Trajectory Optimization for First Human Asteroid Exploration Mission
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A Self Reconfigurable Undulating Grasper for Asteroid Mining
A SELF RECONFIGURABLE UNDULATING GRASPER FOR ASTEROID MINING Suzanna Lucarotti1, Chakravarthini M Saaj1, Elie Allouis2 and Paolo Bianco3 1Surrey Space Centre, Guildford UK 2Airbus DS, Stevenage UK 3Airbus, Portsmouth UK ABSTRACT are estimated as over 1km diameter and 4133 as 300- 1000m diameter. While surface features remain mostly unknown, mass and orbit parameters are available. The Recent missions to asteroids have shown that many have closest NEAs can be reached with less ∆V than the rubble surfaces, which current extra-terrestrial mining Moon. techniques are unsuited for. This paper discusses mod- elling work for autonomous mining on small solar system There have been so far been five missions to the sur- bodies, such as Asteroids. A novel concept of a modular face of SSSBs - NEAR-Shoemaker to Eros, where they robot system capable of the helical caging and grasping unexpectedly landed [9], Hayabusa 1 to Itokawa [10], of surface rocks is presented. The kinematics and co- Rosetta to the Comet 67P Churyumov-Gerasimenko [11], ordinate systems of the Self RecoNfigurable Undulating Hayabusa 2 to Ryugu [12], and OSIRIS-Rex to Bennu Grasper (SNUG) are derived with a new mathematical [13]. Hayabusa 2 and OSIRUS-Rex are both currently formulation. This approach exploits rotational symmetry live missions. Detailed close-range surface images have and homogeneity to form a cage to safely grasp a target of been obtained from Itokawa, 67P and Ryugu, higher alti- uncertain properties. A simple model for grasping is eval- tude images from low orbit or prior to landing have been uated to assess the grasping capabilities of such a robot. -
Chapter 1, Version A
INCLUSIVE EDUCATION AND SCHOOL REFORM IN POSTCOLONIAL INDIA Mousumi Mukherjee MA, MPhil, Calcutta University; MA Loyola University Chicago; EdM University of Illinois, Urbana-Champaign Submitted in total fulfilment of the requirements for the degree of Doctor of Philosophy Education Policy and Leadership Melbourne Graduate School of Education University of Melbourne [5 June 2015] Keywords Inclusive Education, Equity, Democratic School Reform, Girls’ Education, Missionary Education, Postcolonial theory, Globalization, Development Inclusive Education and School Reform in Postcolonial India i Abstract Over the past two decades, a converging discourse has emerged around the world concerning the importance of socially inclusive education. In India, the idea of inclusive education is not new, and is consistent with the key principles underpinning the Indian constitution. It has been promoted by a number of educational thinkers of modern India such as Vivekananda, Aurobindo, Gandhi, Ambedkar, Azad and Tagore. However, the idea of inclusive education has been unevenly and inadequately implemented in Indian schools, which have remained largely socially segregated. There are of course major exceptions, with some schools valiantly seeking to realize social inclusion. One such school is in Kolkata, which has been nationally and globally celebrated as an example of best practice. The main aim of this thesis is to examine the initiative of inclusive educational reform that this school represents. It analyses the school’s understanding of inclusive education; provides an account of how the school promoted its achievements, not only within its own community but also around the world; and critically assesses the extent to which the initiatives are sustainable in the long term. -
Argops) Solution to the 2017 Astrodynamics Specialist Conference Student Competition
