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Asteroid Retrieval Mission
Where you can put your asteroid Nathan Strange, Damon Landau, and ARRM team NASA/JPL-CalTech © 2014 California Institute of Technology. Government sponsorship acknowledged. Distant Retrograde Orbits Works for Earth, Moon, Mars, Phobos, Deimos etc… very stable orbits Other Lunar Storage Orbit Options • Lagrange Points – Earth-Moon L1/L2 • Unstable; this instability enables many interesting low-energy transfers but vehicles require active station keeping to stay in vicinity of L1/L2 – Earth-Moon L4/L5 • Some orbits in this region is may be stable, but are difficult for MPCV to reach • Lunar Weakly Captured Orbits – These are the transition from high lunar orbits to Lagrange point orbits – They are a new and less well understood class of orbits that could be long term stable and could be easier for the MPCV to reach than DROs – More study is needed to determine if these are good options • Intermittent Capture – Weakly captured Earth orbit, escapes and is then recaptured a year later • Earth Orbit with Lunar Gravity Assists – Many options with Earth-Moon gravity assist tours Backflip Orbits • A backflip orbit is two flybys half a rev apart • Could be done with the Moon, Earth or Mars. Backflip orbit • Lunar backflips are nice plane because they could be used to “catch and release” asteroids • Earth backflips are nice orbits in which to construct things out of asteroids before sending them on to places like Earth- Earth or Moon orbit plane Mars cyclers 4 Example Mars Cyclers Two-Synodic-Period Cycler Three-Synodic-Period Cycler Possibly Ballistic Chen, et al., “Powered Earth-Mars Cycler with Three Synodic-Period Repeat Time,” Journal of Spacecraft and Rockets, Sept.-Oct. -
Low-Excess Speed Triple Cyclers of Venus, Earth, and Mars
AAS 17-577 LOW EXCESS SPEED TRIPLE CYCLERS OF VENUS, EARTH, AND MARS Drew Ryan Jones,∗ Sonia Hernandez,∗ and Mark Jesick∗ Ballistic cycler trajectories which repeatedly encounter Earth and Mars may be in- valuable to a future transportation architecture ferrying humans to and from Mars. Such trajectories which also involve at least one flyby of Venus are computed here for the first time. The so-called triple cyclers are constructed to exhibit low excess speed on Earth-Mars and Mars-Earth transit legs, and thereby reduce the cost of hyperbolic rendezvous. Thousands of previously undocumented two synodic pe- riod Earth-Mars-Venus triple cyclers are discovered. Many solutions are identified with average transit leg excess speed below 5 km/sec, independent of encounter epoch. The energy characteristics are lower than previously documented cyclers not involving Venus, but the repeat periods are generally longer. NOMENCLATURE ∆tH Earth-Mars Hohmann transfer flight time, days δ Hyperbolic flyby turning angle, degrees R;^ S;^ T^ B-plane unit vectors B B-plane vector, km µ Gravitational parameter, km3/sec2 θB B-plane angle between B and T^, degrees rp Periapsis radius, km T Cycler repeat period, days t0 Cycle starting epoch ∗ t0 Earth-Mars Hohmann transfer epoch tf Cycle ending epoch Tsyn Venus-Earth-Mars synodic period, days v1 Hyperbolic excess speed, km/sec INTRODUCTION Trajectories are computed which ballistically and periodically cycle between flybys of Venus, Earth, and Mars. Using only gravity assists, a cycling vehicle returns to the starting body after a flight time commensurate with the celestial bodies’ orbital periods, thereby permitting indefinite repetition. -
Martian Outpost the Challenges of Establishing a Human Settlement on Mars Erik Seedhouse
Martian Outpost The Challenges of Establishing a Human Settlement on Mars Erik Seedhouse Martian Outpost The Challenges of Establishing a Human Settlement on Mars Springer Published in association with ~ '· i €I Praxis Publishing PR i ~ . i •", . ~ Chichester, UK Dr Erik Seedhouse, F.B.I.S., As.M.A. Milton Ontario Canada SPRINGER±PRAXIS BOOKS IN SPACE EXPLORATION SUBJECT ADVISORY EDITOR: John Mason M.B.E., B.Sc., M.Sc., Ph.D. ISBN 978-0-387-98190-1 Springer Berlin Heidelberg New York Springer is a part of Springer Science + Business Media (springer.com) Library of Congress Control Number: 2009921645 Apart from any fair dealing for the purposes of research or private study, or criticism or review, as permitted under the Copyright, Designs and Patents Act 1988, this publication may only be reproduced, stored or transmitted, in any form or by any means, with the prior permission in writing of the