History of the Tether Concept and Tether Missions: a Review Chen, Yi; Huang, Rui ; Ren, Xianlin ; He, Liping ; He, Ye
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Bare Tape Tether Scaling Laws
Departamento de F´ısica Aplicada a la Ingenier´ıa Aeronautica´ Escuela Tecnica´ Superior de Ingenieros Aeronauticos´ Bare-tape scaling laws for de-orbit missions in a space debris environment Tesis Doctoral SHAKER BAYAJID KHAN Ingeniero Mecanico´ DIRECTOR JUAN R. SANMART´IN Doctor Ingeniero Aeronautico´ & GONZALO SANCHEZ´ ARRIAGA Doctor Ingeniero Aeronautico´ Madrid, 2014 "সোেচর িবলতা িনেজের অপমান। সেটর ক1নােত হােয়া না িয়মাণ। - মু8 কেরা ভয়, আপনা মােঝ শি8 ধেরা, িনেজের কেরা জয়।" --- রবীনাথ ঠাকু র “Never be demoralized in hesitance In the reason of danger, never lagged behind Release yourself from fear Stand upright, win over thyself with strength.” ---Rabindranath Tagore Tribunal nombrado por el Sr. Rector Magfco. de la Universidad Polit´ecnica de Madrid, el d´ıa ...... de ............... de 2014. Presidente: .............................. Vocal: .................................... Vocal: .................................... Vocal: .................................... Secretario: ................................. Suplente:................................. Suplente: ................................. Realizado el acto de defensa y lectura de la Tesis el d´ıa .... de........ de 2014 en la E.T.S.I. Aeronauticos.´ Calificac´ıon ................................................... EL PRESIDENTE LOS VOCALES EL SECRETARIO Acknowledgements To my Parents It gives me great pleasure in expressing my sincere gratitude to all those people who have supported me and had their contributions in making this thesis possible. First and foremost, I would never have accomplished my achievements upto this point without the unconditional sacrifice and endless support from my parents. Starting from the very beginning of my childhood days, with her stories of admiral Nelson, my mother deserves special acknowledgement for giving me the unyielding mindset, that eventually became a key virtue to lead me through the barriers. -
Modular Spacecraft with Integrated Structural Electrodynamic Propulsion
NAS5-03110-07605-003-050 Modular Spacecraft with Integrated Structural Electrodynamic Propulsion Nestor R. Voronka, Robert P. Hoyt, Jeff Slostad, Brian E. Gilchrist (UMich/EDA), Keith Fuhrhop (UMich) Tethers Unlimited, Inc. 11807 N. Creek Pkwy S., Suite B-102 Bothell, WA 98011 Period of Performance: 1 September 2005 through 30 April 2006 Report Date: 1 May 2006 Phase I Final Report Contract: NAS5-03110 Subaward: 07605-003-050 Prepared for: NASA Institute for Advanced Concepts Universities Space Research Association Atlanta, GA 30308 NAS5-03110-07605-003-050 TABLE OF CONTENTS TABLE OF CONTENTS.............................................................................................................................................1 TABLE OF FIGURES.................................................................................................................................................2 I. PHASE I SUMMARY ........................................................................................................................................4 I.A. INTRODUCTION .............................................................................................................................................4 I.B. MOTIVATION .................................................................................................................................................4 I.C. ELECTRODYNAMIC PROPULSION...................................................................................................................5 I.D. INTEGRATED STRUCTURAL -
Thesis the Effects of a Realistic Hollow Cathode
