The Sixth International Conference of Tethers in Space. Book of Abstracts
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NIAC 2002-2003 Annual Report
TABLE OF CONTENTS EXECUTIVE SUMMARY ...............................................................................................................................................1 ACCOMPLISHMENTS Summary ................................................................................................................................................................2 Call for Proposals CP 01-01 (Phase II)...................................................................................................................2 Call for Proposals CP 01-02 (Phase I)....................................................................................................................3 Call for Proposals CP 02-01 (Phase II)...................................................................................................................4 Call for Proposals CP 02-02 (Phase I)....................................................................................................................5 Phase II Site Visits..................................................................................................................................................5 Infusion of Advanced Concepts into NASA.............................................................................................................6 Survey of Technologies to Enable NIAC Concepts.................................................................................................8 Special Recognition for NIAC Concept ...................................................................................................................9 -
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. -
Graphene Infused Space Industry a Discussion About Graphene
Graphene infused space industry a discussion about graphene NASA Commercial Space Lecture Series Our agenda today Debbie Nelson The Nixene Journal Rob Whieldon Introduction to graphene and Powder applications Adrian Nixon State of the art sheet graphene manufacturing technology Interactive session: Ask anything you like Rob Whieldon Adrian Nixon Debbie Nelson American Graphene Summit Washington D.C. 2019 https://www.nixenepublishing.com/nixene-publishing-team/ Who we are Rob Whieldon Rob Whieldon is Operations Director for Nixene Publishing having spent over 20 years supporting businesses in the SME community in the UK. He was the Executive Director of the prestigious Goldman Sachs 10,000 Small Businesses Adrian Nixon Debbie Nelson programme in Yorkshire and Humber and Adrian began his career as a scientist and is a Chartered Chemist and Debbie has over two decades is the former Director of Small Business Member of the Royal Society of experience in both face-forward and Programmes at Leeds University Business Chemistry. He has over 20 years online networking. She is active with School. He is a Gold Award winner from experience in industry working at ongoing NASA Social activities, and the UK Government Small Business Allied Colloids plc, an international enjoyed covering the Orion capsule Charter initiative and a holder of the EFMD chemicals company (now part of water test and Apollo 50th (European Framework for Management BASF). Adrian is the CEO and Editor anniversary events at Marshall Development) Excellence in Practice in Chief of Nixene Publishing, which Space Center. Debbie serves as Award. More recently he was a judge for he established in the UK in 2017. -
Pathways to Colonization David V
Pathways To Colonization David V. Smitherman, Jr. NASA, Marshall Space F’light Center, Mail CoLFDO2, Huntsville, AL 35812,256-961-7585, Abstract. The steps required for space colonization are many to grow fiom our current 3-person International Space Station,now under construction, to an inhstmcture that can support hundreds and eventually thousands of people in space. This paper will summarize the author’s fmdings fiom numerous studies and workshops on related subjects and identify some of the critical next steps toward space colonization. Findings will be drawn from the author’s previous work on space colony design, space infirastructure workshops, and various studies that addressed space policy. In cmclusion, this paper will note that siBnifcant progress has been made on space facility construction through the International Space Station program, and that si&icant efforts are needed in the development of new reusable Earth to Orbit transportation systems. The next key steps will include reusable in space transportation systems supported by in space propellant depots, the continued development of inflatable habitat and space elevator technologies, and the resolution of policy issues that will establish a future vision for space development A PATH TO SPACE COLONIZATION In 1993, as part of the author’s duties as a space program planner at the NASA Marshall Space Flight Center, a lengthy timeline was begun to determine the approximate length of time it might take for humans to eventually leave this solar system and travel to the stars. The thought was that we would soon discover a blue planet around another star and would eventually seek to send a colony to explore and expand our presence in this galaxy. -
Space Propulsion.Pdf