publishers, or in the case of reprographic reproduction in accordance with the terms of licences issued by the Copyright Licensing Agency. Enquiries concerning reproduction outside those terms should be sent to the publishers. # Copyright, 2009 Praxis Publishing Ltd. The use of general descriptive names, registered names, trademarks, etc. in this publication does not imply, even in the absence of a specific statement, that such names are exempt from the relevant protective laws and regulations and therefore free for general use. Cover design: Jim Wilkie Copy editor: Dr John Mason Typesetting: BookEns Ltd, Royston, Herts., UK Printed in Germany on acid-free paper Contents Preface ..................................................... xiii Acknowledgments................................................xv About the author .............................................. -
Cuberover Luxembourg PR Final
For Immediate Release Contact for CubeRover: John Walk Moosbruger [email protected] +1 (216) 906-2393 Contact for Astrobotic: Carolyn Pace [email protected] +1 (412) 682-3282 Contact for the Luxembourg Ministry of the Economy: Paul Zenners [email protected] (+352) 288 482-24 CubeRover to Develop Next Generation Planetary Rovers in Luxembourg CubeRover Platform to Revolutionize Lunar Access and Capability for Companies, Governments, Universities, and Non-Profits September 27, 2018 Luxembourg City, Luxembourg - CubeRover SARL (CubeRover) and Luxembourg announce today the agreement for the development of next-generation planetary rovers in Luxembourg. This historic agreement marks the establishment of CubeRover’s operations in the Grand Duchy as a spin out organization from Astrobotic Technology, Inc. (Astrobotic), a space robotics company based in Pittsburgh, Pennsylvania, USA. Astrobotic developed the CubeRover platform in partnership with Carnegie Mellon University under a NASA technology development contract at NASA’s Kennedy Space Center. The platform was developed to create low-cost, mobile robotic lunar access for companies, governments, universities and non-profits across the world. !1 The new headquarters in Luxembourg will be a hub for planetary rover design, manufacture, and assembly, as well as a one-stop shop for customers around the world to begin their planetary rover exploration programs. ! The CubeRover will revolutionize low mobile robotic access on the Moon. “We are excited to launch CubeRover in the Grand Duchy and enable customers around the world to begin pursuing lunar science, exploration, and commerce with their own low-cost rovers. The Ministry of the Economy and the newly established Luxembourg Space Agency have been terrific partners and great believers in CubeRover’s vision of opening access to the lunar surface,” says Mike Provenzano, President of CubeRover. -
Technology, Innovation & Engineering Committee Report NASA Advisory
National Aeronautics and Space Administration Technology, Innovation & Engineering Committee Report NASA Advisory Council Presented by: Dr. Bill Ballhaus, Chair December 2, 2015 www.nasa.gov/spacetech TI&E Committee Meeting Attendees November 10, 2015 • Dr. William Ballhaus, Chair • Mr. Gordon Eichhorst, Aperios Partners • Mr. Michael Johns, Southern Research Institute (virtual) • Dr. Matt Mountain, Association of Universities for Research in Astronomy • Mr. David Neyland, Consultant • Mr. Jim Oschmann, Ball Aerospace & Technologies Corp. • Dr. Mary Ellen Weber, STELLAR Strategies, LLC 2 TI&E Committee Meeting Presentations November 10, 2015 • Space Technology Mission Directorate Update – Mr. Stephen Jurczyk, Associate Administrator, STMD • Technology Risk/Challenges Matrix for Humans to Mars and Discussion – Mr. Jason Crusan, Director, Advanced Exploration Systems, HEOMD – Mr. Jim Reuter, Deputy AA for Programs, STMD – Mr. William Gerstenmaier, AA, HEOMD • Chief Technologist Update – Dr. David Miller, NASA Chief Technologist • Agency Technical Capability Assessment Outcomes – Mr. Ralph Roe, NASA Chief Engineer 3 Elements of the Journey to Mars 2010 2020 Now Transition Decade 2030 LEGEND First Human Mars Missions Exploration Human LEO Transition & Cis‐Lunar Habitat Cross-Cutting Long duration human health & habitation build‐up including validation for Mars transit distances (Exploration/Technology/Scie nce) Mars Robotic Precursors Science Identify resources for ISRU, demonstrate round trip surface‐to‐surface capability Asteroid Redirect Mission Human operations in deep space Orion Enabling Crew Operations in Deep Space Space Launch System Traveling beyond low Earth orbit Commercial Cargo and Crew US companies provide affordable access to low earth orbit International Space Station Mastering Long duration stays in space Mars Exploration Program MRO, Curiosity, MAVEN, InSight, Mars 2020. -
