ROBUSTA, a Student Satellite to Serve the Radiation Effects Community
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Orbital Lifetime Predictions
Orbital LIFETIME PREDICTIONS An ASSESSMENT OF model-based BALLISTIC COEFfiCIENT ESTIMATIONS AND ADJUSTMENT FOR TEMPORAL DRAG co- EFfiCIENT VARIATIONS M.R. HaneVEER MSc Thesis Aerospace Engineering Orbital lifetime predictions An assessment of model-based ballistic coecient estimations and adjustment for temporal drag coecient variations by M.R. Haneveer to obtain the degree of Master of Science at the Delft University of Technology, to be defended publicly on Thursday June 1, 2017 at 14:00 PM. Student number: 4077334 Project duration: September 1, 2016 – June 1, 2017 Thesis committee: Dr. ir. E. N. Doornbos, TU Delft, supervisor Dr. ir. E. J. O. Schrama, TU Delft ir. K. J. Cowan MBA TU Delft An electronic version of this thesis is available at http://repository.tudelft.nl/. Summary Objects in Low Earth Orbit (LEO) experience low levels of drag due to the interaction with the outer layers of Earth’s atmosphere. The atmospheric drag reduces the velocity of the object, resulting in a gradual decrease in altitude. With each decayed kilometer the object enters denser portions of the atmosphere accelerating the orbit decay until eventually the object cannot sustain a stable orbit anymore and either crashes onto Earth’s surface or burns up in its atmosphere. The capability of predicting the time an object stays in orbit, whether that object is space junk or a satellite, allows for an estimate of its orbital lifetime - an estimate satellite op- erators work with to schedule science missions and commercial services, as well as use to prove compliance with international agreements stating no passively controlled object is to orbit in LEO longer than 25 years. -
Cubesat Data Analysis Revision
371-XXXXX Revision - CubeSat Data Analysis Revision - November 2015 Prepared by: GSFC/Code 371 National Aeronautics and Goddard Space Flight Center Space Administration Greenbelt, Maryland 20771 371-XXXXX Revision - Signature Page Prepared by: ___________________ _____ Mark Kaminskiy Date Reliability Engineer ARES Corporation Accepted by: _______________________ _____ Nasir Kashem Date Reliability Lead NASA/GSFC Code 371 1 371-XXXXX Revision - DOCUMENT CHANGE RECORD REV DATE DESCRIPTION OF CHANGE LEVEL APPROVED - Baseline Release 2 371-XXXXX Revision - Table of Contents 1 Introduction 4 2 Statement of Work 5 3 Database 5 4 Distributions by Satellite Classes, Users, Mass, and Volume 7 4.1 Distribution by satellite classes 7 4.2 Distribution by satellite users 8 4.3 CubeSat Distribution by mass 8 4.4 CubeSat Distribution by volume 8 5 Annual Number of CubeSats Launched 9 6 Reliability Data Analysis 10 6.1 Introducing “Time to Event” variable 10 6.2 Probability of a Successful Launch 10 6.3 Estimation of Probability of Mission Success after Successful Launch. Kaplan-Meier Nonparametric Estimate and Weibull Distribution. 10 6.3.1 Kaplan-Meier Estimate 10 6.3.2 Weibull Distribution Estimation 11 6.4 Estimation of Probability of mission success after successful launch as a function of time and satellite mass using Weibull Regression 13 6.4.1 Weibull Regression 13 6.4.2 Data used for estimation of the model parameters 13 6.4.3 Comparison of the Kaplan-Meier estimates of the Reliability function and the estimates based on the Weibull regression 16 7 Conclusion 17 8 Acknowledgement 18 9 References 18 10 Appendix 19 Table of Figures Figure 4-1 CubeSats distribution by mass .................................................................................................... -
The Annual Compendium of Commercial Space Transportation: 2012