Deep Space Propulsion K.F. Long Deep Space Propulsion A Roadmap to Interstellar Flight K.F. Long Bsc, Msc, CPhys Vice President (Europe), Icarus Interstellar Fellow British Interplanetary Society Berkshire, UK ISBN 978-1-4614-0606-8 e-ISBN 978-1-4614-0607-5 DOI 10.1007/978-1-4614-0607-5 Springer New York Dordrecht Heidelberg London Library of Congress Control Number: 2011937235 # Springer Science+Business Media, LLC 2012 All rights reserved. This work may not be translated or copied in whole or in part without the written permission of the publisher (Springer Science+Business Media, LLC, 233 Spring Street, New York, NY 10013, USA), except for brief excerpts in connection with reviews or scholarly analysis. Use in connection with any form of information storage and retrieval, electronic adaptation, computer software, or by similar or dissimilar methodology now known or hereafter developed is forbidden. The use in this publication of trade names, trademarks, service marks, and similar terms, even if they are not identified as such, is not to be taken as an expression of opinion as to whether or not they are subject to proprietary rights. Printed on acid-free paper Springer is part of Springer Science+Business Media (www.springer.com) This book is dedicated to three people who have had the biggest influence on my life. My wife Gemma Long for your continued love and companionship; my mentor Jonathan Brooks for your guidance and wisdom; my hero Sir Arthur C. Clarke for your inspirational vision – for Rama, 2001, and the books you leave behind. Foreword We live in a time of troubles. -
Space Elevator a New Way to Gain Orbit Adil Oubou 5/3/2014
Space Elevator A New Way To Gain Orbit Adil Oubou 5/3/2014 Abstract After 56 years of great space exploration, the space flight program found itself asking an intriguing question: What’s next? Should humans constrain the space program to low Earth orbit, revisit the moon, or simply go beyond anything they have done before? No matter what the next step is, there is a great need for a reliable, safe, affordable and easy method of gaining orbit. The space elevator concept discussed in this report, based on the design provided in Peter Swan’s book “Space Elevators: An Assessment of the Technological Feasibility and the Way Forward“, shines the light on an economically and technologically feasible solution within the next two decades that will lift payloads including humans from the earth’s surface into space at a greater capacity than current rockets while significantly lowering cost to $500/kg. The system design includes a tether line that extends from the Earth’s surface to an altitude of 100,000 km that utilizes electrical motor driven climbers to gain orbit. The success feasibility of this space flight system is highly dependent on the development of Carbon Nanotube (CNT) material, which will provide high strength and low mass properties for the space elevator system components to withstand environmental and operational stresses. Table of Contents 1.0 The New Way to Orbit ....................................................................................................... 4 2.0 Why Space Elevator? ........................................................................................................ -
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. -
Analysis of Space Elevator Technology
Analysis of Space Elevator Technology SPRING 2014, ASEN 5053 FINAL PROJECT TYSON SPARKS Contents Figures .......................................................................................................................................................................... 1 Tables ............................................................................................................................................................................ 1 Analysis of Space Elevator Technology ........................................................................................................................ 2 Nomenclature ................................................................................................................................................................ 2 I. Introduction and Theory ....................................................................................................................................... 2 A. Modern Elevator Concept ................................................................................................................................. 2 B. Climber Concept ............................................................................................................................................... 3 C. Base Station Concept ........................................................................................................................................ 4 D. Space Elevator Astrodynamics ........................................................................................................................ -
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 _________________________________________________________________________________________ -
Achievable Space Elevators for Space Transportation and Starship
1991012826-321 :1 TRANSPORTATIONACHIEVABLE SPACEAND ELEVATORSTARSHIPSACCELERATFOR SP_CEION ._ Fl_t_ Dynamic_L',_rator_ N91-22162 Wright-PattersonAFB,Ohio ABSTRACT Spaceelevatorconceptslorlow-costspacelau,'x,,hea_rereviewed.Previousconceptssuffered;rein requirementsforultra-high-strengthmaterials,dynamicallyunstablesystems,orfromdangerofoollisionwith spacedeb._s.Theuseofmagneticgrain_reams,firstF_posedby BenoitLeben,solvestheseproblems. Magneticgrain_reamscansupportshortspace6!evatorsforliftingpayloadscheaplyintoEarthorbit, overcomingthematerialstrengthp_Oiemin.buildingspaceelevators.Alternatively,thestreamcouldsupport an internationaspaceportl circling__heEarthdailyt_nsofmilesabovetheequator,accessibleto adv_ncad aircraft.Marscouldbe equippedwitha similargrainstream,usingmaterialfromitsmoonsPhobosandDefines. Grain-streamarcsaboutthesuncould_ usedforfastlaunchestotheouterplanetsandforaccelerating starshipsto nearikjhtspeedforinterstella:recor_naisar',cGraie. nstreamsareessentiallyimperviousto collisions,andcouldreducethecost_f spacetranspo_ationbyan o_er c,,fmagnih_e. iNTRODUCTION Themajorob_,tacletorapi( spacedevei,apmentisthehighco_ oflaunct_!,'D_gayloadsintoEarthorbit. Currentlaunchcostsare morethan_3000per kilogramand, rocketvehicles_ch asNASP,S,_nger_,'_the AdvancedLaunchSystemwiltstillcost$500perkilogram.Theprospectsforspaceente_dseandsettlement. arenotgoodunlessthesehighlaunchc_stsarereducedsignificantly. Overthepastthirtyyears,severalconceptshavebeendevelopedforlaunchir_la{_opayloadsintoEarth orbitcheaplyusing"_rJeceelevators."The._estructurescanbesupportedbyeithe.rs_ati,for::