THESIS THE EFFECTS OF A REALISTIC HOLLOW CATHODE PLASMA CONTACTOR MODEL ON THE SIMULATION OF BARE ELECTRODYNAMIC TETHER SYSTEMS Submitted by Derek M. Blash Department of Mechanical Engineering In partial fulfillment of the requirements For the Degree of Master of Science Colorado State University Fort Collins, Colorado Fall 2013 Master's Committee: Advisor: John D. Williams Thomas H. Bradley Raymond S. Robinson Copyright by Derek Blash 2013 All Rights Reserved Abstract THE EFFECTS OF A REALISTIC HOLLOW CATHODE PLASMA CONTACTOR MODEL ON THE SIMULATION OF BARE ELECTRODYNAMIC TETHER SYSTEMS The region known as Low-Earth Orbit (LEO) has become populated with artificial satel- lites and space debris since humanities initial venture into the region. This has turned LEO into a hazardous region. Since LEO is very valuable to many different countries, there has been a push to prevent further buildup and talk of even deorbiting spent satellites and de- bris already in LEO. One of the more attractive concepts available for deorbiting debris and spent satellites is a Bare Electrodynamic Tether (BET). A BET is a propellantless propul- sion technique in which two objects are joined together by a thin conducting material. When these tethered objects are placed in LEO, the tether sweeps across the magnetic field lines of the Earth and induces an electromotive force (emf ) along the tether. Current from the space plasma is collected on the bare tether under the action of the induced emf, and this current interacts with the Earth's magnetic field to create a drag force that can be used to deorbit spent satellites and space debris. -
Tethers in Space Handbook - Second Edition
Tethers In Space Handbook - Second Edition - (NASA-- - I SECOND LU IT luN (Spectr Rsdrci ystLSw) 259 P C'C1 ? n: 1 National Aeronautics and Space Administration Office of Space Flight Advanced Program Development NASA Headquarters Code MD Washington, DC 20546 This document is the product of support from many organizations and individuals. SRS Technologies, under contract to NASA Headquarters, compiled, updated, and prepared the final document. Sponsored by: National Aeronautics and Space Administration NASA Headquarters, Code MD Washington, DC 20546 Contract Monitor: Edward J. Brazil!, NASA Headquarters Contract Number: NASW-4341 Contractor: SRS Technologies Washington Operations Division 1500 Wilson Boulevard, Suite 800 Arlington, Virginia 22209 Project Manager: Dr. Rodney W. Johnson, SRS Technologies Handbook Editors: Dr. Paul A. Penzo, Jet Propulsion Laboratory Paul W. Ammann, SRS Technologies Tethers In Space Handbook - Second Edition - May 1989 Prepared For: National Aeronautics and Space Administration Office of Space Flight Advanced Program Development NASA National Aeronautics and Space Administration FOREWORD The Tethers in Space Handbook Second Edition represents an update to the initial volume issued in September 1986. As originally intended, this handbook is designed to serve as a reference manual for policy makers, program managers, educators, engineers, and scientists alike. It contains information for the uninitiated, providing insight into the fundamental behavior of tethers in space. For those familiar with space tethers, it summarizes past and ongoing studies and programs, a complete bibliography of tether publications, and names, addresses, and phone numbers of workers in the field. Perhaps its most valuable asset is the brief description of nearly 50 tether applications which have been proposed and analyzed over the past 10 years. -
A Rapid and Scalable Approach to Planetary Defense Against Asteroid Impactors
THE LEAGUE OF EXTRAORDINARY MACHINES: A RAPID AND SCALABLE APPROACH TO PLANETARY DEFENSE AGAINST ASTEROID IMPACTORS Version 1.0 NASA INSTITUTE FOR ADVANCED CONCEPTS (NIAC) PHASE I FINAL REPORT THE LEAGUE OF EXTRAORDINARY MACHINES: A RAPID AND SCALABLE APPROACH TO PLANETARY DEFENSE AGAINST ASTEROID IMPACTORS Prepared by J. OLDS, A. CHARANIA, M. GRAHAM, AND J. WALLACE SPACEWORKS ENGINEERING, INC. (SEI) 1200 Ashwood Parkway, Suite 506 Atlanta, GA 30338 (770) 379-8000, (770)379-8001 Fax www.sei.aero [email protected] 30 April 2004 Version 1.0 Prepared for ROBERT A. CASSANOVA NASA INSTITUTE FOR ADVANCED CONCEPTS (NIAC) UNIVERSITIES SPACE RESEARCH ASSOCIATION (USRA) 75 5th Street, N.W. Suite 318 Atlanta, GA 30308 (404) 347-9633, (404) 347-9638 Fax www.niac.usra.edu [email protected] NIAC CALL FOR PROPOSALS CP-NIAC 02-02 PUBLIC RELEASE IS AUTHORIZED The League of