AAS 17-621 THE ASTRODYNAMICS RESEARCH GROUP OF PENN STATE (ARGOPS) SOLUTION TO THE 2017 ASTRODYNAMICS SPECIALIST CONFERENCE STUDENT COMPETITION Jason A. Reiter,* Davide Conte,1 Andrew M. Goodyear,* Ghanghoon Paik,* Guanwei. He,* Peter C. Scarcella,* Mollik Nayyar,* Matthew J. Shaw* We present the methods and results of the Astrodynamics Research Group of Penn State (ARGoPS) team in the 2017 Astrodynamics Specialist Conference Student Competition. A mission (named Minerva) was designed to investigate Asteroid (469219) 2016 HO3 in order to determine its mass and volume and to map and characterize its surface. This data would prove useful in determining the necessity and usefulness of future missions to the asteroid. The mission was designed such that a balance between cost and maximizing objectives was found. INTRODUCTION Asteroid (469219) 2016 HO3 was discovered recently and has yet to be explored. It lies in a quasi-orbit about the Earth such that it will follow the Earth around the Sun for at least the next several hundred years providing many opportunities for relatively low-cost missions to the body. Not much is known about 2016 HO3 except a general size range, but its close proximity to Earth makes a scientific mission more feasible than other near-Earth objects. A Request For Proposal (RFP) was provided to university teams searching for cost-efficient mission design solutions to assist in the characterization of the asteroid and the assessment of its potential for future, more in-depth missions and possible resource utilization. The RFP provides constraints on launch mass, bus size as well as other mission architecture decisions, and sets goals for scientific mapping and characterization. -
“Target Selection for a HAIV Flight Demo Mission,” IAA-PDC13-04
Planetary Defense Conference 2013 IAA-PDC13-04-08 Target Selection for a Hypervelocity Asteroid Intercept Vehicle Flight Validation Mission Sam Wagnera,1,∗, Bong Wieb,2, Brent W. Barbeec,3 aIowa State University, 2271 Howe Hall, Room 2348, Ames, IA 50011-2271, USA bIowa State University, 2271 Howe Hall, Room 2325, Ames, IA 50011-2271, USA cNASA/GSFC, Code 595, 8800 Greenbelt Road, Greenbelt, MD, 20771, USA, 301.286.1837 Abstract Asteroids and comets have collided with the Earth in the past and will do so again in the future. Throughout Earth’s history these collisions have played a significant role in shaping Earth’s biological and geological histories. The planetary defense community has been examining a variety of options for mitigating the impact threat of asteroids and comets that approach or cross Earth’s orbit, known as near-Earth objects (NEOs). This paper discusses the preliminary study results of selecting small (100-m class) NEO targets and mission design trade-offs for flight validating some key planetary defense technologies. In particular, this paper focuses on a planetary defense demo mission for validating the effectiveness of a Hypervelocity Asteroid Intercept Vehicle (HAIV) concept, currently being investigated by the Asteroid Deflection Research Center (ADRC) for a NIAC (NASA Advanced Innovative Concepts) Phase 2 project. Introduction Geological evidence shows that asteroids and comets have collided with the Earth in the past and will do so in the future. Such collisions have played an important role in shaping the Earth’s biological and geological histories. Many researchers in the planetary defense community have examined a variety of options for mitigating the impact threat of Earth approaching or crossing asteroids and comets, known as near-Earth objects (NEOs). -
Small in Size Only
editorial Small in size only Planets and their systems have long held the spotlight, but researchers, space agencies and even the private sector and the public have turned their attention to small bodies. stronomy in 2019 started with a collaboration), a spacecraft that will lurk at System, compositionally, structurally bang: the flyby of the farthest body a Lagrange point until a special target — a and dynamically. Aever visited by a human artefact. The pristine comet, or maybe an interstellar Beyond science, the community is also close approach of the New Horizons probe object — will pass by. The probe will then motivated by planetary defence, for which to the recently named Arrokoth, a contact be ready to approach it and perform close we need to characterize near-Earth asteroids binary Kuiper belt object, allowed scientists observations. Other agencies are also active: in order to understand what can be done to to look for the first time at a pristine body, JAXA has laid down a full small-bodies avert a catastrophic impact on our planet. probably undisturbed for the past 4 billion programme (see the Comment by Masaki Both NASA and ESA are stepping up their years or so. Fujimoto and Elizabeth Tasker) and China efforts, which translates into the approval We are living in a golden age for small announced plans to launch in 2022 an of new missions. Two spacecraft that had bodies, as various space exploration events ambitious mission involving flybys of an been previously rejected got approved this of 2019 clearly show. A major theme of the asteroid and a comet, with sample return year. -