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2012 February 2013 About FAA About the FAA Office of Commercial Space Transportation The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA AST) licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 51 United States Code, Subtitle V, Chapter 509 (formerly the Commercial Space Launch Act). FAA AST’s mission is to ensure public health and safety and the safety of property while protecting the national security and foreign policy interests of the United States during commercial launch and reentry operations. In addition, FAA AST is directed to encourage, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA AST’s website: http://www.faa.gov/go/ast Cover art: Phil Smith, The Tauri Group (2013) NOTICE Use of trade names or names of manufacturers in this document does not constitute an official endorsement of such products or manufacturers, either expressed or implied, by the Federal Aviation Administration. • i • Federal Aviation Administration’s Office of Commercial Space Transportation Dear Colleague, 2012 was a very active year for the entire commercial space industry. In addition to all of the dramatic space transportation events, including the first-ever commercial mission flown to and from the International Space Station, the year was also a very busy one from the government’s perspective. It is clear that the level and pace of activity is beginning to increase significantly. -
Cubesat Communication Systems 2003-2013: a Historical Look
CubeSat Communication Systems 2003-2013: A Historical Look Bryan Klofas SRI International [email protected] Nanosatellite Ground Station Workshop San Luis Obispo, California 23 April 2013 Two Survey Papers • “A Survey of CubeSat Communication Systems” – Paper presented at the CubeSat Developers’ Workshop 2008 – By Bryan Klofas, Jason Anderson, and Kyle Leveque – Covers the CubeSats from start of program to 2008 • “A Survey of CubeSat Communication Systems: 2009-2012” – Paper presented at the CubeSat Developers’ Workshop 2013 – By Bryan Klofas and Kyle Leveque – Covers the CubeSats from 2009 to ELaNa-6/NROL-36 launch in 2012 Slide 2 Summary of CubeSat Launches 2003 to 2013 • Eurockot (30 June 2003) • Dnepr Launch 2 (17 Apr 2007) – AAU1 CubeSat – CSTB1 – DTUsat-1 – AeroCube-2 – CanX-1 – CP4 – Cute-1 – Libertad-1 – QuakeSat-1 – CAPE1 – XI-IV – CP3 • SSETI Express (27 Oct 2005) – MAST – XI-V • NLS-4/PSLV-C9 (28 Apr 2008) – NCube-2 – Delfi-C3 – UWE-1 – SEEDS-2 • M-V-8 (22 Feb 2006) – CanX-2 – Cute-1.7+APD – AAUSAT-II • Minotaur 1 (11 Dec 2006) – Compass-1 – GeneSat-1 Slide 3 Summary of CubeSat Launches 2003 to 2013 • Minotaur-1 (19 May 2009) • NLS-6/PSLV-C15 (12 July 2010) – AeroCube-3 – Tisat-1 – CP6 – StudSat – HawkSat-1 • STP-S26 (19 Nov 2010) – PharmaSat – RAX-1 • ISILaunch 01 (23 Sep 2009) – O/OREOS – BEESAT-1 – NanoSail-D2 – UWE-2 • Falcon 9-002 (8 Dec 2010) – ITUpSAT-1 – Perseus (4) – SwissCube – QbX (2) • H-IIA F17 (20 May 2010) – SMDC-ONE – Hayato – Mayflower – Waseda-SAT2 – PSLV-C18 (12 Oct 2011) – Negai-Star – Jugnu Slide 4 Summary -
Prototype Design and Mission Analysis for a Small Satellite Exploiting Environmental Disturbances for Attitude Stabilization
Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis and Dissertation Collection 2016-03 Prototype design and mission analysis for a small satellite exploiting environmental disturbances for attitude stabilization Polat, Halis C. Monterey, California: Naval Postgraduate School http://hdl.handle.net/10945/48578 NAVAL POSTGRADUATE SCHOOL MONTEREY, CALIFORNIA THESIS PROTOTYPE DESIGN AND MISSION ANALYSIS FOR A SMALL SATELLITE EXPLOITING ENVIRONMENTAL DISTURBANCES FOR ATTITUDE STABILIZATION by Halis C. Polat March 2016 Thesis Advisor: Marcello Romano Co-Advisor: Stephen Tackett Approved for public release; distribution is unlimited THIS PAGE INTENTIONALLY LEFT BLANK REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704–0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instruction, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302, and to the Office of Management and Budget, Paperwork Reduction Project (0704-0188) Washington, DC 20503. 1. AGENCY USE ONLY 2. REPORT DATE 3. REPORT TYPE AND DATES COVERED (Leave blank) March 2016 Master’s thesis 4. TITLE AND SUBTITLE 5. FUNDING NUMBERS PROTOTYPE DESIGN AND MISSION ANALYSIS FOR A SMALL SATELLITE EXPLOITING ENVIRONMENTAL DISTURBANCES FOR ATTITUDE STABILIZATION 6. AUTHOR(S) Halis C. Polat 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) 8. PERFORMING Naval Postgraduate School ORGANIZATION REPORT Monterey, CA 93943-5000 NUMBER 9. -
Space Security Index 2013