NASA Technical Memorandum 0000
NASA/TM–2016-219182 Frontier In-Situ Resource Utilization for Enabling Sustained Human Presence on Mars Robert W. Moses and Dennis M. Bushnell Langley Research Center, Hampton, Virginia April 2016 NASA STI Program . in Profile Since its founding, NASA has been dedicated to the CONFERENCE PUBLICATION. advancement of aeronautics and space science. The Collected papers from scientific and technical NASA scientific and technical information (STI) conferences, symposia, seminars, or other program plays a key part in helping NASA maintain meetings sponsored or this important role. co-sponsored by NASA. The NASA STI program operates under the auspices SPECIAL PUBLICATION. Scientific, of the Agency Chief Information Officer. It collects, technical, or historical information from NASA organizes, provides for archiving, and disseminates programs, projects, and missions, often NASA’s STI. The NASA STI program provides access concerned with subjects having substantial to the NTRS Registered and its public interface, the public interest. NASA Technical Reports Server, thus providing one of the largest collections of aeronautical and space TECHNICAL TRANSLATION. science STI in the world. Results are published in both English-language translations of foreign non-NASA channels and by NASA in the NASA STI scientific and technical material pertinent to Report Series, which includes the following report NASA’s mission. types: Specialized services also include organizing TECHNICAL PUBLICATION. Reports of and publishing research results, distributing completed research or a major significant phase of specialized research announcements and feeds, research that present the results of NASA providing information desk and personal search Programs and include extensive data or theoretical support, and enabling data exchange services. -
Communication Strategies for Colonization Mission to Mars
Communication Strategies for Colonization Mission to Mars A Thesis Submitted to the Faculty of Universidad Carlos III de Madrid In Partial Fulfillment of the Requirements for the Bachelor’s Degree in Aerospace Engineering By Pablo A. Machuca Varela June 2015 Dedicated to my dear mother, Teresa, for her education and inspiration; for making me the person I am today. And to my grandparents, Teresa and Hernan,´ for their care and love; for being the strongest motivation to pursue my goals. Acknowledgments I would like to thank my advisor, Professor Manuel Sanjurjo-Rivo, for his help and guidance along the past three years, and for his advice on this thesis. Professor Sanjurjo-Rivo first accepted me as his student and helped me discover my passion for the Orbital Mechanics research area. I am very thankful for the opportunity Professor Sanjurjo-Rivo gave me to do research for the first time, which greatly helped me improve my knowledge and skills as an engineer. His valuable advice also encouraged me to take Professor Howell’s Orbital Mechanics course and Professor Longuski’s Senior Design course while at Purdue University, as an exchange student, which undoubtedly enhanced my desire, and created the opportunity, to become a graduate student at Purdue University. I would like to thank Sarag Saikia, the Mission Design Advisor of Project Aldrin-Purdue, for his exemplary passion and enthusiasm for the field. Sarag is responsible for making me realize the interest and relevance of a Mars communication network. He encouraged me to work on this thesis, and advised me along the way. -
Study of a Crew Transfer Vehicle Using Aerocapture for Cycler Based Exploration of Mars by Larissa Balestrero Machado a Thesis S