Strategic Investments in Instrumentation and Facilities for Extraterrestrial Sample Curation and Analysis
PREPUBLICATION COPY—SUBJECT TO FURTHER EDITORIAL CORRECTION Strategic Investments in Instrumentation and Facilities for Extraterrestrial Sample Curation and Analysis ADVANCE COPY NOT FOR PUBLIC RELEASE BEFORE Thursday, December 20, 2018 at 11:00 a.m. ___________________________________________________________________________________ PLEASE CITE AS A REPORT OF THE NATIONAL ACADEMIES OF SCIENCES, ENGINEERING, AND MEDICINE Committee on Extraterrestrial Sample Analysis Facilities Space Studies Board Division on Engineering and Physical Sciences A Consensus Study Report of PREPUBLICATION COPY—SUBJECT TO FURTHER EDITORIAL CORRECTION THE NATIONAL ACADEMIES PRESS 500 Fifth Street, NW Washington, DC 20001 This activity was supported by Grant/Contract No. XXXX with XXXXX. Any opinions, findings, conclusions, or recommendations expressed in this publication do not necessarily reflect the views of any organization or agency that provided support for the project. International Standard Book Number-13: 978-0-309-XXXXX-X International Standard Book Number-10: 0-309-XXXXX-X Digital Object Identifier: https://doi.org/10.17226/25312 Additional copies of this publication are available for sale from the National Academies Press, 500 Fifth Street, NW, Keck 360, Washington, DC 20001; (800) 624-6242 or (202) 334-3313; http://www.nap.edu. Copyright 2018 by the National Academy of Sciences. All rights reserved. Printed in the United States of America Suggested citation: National Academies of Sciences, Engineering, and Medicine. 2018. Strategic Investments in Instrumentation and Facilities for Extraterrestrial Sample Curation and Analysis. Washington, DC: The National Academies Press. https://doi.org/10.17226/25312. PREPUBLICATION COPY—SUBJECT TO FURTHER EDITORIAL CORRECTION The National Academy of Sciences was established in 1863 by an Act of Congress, signed by President Lincoln, as a private, nongovernmental institution to advise the nation on issues related to science and technology. -
Outline of the Operation of MINERVA-II2 (Rover 2) Deployment
Outline of the operation of MINERVA-II2 (Rover 2) deployment Sep. 24 (Tue) 2019 Prof. Kazuya Yoshida Tohoku University (University Consortium for MINERVA-Ⅱ2 Development) Micro-Rovers and Landers Onboard Hayabusa-2 Deployed in Sep. 2018 This time ©JAXA Deployed in Oct. 2018 MASCOT By DLR/CNES By JAXA By Univ. consortium 2 Status of Rovers 2 and Purpose of the deployment (update) ⚫In the onboard function tests, the communication system between Hayabusa 2 and Rover 2 can be established. However, the Rover 2 data processor cannot be booted normally. This situation is still the same since it was reported in November 2018. ⚫To obtain scientifically interesting/meaningful results from the rover 2 deployment, the Hayabusa 2 team, the University of Colorado in US, Kyushu Institute of Technology, and Tohoku University have discussed possible options. ⚫Instead of operating the rover 2 on the surface for the mobility and imaging missions, the idea was developed to release the rover at a higher altitude and put it into an orbit to go around Ryugu. If the orbital motion of rover 2 is observed by the optical cameras from Hayabusa 2, we will make a better understanding of the gravity field of Ryugu. 3 Goal of the Updated Rover 2 Operation ⚫ Acquire the scientific data that contributes to improving the accuracy of Ryugu's gravity model. ⚫ Accumulate the engineering experience for orbital maneuvering technology by orbiting a small artifact such as a CubeSat around an asteroid. Operation Plan ⚫ Separate Rover 2 at an altitude of about 1km from the surface of Ryugu. ⚫ Inject Rover 2 into an equatorial orbit toward the direction of the Ryugu’s rotation. -
An Innovative Solution to NASA's NEO Impact Threat Mitigation Grand