SPACE SECURITY INDEX 2013 www.spacesecurity.org 10th Edition SPACE SECURITY INDEX 2013 SPACESECURITY.ORG iii Library and Archives Canada Cataloguing in Publications Data Space Security Index 2013 ISBN: 978-1-927802-05-2 FOR PDF version use this © 2013 SPACESECURITY.ORG ISBN: 978-1-927802-05-2 Edited by Cesar Jaramillo Design and layout by Creative Services, University of Waterloo, Waterloo, Ontario, Canada Cover image: Soyuz TMA-07M Spacecraft ISS034-E-010181 (21 Dec. 2012) As the International Space Station and Soyuz TMA-07M spacecraft were making their relative approaches on Dec. 21, one of the Expedition 34 crew members on the orbital outpost captured this photo of the Soyuz. Credit: NASA. Printed in Canada Printer: Pandora Print Shop, Kitchener, Ontario First published October 2013 Please direct enquiries to: Cesar Jaramillo Project Ploughshares 57 Erb Street West Waterloo, Ontario N2L 6C2 Canada Telephone: 519-888-6541, ext. 7708 Fax: 519-888-0018 Email: [email protected] Governance Group Julie Crôteau Foreign Aairs and International Trade Canada Peter Hays Eisenhower Center for Space and Defense Studies Ram Jakhu Institute of Air and Space Law, McGill University Ajey Lele Institute for Defence Studies and Analyses Paul Meyer The Simons Foundation John Siebert Project Ploughshares Ray Williamson Secure World Foundation Advisory Board Richard DalBello Intelsat General Corporation Theresa Hitchens United Nations Institute for Disarmament Research John Logsdon The George Washington University Lucy Stojak HEC Montréal Project Manager Cesar Jaramillo Project Ploughshares Table of Contents TABLE OF CONTENTS TABLE PAGE 1 Acronyms and Abbreviations PAGE 5 Introduction PAGE 9 Acknowledgements PAGE 10 Executive Summary PAGE 23 Theme 1: Condition of the space environment: This theme examines the security and sustainability of the space environment, with an emphasis on space debris; the potential threats posed by near-Earth objects; the allocation of scarce space resources; and the ability to detect, track, identify, and catalog objects in outer space. -
PRESS KIT Vega Qualification Flight VV01
→ PRESS KIT Vega qualification flight VV01 European Space Agency Agence spatiale européenne PRESS KIT Vega qualification flight VV01 ESA inaugurates its new small launch vehicle...................................................................................................... 3 1 The Vega launch system...................................................................................................................................... 4 1.1 General design of the launch vehicle ................................................................................................... 4 1.2 The P80FW stage and new technologies............................................................................................ 5 1.3 The Zefiro stages .......................................................................................................................................... 6 1.4 AVUM ................................................................................................................................................................ 6 1.5 The fairing and adapters............................................................................................................................ 7 1.6 The launch facility ........................................................................................................................................ 8 2 The VV01 mission................................................................................................................................................... 9 2.1 Purpose of the -
Istnanosat-1 Quality Assurance, Risk Management and Assembly, Integration and Verification Planning