Study of a Crew Transfer Vehicle Using Aerocapture for Cycler Based Exploration of Mars by Larissa Balestrero Machado A thesis submitted to the College of Engineering and Science of Florida Institute of Technology in partial fulfillment of the requirements for the degree of Master of Science in Aerospace Engineering Melbourne, Florida May, 2019 © Copyright 2019 Larissa Balestrero Machado. All Rights Reserved The author grants permission to make single copies ____________________ We the undersigned committee hereby approve the attached thesis, “Study of a Crew Transfer Vehicle Using Aerocapture for Cycler Based Exploration of Mars,” by Larissa Balestrero Machado. _________________________________________________ Markus Wilde, PhD Assistant Professor Department of Aerospace, Physics and Space Sciences _________________________________________________ Andrew Aldrin, PhD Associate Professor School of Arts and Communication _________________________________________________ Brian Kaplinger, PhD Assistant Professor Department of Aerospace, Physics and Space Sciences _________________________________________________ Daniel Batcheldor Professor and Head Department of Aerospace, Physics and Space Sciences Abstract Title: Study of a Crew Transfer Vehicle Using Aerocapture for Cycler Based Exploration of Mars Author: Larissa Balestrero Machado Advisor: Markus Wilde, PhD This thesis presents the results of a conceptual design and aerocapture analysis for a Crew Transfer Vehicle (CTV) designed to carry humans between Earth or Mars and a spacecraft on an Earth-Mars cycler trajectory. The thesis outlines a parametric design model for the Crew Transfer Vehicle and presents concepts for the integration of aerocapture maneuvers within a sustainable cycler architecture. The parametric design study is focused on reducing propellant demand and thus the overall mass of the system and cost of the mission. This is accomplished by using a combination of propulsive and aerodynamic braking for insertion into a low Mars orbit and into a low Earth orbit. -
Download the SSP16 Program Handbook
International Space University Space Studies Program 2016 Program Handbook Design and edit: Zhuoyan Lu with contributions from SSP Team, Local Organizing Committee, Chairs, and Faculty Image courtesy: ISU and Technion (unless otherwise specified) Poster/Cover design: Mr. Omri Tal Information reflects planning as of 9 July, 2016 Changes may occur depending upon availability of personnel and resources SSP16 website: ssp16.isunet.edu ISU website: www.isunet.edu 1 ISU SSP16 is supported at different levels by the following organizations: Major Sponsors European Astronaut Centre (EAC) Adelis Foundation Gilat Satellite Networks Ltd. Axiom Space LLC Haifa University Haifa Municipality ImageSat International (ISI) Israel Aerospace Industries Ltd. Israel Oceanographic and Limnologic Research Institute Lockheed Martin Corporation Japanese Aerospace Exploration Agency (JAXA) The Aerospace Corporation Korean Airforce Kyushu Institute of Technology LOC Precision Rocketry Program Supported by Magellan Aerospace Corporation The Boeing Company ManSat LLC Centre National d’Etudes Spatiales (CNES) Massachusetts Institute of Technology (MIT) China Space Foundation (CSF) Mission Control Space Services Inc. China Aerospace Science & Technology Corporation (CASC) Moon Express European Space Agency (ESA) MOONA - A Space for Change Ilan Ramon Foundation NanoRacks LLC Indian Space Research Organisation (ISRO) Norwegian University of Science and Technology Israel Space Agency (ISA) Odyssey Space Research National Aeronautics and Space Administration (NASA) ORBIT Communication Systems Ltd. UK Space Agency (UKSA) Orbital ATK Planet Labs Host Institution Provectus Robotics Solutions Israel Institute of Technology - Technion Royal Canadian Air Force Asher Space Research Institute Royal Military College of Canada Secure World Foundation (SWF) Sponsor Singularity University SES Deutsches Zentrum fur Luft und Raumfahrt (DLR) SNECMA El Al Israel Airlines Ltd. -
TFAWS 2019 Program
National Aeronautics and Space Administration 30th Annual Thermal & Fluids 2019 Analysis Workshop (TFAWS) August 26 to 30, 2019 City Center Marriott, Newport News, VA Sponsored by: NASA Engineering and Safety Center 30 Years Hosted by: of TFAWS: NASA Langley Research Center Power of the Past, Force of the Future https://tfaws.nasa.gov www.nasa.gov Table of Contents Overview of TFAWS 2019 ......................................................................................................... 2 Agenda....................................................................................................................................... 3 Monday, August 26, 2019 ....................................................................................................... 3 Tuesday, August 27, 2019 ...................................................................................................... 4 Wednesday, August 28, 2019 ................................................................................................. 5 Thursday, August 29, 2019 .................................................................................................... 6 Friday, August 30, 2019 ......................................................................................................... 7 TFAWS 2019 Host Center – Langley Research Center ........................................................... 8 TFAWS 2019 Hotel Information ................................................................................................ 9 Map of City Center Marriott Meeting -