Extraordinary Machines: NIAC CP-NIAC 02-02 Phase I Final Report A Rapid and Scalable Approach to Planetary Defense Against Asteroid Impactors Table of Contents List of Acronyms ________________________________________________________________________________________ iv Foreword and Acknowledgements___________________________________________________________________________ v Executive Summary______________________________________________________________________________________ vi 1.0 Introduction _________________________________________________________________________________________ 1 2.0 Background _________________________________________________________________________________________ -
Siewnarine Vishal 2015 Masters
THE IMPACT OF ATMOSPHERIC MODELS ON THE DYNAMICS OF SPACE TETHER SYSTEMS Vishal Siewnarine A THESIS SUBMITTED TO THE FACULTY OF GRADUATE STUDIES IN PARTIAL FULFILMENT OF THE REQUIREMENTS FOR THE DEGREE OF MASTER OF SCIENCE Graduate Program in Physics and Astronomy York University Toronto, Ontario September 2015 Vishal Siewnarine, 2015 Abstract Space debris has become an increasingly larger concern for aerospace travel and exploration. One idea to control the space debris population is to de-orbit defunct satellites using a space tether system. A space tether system is often made up of three parts: the main satellite, the tether and the sub-satellite. The tether connects the main satellite and the sub-satellite. Space tether systems make use of the Lorentz force as an electrodynamic drag for de-orbit. We use an established model of a space tether system to observe how satellites de- orbit. This model was constructed in MATLAB (Simulink) and uses the 1976 U.S. Standard Atmosphere. However, we wish to investigate how the model behaves using newer and more accurate atmospheric models, namely, the Jacchia-Bowman 2008 model and the Drag Temperature Model 2013. We also investigate the effect of controlling the tether's libration energy under the three aforementioned atmospheric models. ii Acknowledgements First of all, I would like to thank God for bringing me to this point. Without her, nothing is possible. Next, I would like to thank Professor Zheng Hong Zhu for his enduring patience and effort in being my supervisor and mentor whose sincerity, encouragement, late nights and tireless efforts helped shape my focus and inspire me as I hurdle all the obstacles and barriers in the completion of this work. -
Tethers in Space Handbook
Tethers In Space Handbook rampantly.Compensatory Chancy and Jeremiasmustached flamed, Casey his denationalises loon stapling herconned role plumingdebauchedly. or james retrorsely. Aleck brush-off Some cases where they conserve energy gap is especially useful to tethers in space handbook is made Upper atmosphere after which exploit the space handbook provides good agreement to! Scientists expect the see tethers doing real authority in orbit in copper not reach distant. This paper introduces history of space tethers including tether concepts and tether. Feedback eligible for Retrieving an Electro IEEE Xplore. The handbook is moving plasma grounding techniques in tethers space handbook: a unique and are examined in general innovative space has separated from the performance of the tether part is. Tethers in this Handbook NASA Marshall Space service Center Huntsville Ala. A NUCLEAR SPACE door system the SP-100 is being developed for. Tethers In that Handbook Cosmo M L Lorenzini E C Administration National Aeronautics and Amazoncomau Books. 1 ML Cosmo EC Lorenzini Tethers in this Handbook Smithsonian. Space tether technologies in working space missions 3 7. Phase which includes tether picks up to space handbook: terms of the handbook, advanced tether will require at large counterweight, there are taken along with. Mechanisms and lubrication of electrodynamic tether system. Applications for space handbook has developed controller proved effective effort has focused definition of tethers in space handbook is the figure gives the connection is the grapple would quickly be transported up. Tethers In adventure Handbook Amazonde Cosmo M L Lorenzini. The handbook is increased tensile mode allows to space handbook: this magnetic field. -