Final Technical Report of a NIAC Phase 2 Study December 9, 2014 NASA Grant and Cooperative Agreement Number: NNX12AQ60G NIAC Phase 2 Study Period: 09/10/2012 – 09/09/2014 An Innovative Solution to NASA’s NEO Impact Threat Mitigation Grand Challenge and Flight Validation Mission Architecture Development PI: Dr. Bong Wie, Vance Coffman Endowed Chair Professor Asteroid Deflection Research Center Department of Aerospace Engineering Iowa State University, Ames, IA 50011 email: [email protected] (515) 294-3124 Co-I: Brent Barbee, Flight Dynamics Engineer Navigation and Mission Design Branch (Code 595) NASA Goddard Space Flight Center Greenbelt, MD 20771 email: [email protected] (301) 286-1837 Graduate Research Assistants: Alan Pitz (M.S. 2012), Brian Kaplinger (Ph.D. 2013), Matt Hawkins (Ph.D. 2013), Tim Winkler (M.S. 2013), Pavithra Premaratne (M.S. 2014), Sam Wagner (Ph.D. 2014), George Vardaxis, Joshua Lyzhoft, and Ben Zimmerman NIAC Program Executive: Dr. John (Jay) Falker NIAC Program Manager: Jason Derleth NIAC Senior Science Advisor: Dr. Ronald Turner NIAC Strategic Partnerships Manager: Katherine Reilly Contents 1 Hypervelocity Asteroid Intercept Vehicle (HAIV) Mission Concept 2 1.1 Introduction ...................................... 2 1.2 Overview of the HAIV Mission Concept ....................... 6 1.3 Enabling Space Technologies for the HAIV Mission . 12 1.3.1 Two-Body HAIV Configuration Design Tradeoffs . 12 1.3.2 Terminal Guidance Sensors/Algorithms . 13 1.3.3 Thermal Protection and Shield Issues . 14 1.3.4 Nuclear Fuzing Mechanisms ......................... 15 2 Planetary Defense Flight Validation (PDFV) Mission Design 17 2.1 The Need for a PDFV Mission ............................ 17 2.2 Preliminary PDFV Mission Design by the MDL of NASA GSFC . -
Bio-Inspired Method for Close-Proximity Operations on a Near- Earth Asteroid
University of Texas at El Paso ScholarWorks@UTEP Open Access Theses & Dissertations 2020-01-01 Bio-Inspired Method for Close-Proximity Operations on a Near- Earth Asteroid Rene Alberto Valenzuela Najera University of Texas at El Paso Follow this and additional works at: https://scholarworks.utep.edu/open_etd Part of the Aerospace Engineering Commons Recommended Citation Valenzuela Najera, Rene Alberto, "Bio-Inspired Method for Close-Proximity Operations on a Near-Earth Asteroid" (2020). Open Access Theses & Dissertations. 3053. https://scholarworks.utep.edu/open_etd/3053 This is brought to you for free and open access by ScholarWorks@UTEP. It has been accepted for inclusion in Open Access Theses & Dissertations by an authorized administrator of ScholarWorks@UTEP. For more information, please contact [email protected]. BIO-INSPIRED METHOD FOR CLOSE-PROXIMITY OPERATIONS ON A NEAR-EARTH ASTEROID RENÉ ALBERTO VALENZUELA NÁJERA Doctoral Program in Mechanical Engineering APPROVED: Angel Flores Abad, Ph.D., Chair Louis Everett, Ph.D. Co-Chair Jack F. Chessa, Ph. D Virgilio Gonzalez, Ph.D. Stephen L. Crites, Jr., Ph.D. Dean of the Graduate School Copyright © by René Alberto Valenzuela Nájera 2020 Dedication This work is dedicated to all the people who dedicate time to teach me, people have been by my side to support me in difficult times, for all my family and especially my Father and Mother who have always been present in my successes and failures. BIO-INSPIRED METHOD FOR CLOSE-PROXIMITY OPERATIONS ON A NEAR-EARTH ASTEROID by RENÉ ALBERTO VALENZUELA -
MINERVA-II Rovers Developed for Hayabusa-2 Mission
Abstract for 11th Low Cost Planetary Missions Conference June 9-11, 2015, Berlin, Germany MINERVA-II rovers developed for Hayabusa-2 mission Tetsuo YOSHIMITSU, Takashi KUBOTA, and Atsushi TOMIKI (Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency) The authors have installed a rover package named ``MINERVA-II'' to the asteroid sample return mission ``Hayabusa-2'', which was launched on 3 December 2014 heading for the C-type Near Earth asteroid 1999JU3. The package consist of two rover containers, a relay module and an antenna to communicate with the rovers. Three rovers are included in the two containers. Two of them are the responsibilities of the authors installed together in one container. Another one rover packed in the secondary container comes