Streamlining a Critical Path to Lunar Settlement Kevin Hubbard,1 Linda T
Streamlining a Critical Path to Lunar Settlement Kevin Hubbard,1 Linda T. Elkins- Tanton,1 Chris Hadfield,2 School of Earth and Space Exploration, Arizona State University.1 Chris Hadfield Inc.; University of Waterloo.2 [email protected], [email protected], chris@chrishadfield.ca.3 Sort Order: Relevance; Words and Phrases: ; Status: Commu- Human Trans- Active, Completed, Planned; Technology Area Water Mobility Habitat (Roadmaps): Power nication Support portation 4.2.1 Extreme-Terrain Mobility, 4.2.4 Small-Body and Microgravity Mobility, 4.2.5 Surface Mobility, 4.2.6 + Robot Navigation, 4.2.8 Mobility Components, 4.3.1 Generation & Handling Navigation & Tracking Water Propellant Surface Operations Infrastruture & Development ECLSS + Human Health Lunar Transit Manipulator Components, 4.3.6 Sample Acquisition and Handling, 4.5.1 System Health Management, 4.5.2 Activity Planning, Scheduling, and Execution, 4.5.4 Multi-Agent Coordination, 4.5.8 Automated Data Analysis for Decision Making, 4.6.1 Relative Naviga- tion Sensors, 4.7.3 Robot Modeling and Simulation; Target Destinations: The Moon Ames Research Center x6 Johnson Space Center Army Research Laboratory California Institute of Technology x2 ASU Actors Portfolio Columbia University x2 Draper Ames Research Center x2 Adherent Technologies Adherent Technologies ASRC Aerospace Corp. Astrobotic Energid Technologies BAE Systems Energia (Russia) Applied Physics Laboratory x2 Astrobotic Apis Cor Beihang University, China Blue Origin Glenn Research Center x4 BarcelonaTech Mission Control Space Services Arizona State University x2 Boeing BASF x2 Colorado School of Mines Deep Space Systems NASA Cross Cutting Actors Goddard Space Flight Center x2 Caltech Inc. (Canada) Astrobotic x2 Carnegie Mellon University Bechtel Dynetics, Inc. -
Earth – Mars Cycler Vehicle Conceptual Design
Earth – Mars Cycler Vehicle Conceptual Design by Bhumika Patel A thesis submitted to the Department of Aerospace, Physics, and Space Sciences at Florida Institute of Technology in partial fulfillment of the requirements for the degree of Master of Science in Aerospace Engineering Flight Mechanics and Control Systems Melbourne, Florida December 2019 We the undersigned committee hereby approve the attached thesis, “Earth – Mars Cycler Vehicle Conceptual Design,” by Bhumika Patel. _________________________________________________ Markus Wilde, Ph.D. Assistant Professor Aerospace, Physics, and Space Sciences Thesis Advisor _________________________________________________ Andrew Aldrin, Ph.D. Associate Professor Aldrin Space Institute Committee Member _________________________________________________ Brian Kish, Ph.D. Assistant Professor Aerospace, Physics, and Space Sciences Committee Member _________________________________________________ Daniel Batcheldor, Ph.D. Professor Aerospace, Physics, and Space Sciences Department Head Abstract Title: Earth – Mars Cycler Vehicle Conceptual Design Author: Bhumika Patel Advisor: Markus Wilde, Ph. D. This thesis summarizes a conceptual design for an Earth – Mars Cycler vehicle designed to transfer astronauts between Earth and Mars. The primary objective of the design study is to accommodate the crews’ needs and to estimate the overall mass and power required during Earth – Mars transfer. The study defines a concept of operations and system functional requirements and discusses the systems breakdown and subsystems design analysis. Systems developed for the cycler vehicle is designed primarily for the S1L1 cycler trajectory. The initial sizing of cycler subsystems is based on reference data from historical human spaceflight. The study performed for subsystems requirements is based on one-way trip (~154 days) to Mars. The study also addresses accommodations and life support requirements. The study does not include any detailed discussions related to the process of the vehicle assembly and launch from the ground.