The Emerging Role of Cubesats for Earth Observation Applications in South Africa
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The Space-Based Global Observing System in 2010 (GOS-2010)
WMO Space Programme SP-7 The Space-based Global Observing For more information, please contact: System in 2010 (GOS-2010) World Meteorological Organization 7 bis, avenue de la Paix – P.O. Box 2300 – CH 1211 Geneva 2 – Switzerland www.wmo.int WMO Space Programme Office Tel.: +41 (0) 22 730 85 19 – Fax: +41 (0) 22 730 84 74 E-mail: [email protected] Website: www.wmo.int/pages/prog/sat/ WMO-TD No. 1513 WMO Space Programme SP-7 The Space-based Global Observing System in 2010 (GOS-2010) WMO/TD-No. 1513 2010 © World Meteorological Organization, 2010 The right of publication in print, electronic and any other form and in any language is reserved by WMO. Short extracts from WMO publications may be reproduced without authorization, provided that the complete source is clearly indicated. Editorial correspondence and requests to publish, reproduce or translate these publication in part or in whole should be addressed to: Chairperson, Publications Board World Meteorological Organization (WMO) 7 bis, avenue de la Paix Tel.: +41 (0)22 730 84 03 P.O. Box No. 2300 Fax: +41 (0)22 730 80 40 CH-1211 Geneva 2, Switzerland E-mail: [email protected] FOREWORD The launching of the world's first artificial satellite on 4 October 1957 ushered a new era of unprecedented scientific and technological achievements. And it was indeed a fortunate coincidence that the ninth session of the WMO Executive Committee – known today as the WMO Executive Council (EC) – was in progress precisely at this moment, for the EC members were very quick to realize that satellite technology held the promise to expand the volume of meteorological data and to fill the notable gaps where land-based observations were not readily available. -
2015 October
TTSIQ #13 page 1 OCTOBER 2015 www.nasa.gov/press-release/nasa-confirms-evidence-that-liquid-water-flows-on-today-s-mars Flash! Sept. 28, 2015: www.space.com/30674-flowing-water-on-mars-discovery-pictures.html www.space.com/30673-water-flows-on-mars-discovery.html - “boosting odds for life!” These dark, narrow, 100 meter~yards long streaks called “recurring slope lineae” flowing downhill on Mars are inferred to have been formed by contemporary flowing water www.space.com/30683-mars-liquid-water-astronaut-exploration.html INDEX 2 Co-sponsoring Organizations NEWS SECTION pp. 3-56 3-13 Earth Orbit and Mission to Planet Earth 13-14 Space Tourism 15-20 Cislunar Space and the Moon 20-28 Mars 29-33 Asteroids & Comets 34-47 Other Planets & their moons 48-56 Starbound ARTICLES & ESSAY SECTION pp 56-84 56 Replace "Pluto the Dwarf Planet" with "Pluto-Charon Binary Planet" 61 Kepler Shipyards: an Innovative force that could reshape the future 64 Moon Fans + Mars Fans => Collaboration on Joint Project Areas 65 Editor’s List of Needed Science Missions 66 Skyfields 68 Alan Bean: from “Moonwalker” to Artist 69 Economic Assessment and Systems Analysis of an Evolvable Lunar Architecture that Leverages Commercial Space Capabilities and Public-Private-Partnerships 71 An Evolved Commercialized International Space Station 74 Remembrance of Dr. APJ Abdul Kalam 75 The Problem of Rational Investment of Capital in Sustainable Futures on Earth and in Space 75 Recommendations to Overcome Non-Technical Challenges to Cleaning Up Orbital Debris STUDENTS & TEACHERS pp 85-96 Past TTSIQ issues are online at: www.moonsociety.org/international/ttsiq/ and at: www.nss.org/tothestarsOO TTSIQ #13 page 2 OCTOBER 2015 TTSIQ Sponsor Organizations 1. -
Ssc09-Xii-03
SSC09-XII-03 The Promise of Innovation from University Space Systems: Are We Meeting It? Michael Swartwout St. Louis University 3450 Lindell Boulevard St. Louis, Missouri 63103; (314) 977-8240 [email protected] ABSTRACT A popular notion among universities is that we are innovation-drivers in the staid, risk-adverse spacecraft industry – we are to professional small satellites what small satellites are to the “battlestars”. By contrast, professional industry takes a much different perspective on university-class spacecraft; these programs are good for attracting students to space and providing valuable pre-career training, but the actual flight missions are ancillary, even unimportant. Which opinion is correct? Both are correct. The vast majority of the 111 student-built spacecraft that have flown have made no innovative contributions. That is not to say that they have been without contribution. In addition to the inarguable benefits to education, many have served as radio Amateur communications, science experiments and even technological demonstrations. But “innovative”? Not so much. However, there have been two innovative contributors, whose contributions are large enough to settle the question: the University of Surrey begat SSTL, which helped create the COTS-based small satellite industry. Stanford and Cal Poly begat CubeSats, whose contributions are still being created today. This paper provides an update to our earlier submissions on the history of student-built spacecraft. Major trends identified in previous years will be re-examined with new data -- especially the bifurcation between larger-scale, larger-scope "flagship" programs and small-scale, reduced-mission "independents". In particular, we will demonstrate that the general history of student-built spacecraft has not been one of innovation, nor of development of new space systems -- with those few, extremely noteworthy, exceptions. -