from the domestic university members. All the rovers were developed without the official budget from the mission to seek for the technology- driven challenges on the surface of the target asteroid. This paper describes what the authors developed as well as the capabilities and the current status of the rovers. The rovers are ejected with an expected speed of 5[cm/s] when the spacecraft descends to the asteroid after the arrival at the target around 2018. They fall into the asteroid surface captured by the weak gravity and then start the autonomous exploration when the obtained data are transmitted to the relay module on the mother spacecraft. They have a hopping mobile system fitted for the movement on the microgravity environment of the asteroid surface. Two rovers are almost identical except the thermal parameters of the surface with a mass of approximately 1.1[kg]. -
Astronomy Magazine 2020 Index
Astronomy Magazine 2020 Index SUBJECT A AAVSO (American Association of Variable Star Observers), Spectroscopic Database (AVSpec), 2:15 Abell 21 (Medusa Nebula), 2:56, 59 Abell 85 (galaxy), 4:11 Abell 2384 (galaxy cluster), 9:12 Abell 3574 (galaxy cluster), 6:73 active galactic nuclei (AGNs). See black holes Aerojet Rocketdyne, 9:7 airglow, 6:73 al-Amal spaceprobe, 11:9 Aldebaran (Alpha Tauri) (star), binocular observation of, 1:62 Alnasl (Gamma Sagittarii) (optical double star), 8:68 Alpha Canum Venaticorum (Cor Caroli) (star), 4:66 Alpha Centauri A (star), 7:34–35 Alpha Centauri B (star), 7:34–35 Alpha Centauri (star system), 7:34 Alpha Orionis. See Betelgeuse (Alpha Orionis) Alpha Scorpii (Antares) (star), 7:68, 10:11 Alpha Tauri (Aldebaran) (star), binocular observation of, 1:62 amateur astronomy AAVSO Spectroscopic Database (AVSpec), 2:15 beginner’s guides, 3:66, 12:58 brown dwarfs discovered by citizen scientists, 12:13 discovery and observation of exoplanets, 6:54–57 mindful observation, 11:14 Planetary Society awards, 5:13 satellite tracking, 2:62 women in astronomy clubs, 8:66, 9:64 Amateur Telescope Makers of Boston (ATMoB), 8:66 American Association of Variable Star Observers (AAVSO), Spectroscopic Database (AVSpec), 2:15 Andromeda Galaxy (M31) binocular observations of, 12:60 consumption of dwarf galaxies, 2:11 images of, 3:72, 6:31 satellite galaxies, 11:62 Antares (Alpha Scorpii) (star), 7:68, 10:11 Antennae galaxies (NGC 4038 and NGC 4039), 3:28 Apollo missions commemorative postage stamps, 11:54–55 extravehicular activity -
Institut Für Weltraumforschung (IWF) Österreichische Akademie Der Wissenschaften (ÖAW) Schmiedlstraße 6, 8042 Graz, Austria Twitter: @IWF Oeaw
WWW.OEAW.AC.AT ANNUAL REPORT 2020 IWF INSTITUT FÜR WELTRAUMFORSCHUNG WWW.OEAW.AC.AT/IWF COVER IMAGE Artist's impression of ESA's Solar Orbiter mission, which will face the Sun from within the orbit of Mercury at its closest approach (© ESA/ATG medialab). TABLE OF CONTENTS INTRODUCTION 5 NEAR-EARTH SPACE 7 SOLAR SYSTEM 15 SUN & SOLAR WIND 15 MERCURY 18 VENUS AND MARS 21 JUPITER AND SATURN 23 COMETS AND DUST 25 EXOPLANETARY SYSTEMS 27 SATELLITE LASER RANGING 35 TECHNOLOGIES 37 NEW DEVELOPMENTS 37 INFRASTRUCTURE 40 LAST BUT NOT LEAST 41 PUBLICATIONS 43 PERSONNEL 55 IMPRESSUM INTRODUCTION INTRODUCTION The Space Research Institute (Institut für Weltraum- The Cluster mission celebrated its 20th anniversary forschung, IWF) in Graz focuses on the physics of in 2020 and still provides unique data to better our solar system and exoplanets. With about 100 staff understand space plasma. members from 20 nations it is one of the largest institutes For already five years, the four MMS spacecraft of the Austrian Academy of Sciences (Österreichische explore the acceleration processes that govern the Akademie der Wissenschaften, ÖAW). dynamics of the Earth's magnetosphere. IWF develops and builds space-qualified instruments and The first China Seismo-Electromagnetic Satellite analyzes and interprets the data returned by them. Its core (CSES-1) has studied the Earth's ionosphere since engineering expertise is in building magnetometers and 2018. CSES-2 will follow in 2022. on-board computers, as well as in satellite laser ranging, which is performed at a station operated by IWF at the On its way to Mercury, BepiColombo, had gravity Lustbühel Observatory.