC), Bremen, Germany, 1-5 October 2018. Copyright © 2018 by Lockheed Martin Corporation. Published by the IAF, with permission and released to the IAF to publish in all forms. IAC-18.A5.1.4x46653 Concept for a Crewed Lunar Lander Operating from the Lunar Orbiting Platform-Gateway Timothy Cichana*, Stephen A. Baileyb, Adam Burchc, Nickolas W. Kirbyd aSpace Exploration Architect, P.O. Box 179, MS H3005, Lockheed Martin Space, Denver, Colorado, U.S.A. 80201, [email protected] bPresident, 8100 Shaffer Parkway, Unit 130, Deep Space Systems, Inc., Littleton, Colorado, 80127-4124, [email protected] cDesign Engineer / Graphic Artist, 8341 Sangre de Christo Rd, Deep Space Systems, Inc., Littleton, Colorado, 80127, [email protected] dSystems Engineer, Advanced Programs, P.O. Box 179, MS H3005, Lockheed Martin Space, Denver, Colorado, U.S.A. 80201, [email protected] * Corresponding Author Abstract Lockheed Martin is working with NASA on the development of the Lunar Orbiting Platform – Gateway, or Gateway. Positioned in the vicinity of the Moon, the Gateway allows astronauts to demonstrate operations beyond Low Earth Orbit for months at a time. The Gateway is evolvable, flexible, modular, and is a precursor and mission demonstrator directly on the path to Mars. Mars Base Camp is Lockheed Martin's vision for sending humans to Mars. Operations from an orbital base camp will build on a strong foundation of today's technologies and emphasize scientific exploration as mission cornerstones. Key aspects of Mars Base Camp include utilizing liquid oxygen and hydrogen as the basis for a nascent water-based economy and the development of a reusable lander/ascent vehicle. -
European Astronaut Selection ESA Prepares for the Missions of the 21 St Century
European Astronaut Selection ESA prepares for the missions of the 21 st century With the selection of its first astronauts ESA’s human spaceflight activities in 1978 and the first Spacelab mission are now entering a new era, with ESA in 1983, the European Space Agency astronauts working aboard the (ESA) took its first steps into human International Space Station (ISS), spaceflight. The advent of the Columbus Columbus starting operations, and orbital laboratory project required a the new ‘ATV’ cargo ship delivering second selection of astronauts in 1992. fresh supplies to the Station. The exploration of the Solar System will be one of humanity’s most exciting adventures in the near future. All of the world’s spacefaring nations are preparing for this huge enterprise, and an astronaut corps is essential for Europe, thanks to ESA, to take part in this endeavour. Now is the time for ESA to seek new talents to reinforce its astronaut team, to prepare for missions to the ISS, the Moon and beyond. T The Selection | How? When? Where? h e S e l e c t i o n How can I apply? You can apply online via the ESA web portal (www.esa.int/ astronautselection). Registration is in two steps: • pre-registration: provide identity information and a JAR-FCL 3, Class 2 medi- cal examination certificate, from an Aviation Medical Examiner who has been certified by his/her national Aviation Medical Authority; • a password then allows you to access the application form. T The Selection | How? When? Where? h e S e l e • initial selection according to basic criteria; c t i What are the o • psychological tests for selected candidates; n • second round of psychological tests and interviews; steps in the • medical tests; selection • job interview. -
Determination of Optimal Earth-Mars Trajectories to Target the Moons Of
The Pennsylvania State University The Graduate School Department of Aerospace Engineering DETERMINATION OF OPTIMAL EARTH-MARS TRAJECTORIES TO TARGET THE MOONS OF MARS A Thesis in Aerospace Engineering by Davide Conte 2014 Davide Conte Submitted in Partial Fulfillment of the Requirements for the Degree of Master of Science May 2014 ii The thesis of Davide Conte was reviewed and approved* by the following: David B. Spencer Professor of Aerospace Engineering Thesis Advisor Robert G. Melton Professor of Aerospace Engineering Director of Undergraduate Studies George A. Lesieutre Professor of Aerospace Engineering Head of the Department of Aerospace Engineering *Signatures are on file in the Graduate School iii ABSTRACT The focus of this thesis is to analyze interplanetary transfer