The SUNSAT Micro Satellite Program
The SUNSAT Micro Satellite Program: Technical performance and limits of imaging micro satellites Sias Mostert, Thys Cronje and Francois du Plessis Department of Electrical and Electronic Engineering Stellenbosch University. Private Bag X1, MATIELAND, 7602. South Africa. Fax: +27 21 808 4981. Internet: [email protected]. http:\\sunsat.ee.sun.ac.za ABSTRACT - This paper examines the technical performance of the SUNSAT micro satellite bus, which is supporting the high resolution imager (HRI) payload on the micro satellite which is scheduled for launch in December 1998. A number of existing remote sensing satellites are investigated to determine some key parameters by which a micro satellite remote sensing mission should be evaluated. The SUNSAT 1 HRI instrument is then evaluated in this context and future possible missions suggested which is suitable for micro satellite missions. 1. INTRODUCTION SUNSAT, a professional micro satellite developed by a team of graduate students and engineers at Stellenbosch University in South Africa, is scheduled for launch from Vandenberg Airforce Base on a Delta II rocket, currently manifested for December 1998. The Flight Model hardware is complete and the pre-flight testing is drawing to a close. This paper examines the technical performance and capabilities of SUNSAT 1 micro satellite supporting the high resolution imager (HRI). Laboratory measured performance data are provided for the 15 m resolution 3 color CCD imager of SUNSAT, developed jointly by Stellenbosch University, the Council for Scientific Industrial Research (CSIR) in South Africa and the Korean Advanced Institute of Science and Technology (KAIST). The performance of the Attitude Determination and Control System (ADCS), which is required to support the imager, is described. -
Issue #1 – 2012 October
TTSIQ #1 page 1 OCTOBER 2012 Introducing a new free quarterly newsletter for space-interested and space-enthused people around the globe This free publication is especially dedicated to students and teachers interested in space NEWS SECTION pp. 3-22 p. 3 Earth Orbit and Mission to Planet Earth - 13 reports p. 8 Cislunar Space and the Moon - 5 reports p. 11 Mars and the Asteroids - 5 reports p. 15 Other Planets and Moons - 2 reports p. 17 Starbound - 4 reports, 1 article ---------------------------------------------------------------------------------------------------- ARTICLES, ESSAYS & MORE pp. 23-45 - 10 articles & essays (full list on last page) ---------------------------------------------------------------------------------------------------- STUDENTS & TEACHERS pp. 46-56 - 9 articles & essays (full list on last page) L: Remote sensing of Aerosol Optical Depth over India R: Curiosity finds rocks shaped by running water on Mars! L: China hopes to put lander on the Moon in 2013 R: First Square Kilometer Array telescopes online in Australia! 1 TTSIQ #1 page 2 OCTOBER 2012 TTSIQ Sponsor Organizations 1. About The National Space Society - http://www.nss.org/ The National Space Society was formed in March, 1987 by the merger of the former L5 Society and National Space institute. NSS has an extensive chapter network in the United States and a number of international chapters in Europe, Asia, and Australia. NSS hosts the annual International Space Development Conference in May each year at varying locations. NSS publishes Ad Astra magazine quarterly. NSS actively tries to influence US Space Policy. About The Moon Society - http://www.moonsociety.org The Moon Society was formed in 2000 and seeks to inspire and involve people everywhere in exploration of the Moon with the establishment of civilian settlements, using local resources through private enterprise both to support themselves and to help alleviate Earth's stubborn energy and environmental problems. -
Operational Aspects of Orbit Determination with GPS for Small Satellites with SAR Payloads Sergio De Florio, Tino Zehetbauer, Dr