Space Tethers and Small Satellites: Formation Flight and Propulsion
SpaceSpace TethersTethers andand SmallSmall Satellites:Satellites: FormationFormation FlightFlight andand PropulsionPropulsion ApplicationsApplications NestorNestor VoronkaVoronka TTETHERSETHERS UUNLIMITED,NLIMITED, IINC.NC. 11711 N. Creek Pkwy S., Suite D-113 Bothell, WA 98011 (425) 486-0100x678 Fax: (425) 482-9670 [email protected] SpaceSpace TetherTether ApplicationsApplications && BenefitsBenefits – EnableEnable highhigh ∆∆VV missionsmissions byby usingusing mechanicalmechanical oror electrodynamicelectrodynamic propulsionpropulsion andand motionmotion controlcontrol – ReduceReduce systemsystem massmass byby eliminatingeliminating complexcomplex subsystemssubsystems – MinimizeMinimize formationformation flyingflying systemsystem complexitycomplexity andand risksrisks – EnableEnable newnew missionsmissions byby nonnon-- KeplerianKeplerian motionmotion ofof tetheredtethered satellitessatellites Provide new and improved system capabilities by exploiting unique motion of tethered satellite system Orbit-Raising and Repositioning Launch-Assist & of LEO Spacecraft Space Tethers LEO to GTO Payload Transfer for Propellantless Propulsion Propellantless propulsion enables large ∆V missions with low mass impact Drag-Makeup Stationkeeping Capture & Deorbit of Space Debris for LEO Assets Formation Flying for Long-Baseline SAR & Interferometry PastPast TetherTether FlightFlight ExperimentsExperiments – ≥≥ 1717 tethertether experimentsexperiments flown,flown, startingstarting withwith GeminiGemini capsulecapsule tethertether – SmallSmall ExpendableExpendable -
Today's Space Elevator
International Space Elevator Consortium ISEC Position Paper # 2019-1 Today's Space Elevator Space Elevator Matures into the Galactic Harbour A Primer for Progress in Space Elevator Development Peter Swan, Ph.D. Michael Fitzgerald ii Today's Space Elevator Space Elevator Matures into the Galactic Harbour Peter Swan, Ph.D. Michael Fitzgerald Prepared for the International Space Elevator Consortium Chief Architect's Office Sept 2019 iii iv Today's Space Elevator Copyright © 2019 by: Peter Swan Michael Fitzgerald International Space Elevator Consortium All rights reserved, including the rights to reproduce this manuscript or portions thereof in any form. Published by Lulu.com [email protected] 978-0-359-93496-6 Cover Illustrations: Front – with permission of Galactic Harbour Association. Back – with permission of Michael Fitzgerald. Printed in the United States of America v vi Preface The Space Elevator is a Catalyst for Change! There was a moment in time that I realized the baton had changed hands - across three generations. I was talking within a small but enthusiastic group of attendees at the International Space Development Conference in June 2019. On that stage there was generation "co-inventor" Jerome Pearson, generation "advancing concept" Michael Fitzgerald and generation "excited students" James Torla and Souvik Mukherjee. The "moment" was more than an assembly of young and old. It was also a portrait of the stewards of the Space Elevator revolution -- from Inventor to Developer to Innovators. James was working a college research project on how to get to Mars in 77 days from the Apex Anchor and Souvik (16 years old) was representing his high school from India. -
Open Access Proceedings Journal of Physics: Conference Series
Journal of Physics: Conference Series PAPER • OPEN ACCESS Celestial Mechanics: from the bases of the past to the challenges of the future To cite this article: C F de Melo et al 2015 J. Phys.: Conf. Ser. 641 011001 View the article online for updates and enhancements. This content was downloaded from IP address 186.217.236.55 on 17/05/2019 at 17:44 XVII Colóquio Brasileiro de Dinâmica Orbital – CBDO IOP Publishing Journal of Physics: Conference Series 641 (2015) 011001 doi:10.1088/1742-6596/641/1/011001 Celestial Mechanics: from the bases of the past to the challenges of the future C F de Melo1, A F B A Prado2, E E N Macau2, O C Winter3, V M Gomes3 1 Federal University