ISTNanosat-1 Quality Assurance, Risk Management and Assembly, Integration and Verification Planning Pedro Filipe Rodrigues Coelho Thesis to obtain the Master of Science Degree in Aerospace Engineering Supervisor: Prof. Rui M. Rocha Co-Supervisor: Prof. Moisés S. Piedade Examination Committee Chairperson: Prof. João Miranda Lemos Supervisor: Prof. Rui M. Rocha Co-Supervisor: Prof. Moisés S. Piedade Members of the Committee: Prof. Agostinho A. da Fonseca May 2016 ii Acknowledgments To Professor Rui Rocha and Professor Moisés Piedade, I have to thank the opportunity to work in the ISTNanoSat-1 Project, the guidance throughout the project and the most required pushes for this project conclusion. I would like to thank Laurent Marchand and Nicolas Saillen for the support, drive and belief. It would never have been possible to complete this work without their support and flexibility as well as their drive in my professional endeavors. To all the friendships university brought and endured in my life, that shared the worst and best of university, the late nights of work and study, the challenging exchange of ideas and ideals and all the growing into adulthood. To all my friends in ESA/ESTEC, for filling the best possible work experience with the best personnel environment. Their joy and enthusiasm in work and life were and will always be an inspiration in my life. A lei, bella Annalisa coppia di ballo, per essere la musica e la giola in tutti i76955+ momenti… À minha família, Mãe, Pai e Irmã, pelo amor incondicional, paciência e crença sem limites. Não tenho como retribuir o esforço incansável, todo o carinho e a educação modelar, senão agarrar o futuro pelo qual tanto lutaram comigo. -
A Sample AMS Latex File
PLEASE SEE CORRECTED APPENDIX A IN CORRIGENDUM, JOSS VOL. 6, NO. 3, DECEMBER 2017 Zea, L. et al. (2016): JoSS, Vol. 5, No. 3, pp. 483–511 (Peer-reviewed article available at www.jossonline.com) www.DeepakPublishing.com www. JoSSonline.com A Methodology for CubeSat Mission Selection Luis Zea, Victor Ayerdi, Sergio Argueta, and Antonio Muñoz Universidad del Valle de Guatemala, Guatemala City, Guatemala Abstract Over 400 CubeSats have been launched during the first 13 years of existence of this 10 cm cube-per unit standard. The CubeSat’s flexibility to use commercial-off-the-shelf (COTS) parts and its standardization of in- terfaces have reduced the cost of developing and operating space systems. This is evident by satellite design projects where at least 95 universities and 18 developing countries have been involved. Although most of these initial projects had the sole mission of demonstrating that a space system could be developed and operated in- house, several others had scientific missions on their own. The selection of said mission is not a trivial process, however, as the cost and benefits of different options need to be carefully assessed. To conduct this analysis in a systematic and scholarly fashion, a methodology based on maximizing the benefits while considering program- matic risk and technical feasibility was developed for the current study. Several potential mission categories, which include remote sensing and space-based research, were analyzed for their technical requirements and fea- sibility to be implemented on CubeSats. The methodology helps compare potential missions based on their rele- vance, risk, required resources, and benefits. -
Cnescnesle MAGAZINE D’INFORMATION DU Centremag NATIONAL D’ÉTUDES SPATIALES
cnescnesLE MAGAZINE D’INFORMATION DU CENTREmag NATIONAL D’ÉTUDES SPATIALES N°50 07/2011 L’ESPACE AU SERVICE DU PATRIMOINE MONDIAL Space serving world heritage EXOBIOLOGIE D’OÙ VENONS-NOUS ? OÙ SOMMES-NOUS ? Exobiology - Where are we from? Where are we now? PASCAL PICQ La vie extraterrestre sous le regard du paléoanthropologue Life ‘out there’ - a paleoanthropologist’s perspective ERATJ sommaire contents N°50 - 07/2011 04 04 / 15 news ATV-2, la fin de l’aventure ATV2 - Mission accomplished Un ballon pour la prison A balloon for prison 11 C’Space 2011, les projets étudiants s’envolent C’Space 2011 - Student projects on the launch pad politique 16 16 / 29 Business & politics Interview exclusive de Rodolphe Alexandre, président de la région Guyane, à l’occasion de l’Année des outre-mer Exclusive interview with Rodolphe Alexandre, President of the French Guiana regional council, marking French overseas territories year Nereus assure la promotion des régions européennes utilisatrices d’espace NEREUS networks European space user regions Histoire d’espace: La France dans l’exploration martienne Space history: France and Mars exploration société 30 30 / 37 Society Des sites forestiers classés par l’Unesco sous surveillance spatiale UNESCO natural heritage forests monitored from space Le mystère de L’Oiseau blanc The mystery of L’Oiseau blanc 38 / 55 dossier Special report Exobiologie, à la recherche d’une autre vie Special Report: Exobiology - Looking for other-worldly life 56 / 64 Monde World L’agence spatiale japonaise face à la catastrophe JAXA supports emergency response Europe : la communication de la Commission Europe: EC charts the way ahead 65 / 71 culture Arts & living Chapelle des îles du Salut, appel à souscription Fundraising appeal for Îles du Salut chapel restoration Faites décoller Ariane sur votre Iphone Ariane launches on iPhone 56 CNESMAG journal trimestriel de communication externe du Centre national d’études spatiales. -