maneuvers from Earth to Mars in order to target the Martian moons, Phobos and Deimos. Such analysis is done by solving Lambert’s Problem and investigating the necessary targeting upon Mars arrival. Additionally, the orbital parameters of the arrival trajectory as well as the relative required ΔVs and times of flights were determined in order to define the optimal departure and arrival windows for a given range of date. The first step in solving Lambert’s Problem consists in finding the positions and velocities of the departure (Earth) and arrival (Mars) planets for a given range of dates. Then, by solving Lambert’s problem for various combinations of departure and arrival dates, porkchop plots can be created and examined. Some of the key parameters that are plotted on porkchop plots and used to investigate possible transfer orbits are the departure characteristic energy, C3, and the arrival v∞. -
First Galileo Satellites Galileo In-Orbit Validation Element
BR-251cover 7/8/06 13:28 Page 1 BR-251 Galileo Joint Undertaking Rue du Luxembourg 3 B-1000 Brussels, Belgium Tel: +32 2 507 80 00 The First Fax: +32 2 507 80 01 Email: [email protected] http://www.galileoju.com European Space Agency Directorate of European Union and Industrial Programmes Galileo Satellites 8-10 rue Mario Nikis F-75738 Paris Cedex 15, France Tel: +33 1 53 69 77 26 Fax: +33 1 53 69 72 86 Email: [email protected] http://www.esa.int/navigation/ European Commission Galileo In-Orbit Validation Element Directorate General for Energy and Transport Unit E.4 Satellite Navigation System (Galileo), Intelligent Transport, DM28 1/64 B-1049 Brussels, Belgium GIOVE Tel: +32 2 29 56040 Fax: +32 2 296 5372 Email: [email protected] http://europa.eu.int/comm/dgs/energy_transport/galileo/ BR-251cover 7/8/06 13:28 Page 2 BR-251 (2nd imprint, August 2006) Published by: ESA Publications Division ESTEC, PO Box 299 2200 AG Noordwijk The Netherlands Editor: Andrew Wilson Design/Layout: Eva Ekstrand Text coordination: Dominique Detain Copyright: ©2006 European Space Agency ISSN: 0250-1589 ISBN: 92-9092-497-7 Photo/image credits: Royal Astronomical Society Library (p.18), C. Beetles/Bridgeman-Giraudon (p.18), Galileo Price: 10 Euros Industries (pp. 7, 11); ESA: P.Carril (front cover, pp. 4, 5, 6, 7), S. Corvaja (front cover, pp. 6, 12), D. Detain (p. 13), J. Huart (pp. 3, 8, 9), A. Le Floch (pp. 4, 10, 16), E. Pedoussaut (p. 13), P.Sebirot (front cover),Trimaran (p. -
Human Exploration of Mars Design Reference Architecture 5.0
July 2009 “We are all . children of this universe. Not just Earth, or Mars, or this System, but the whole grand fireworks. And if we are interested in Mars at all, it is only because we wonder over our past and worry terribly about our possible future.” — Ray Bradbury, 'Mars and the Mind of Man,' 1973 Cover Art: An artist’s concept depicting one of many potential Mars exploration strategies. In this approach, the strengths of combining a central habitat with small pressurized rovers that could extend the exploration range of the crew from the outpost are assessed. Rawlings 2007. NASA/SP–2009–566 Human Exploration of Mars Design Reference Architecture 5.0 Mars Architecture Steering Group NASA Headquarters Bret G. Drake, editor NASA Johnson Space Center, Houston, Texas July 2009 ACKNOWLEDGEMENTS The individuals listed in the appendix assisted in the generation of the concepts as well as the descriptions, images, and data described in this report. Specific contributions to this document were provided by Dave Beaty, Stan Borowski, Bob Cataldo, John Charles, Cassie Conley, Doug Craig, Bret Drake, John Elliot, Chad Edwards, Walt Engelund, Dean Eppler, Stewart Feldman, Jim Garvin, Steve Hoffman, Jeff Jones, Frank Jordan, Sheri Klug, Joel Levine, Jack Mulqueen, Gary Noreen, Hoppy Price, Shawn Quinn, Jerry Sanders, Jim Schier, Lisa Simonsen, George Tahu, and Abhi Tripathi. Available from: NASA Center for AeroSpace Information National Technical Information Service 7115 Standard Drive 5285 Port Royal Road Hanover, MD 21076-1320 Springfield, VA 22161 Phone: 301-621-0390 or 703-605-6000 Fax: 301-621-0134 This report is also available in electronic form at http://ston.jsc.nasa.gov/collections/TRS/ CONTENTS 1 Introduction ......................................................................................................................