of Minas Gerais – UFMG, Belo Horizonte (MG), Brazil 2 National Institute for Space Research – INPE, São José dos Campos (SP), Brazil 3 São Paulo University State – UNESP, Guaratinguetá (SP), Brazil E-mail: [email protected] Abstract: This special issue of Journal of Physics: Conference Series brings a set of 31 papers presented in the Brazilian Colloquium on Orbital Dynamics (CBDO), held on December 1 - 5, 2014, in the city of Águas de Lindoia (SP), Brazil. CBDO is a traditional and important scientific meeting in the areas of Theoretical and Applied Celestial Mechanics. The meeting takes place every two years, when researchers from South America and also guests from other continents present their works and discuss the paths trodden by the space sciences. 1. Introduction Astronomy is considered the oldest of the sciences because of interest and, especially, the need to understand the celestial phenomena since the beginning of mankind. -
Space Webs Final Report
Space Webs Final Report Authors: David McKenzie, Matthew Cartmell, Gianmarco Radice, Massimiliano Vasile Affiliation: University of Glasgow ESA Research Fellow/Technical Officer: Dario Izzo Contacts: Matthew Cartmell Tel: +44(0)141 330 4337 Fax: +44(0)141 330 4343 e-mail: [email protected] Dario Izzo Tel: +31(0)71 565 3511 Fax: +31(0)71 565 8018 e-mail: [email protected] Ariadna ID: 05/4109 Study Duration: 4 months Available on the ACT website http://www.esa.int/act Contract Number: 4919/05/NL/HE Contents 1 Introduction 4 2 Literature Review 7 3 Modelling of Space-webs 9 3.1 Introduction............................ 9 3.2 ModellingMethodology. 9 3.3 WebMeshing ........................... 10 3.3.1 WebStructure... .. .. .. .. .. ... .. .. .. 10 3.3.2 DividingtheWeb . 10 3.3.3 Web Divisions . 11 3.4 EquationsofMotion . 12 3.4.1 Centre of Mass Modelling . 12 3.4.2 Rotations ......................... 13 3.4.3 Position equations . 15 3.5 EnergyModelling ......................... 15 3.5.1 SimplifyingAssumptions . 17 3.5.2 Robot Position Modelling . 17 4 Space-web Dynamics 19 4.1 Dynamical Simulation . 19 4.2 Investigating the Stability of the Space-web . 19 4.2.1 Massoftheweb...................... 20 1 4.2.2 Robot crawl velocity . 20 4.2.3 Robotmass ........................ 21 4.2.4 WebAsymmetry ..................... 21 4.3 Numerical Investigation into Stability . 23 4.3.1 Masses of the Web and Satellite . 24 4.3.2 Masses of the Web and Robot . 25 4.3.3 Mass of the Web and Angular Velocity . 26 4.3.4 Mass of the Robot and Angular Velocity . -
SPACE TETHERS: Lessons from Developing “Revolutionary” Technologies
SPACE TETHERS: Lessons from Developing “Revolutionary” Technologies Robert Hoyt Tethers Unlimited, Inc. 11807 North Creek Parkway South, Suite B-102, Bothell, WA 98011 (425) 486-0100 [email protected] www.tethers.com © 2004 TUI Agenda What’s a Space Tether? History & Status of Tethers 10 Lessons from the Development of “High-Risk/High-Payoff” Technologies 2 © 2004 TUI Space Tethers Long, thin cable or wire deployed from a spacecraft High strength tethers can enable momentum transfer from one spacecraft to another Conducting tethers can create propulsive forces through Lorentz force interactions with the Earth’s magnetic field 3 © 2004 TUI Orbit-Raising and Repositioning Launch-Assist & of LEO Spacecraft Space Tethers LEO to GTO Payload Transfer for Propellantless Propulsion Propellantless propulsion enables large ∆V missions with low mass impact Drag-Makeup Stationkeeping Capture & Deorbit of Space Debris for LEO Assets Formation Flying for Long-Baseline SAR & Interferometry Momentum Exchange • Rotating tether picks payload up from low-LEO or a suborbital launch vehicle & tosses it to GTO • Reduces the ∆V the launch vehicle must give to the payload • Greatly reduces launch vehicle size and cost, or • Increases payload capacity of launch vehicle • MXER Launch Assist could make single-stage RLV system viable 7 6 5 4 3 2 1 Payload Capacity Scaling 0 0 1000 2000 3000 5 ∆V Provided by Tether (m/s) © 2004 TUI Momentum-Exchange/Electrodynamic-Reboost (MXER) Tether Rotating tether rapidly boosts payloads to higher orbits Tether uses electrodynamic