Small Spacecraft Technology State of the Art
NASA/TP–2015–216648/REV1 Small Spacecraft Technology State of the Art Mission Design Division Ames Research Center, Moffett Field, California December 2015 NASA STI Program . in Profile Since its founding, NASA has been dedicated • CONFERENCE PUBLICATION. to the advancement of aeronautics and space Collected papers from scientific and science. The NASA scientific and technical technical conferences, symposia, seminars, information (STI) program plays a key part or other meetings sponsored or in helping NASA maintain this important co-sponsored by NASA. role. • SPECIAL PUBLICATION. Scientific, The NASA STI Program operates under the technical, or historical information from auspices of the Agency Chief Information NASA programs, projects, and missions, Officer. It collects, organizes, provides for often concerned with subjects having archiving, and disseminates NASA’s STI. substantial public interest. The NASA STI Program provides access to the NASA Aeronautics and Space Database • TECHNICAL TRANSLATION. English- and its public interface, the NASA Technical language translations of foreign scientific Report Server, thus providing one of the and technical material pertinent to largest collection of aeronautical and space NASA’s mission. science STI in the world. Results are Specialized services also include creating published in both non-NASA channels and custom thesauri, building customized by NASA in the NASA STI Report Series, databases, and organizing and publishing which includes the following report types: research results. • TECHNICAL PUBLICATION. Reports of For more information about the NASA STI completed research or a major significant Program, see the following: phase of research that present the results of NASA programs and include extensive • Access the NASA STI program home page data or theoretical analysis. -
Thermal Analysis of a Small Satellite in Post- Mission Phase
Journal of Multidisciplinary Engineering Science and Technology (JMEST) ISSN: 2458-9403 Vol. 6 Issue 2, February - 2019 Thermal Analysis of a Small Satellite in Post- Mission Phase Ahmed Elhefnawy Ahmed Elweteedy Space Technology Center Military Technical College Cairo, Egypt Cairo, Egypt [email protected] [email protected] Abstract— The objective of satellite thermal perigee altitude of 354 km, an apogee altitude of 1447 control is maintaining all satellite components km and an inclination of 71˚. A passive thermal control within their operational temperature range for system was used, with a small electric heater for the different missions. Most small satellites are battery. Thermal models were developed within both designed to have passive thermal control system. MATLAB/Simulink and ESATAN/ESARAD In this paper the thermal analysis of a small environments. satellite in post-mission phase is introduced. The Dinh [4] illustrated the modeling of a nanosatellite European Student Earth Orbiter (ESEO) satellite using Thermal Desktop software. The satellite has a was chosen in this study. This phase starts at the passive thermal control system. It was designed to end of the operational phase and should last at operate in LEO with altitude of 400 km. least 2 years for the chosen satellite. A finite Bulut et al [5] described the thermal control system difference thermal model using a commercial of Turksat-3U Nanosatellite [6]. The satellite orbit is software “Thermal Desktop” was described for the sun-synchronous orbit with altitude 600 km and selected satellite. Model results verification were inclination 98˚. The satellite has passive thermal performed by varying design variables and seeing control system.