Deutsches Zentrum Microwave and Radar Institute für Luft und Raumfahrt e.V. Department Reconnaissance and Security Operational Aspects of Orbit Determination with GPS for Small Satellites with SAR Payloads Sergio De Florio, Tino Zehetbauer, Dr. Thomas Neff Phone: +498153282357, [email protected] Abstract Requirements Scientific small satellite missions for remote sensing with Synthetic Taylor expansion of the phase Φ of the radar signal as a Aperture Radar (SAR) payloads or high accuracy optical sensors, pose very function of time varying position, velocity and acceleration: strict requirements on the accuracy of the reconstructed satellite positions, velocities and accelerations. Today usual GPS receivers can fulfill the 4π 233 Φ==++++()t Rtap ()()01kk apttaptt ()(-) 02030 ()(-) k aptt ()(-) k ο () t accuracy requirements of this missions in most cases, but for low-cost- λ missions the decision for a appropriate satellite hardware has to take into Typical requirements, for 0.5 to 1.0 m image resolution, on account not only the reachable quality of data but also the costs. An spacecraft position vector x: analysis is carried out in order to assess which on board and ground equipment, which type of GPS data and processing methods are most −−242 appropriate to minimize mission costs and full satisfying mission payload x≤≤⋅≤⋅ 15 mmsms x 1.5 10 / x 6.0 10 / (3σ ) requirements focusing the attention on a SAR payload. These are requirements on the measurements, not on the real motion of the satellite Required Hardware Typical Position -
Quarterly Launch Report
Commercial Space Transportation QUARTERLY LAUNCH REPORT Featuring the launch results from the previous quarter and forecasts for the next two quarters 4th Quarter 1997 U n i t e d S t a t e s D e p a r t m e n t o f T r a n s p o r t a t i o n • F e d e r a l A v i a t i o n A d m i n i s t r a t i o n A s s o c i a t e A d m i n i s t r a t o r f o r C o m m e r c i a l S p a c e T r a n s p o r t a t i o n QUARTERLY LAUNCH REPORT 1 4TH QUARTER 1997 REPORT Objectives This report summarizes recent and scheduled worldwide commercial, civil, and military orbital space launch events. Scheduled launches listed in this report are vehicle/payload combinations that have been identified in open sources, including industry references, company manifests, periodicals, and government documents. Note that such dates are subject to change. This report highlights commercial launch activities, classifying commercial launches as one or more of the following: • Internationally competed launch events (i.e., launch opportunities considered available in principle to competitors in the international launch services market), • Any launches licensed by the Office of the Associate Administrator for Commercial Space Transportation of the Federal Aviation Administration under U.S. -
Quarterly Launch Report
Commercial Space Transportation QUARTERLY LAUNCH REPORT Featuring the launch results from the previous quarter and forecasts for the next two quarters 1st Quarter 1998 U n i t e d S t a t e s D e p a r t m e n t o f T r a n s p o r t a t i o n • F e d e r a l A v i a t i o n A d m i n i s t r a t i o n A s s o c i a t e A d m i n i s t r a t o r f o r C o m m e r c i a l S p a c e T r a n s p o r t a t i o n QUARTERLY LAUNCH REPORT 1 1ST QUARTER 1998 REPORT Objectives This report summarizes recent and scheduled worldwide commercial, civil, and military orbital space launch events. Scheduled launches listed in this report are vehicle/payload combinations that have been identified in open sources, including industry references, company manifests, periodicals, and government documents. Note that such dates are subject to change. This report highlights commercial launch activities, classifying commercial launches as one or more of the following: • Internationally competed launch events (i.e., launch opportunities considered available in principle to competitors in the international launch services market), • Any launches licensed by the Office of the Associate Administrator for Commercial Space Transportation of the Federal Aviation Administration under U.S. -
Aspects of SUNSAT Main Structure Design and Manufa
Aspects of Sunser main structure design and manufacturing fI.R. Schusterl and A.H. Basson2 (Received: January 1995; Final version May 1995) Abstract SUNSAT micro satellite project in 1989. Studies of the Department's capabilities and other programs at the uni- This paper describes sorne ouerall mechanical design 0,s- versities of Surrey and Berlin led to the January 1992 base- pects of the Stellenbosch Uniaersity satellite,'SUNSAT'. An line design compatible with Anlarup launch requirements. introduction to lhe SUNSAT project is giuen. The mechan- In 1994, NASA expressed interest in launching Sut{sar in ical design requirements are described. The design of the the same mission a^s the Danish Oersted magnetic research module trays, which conslitutes a major part of the main satellite,[2] both as secondary payloads on the Argos/Pgl- stracture, is discussed. The design and rnanufacturing of 1 Delta ll mission in October 1996. In exchange, SUNSAT the horizon sensor housing and the imager bearing hous- will provide data gathered by a precision GPS receiver ings are described to illustrate the infl,uence of the design (that NASA will supply) and the mountitrg of a set of requirements, the use of solid modelling CAD software and laser retro-reflectors on SUNSAT. The proposed orbit is the application of design fo, assembly principles in the near-polar with an inclination of 96o and an altitude vary- satellite's mechanical design. The resulting design satis- ing from 450 to 850 km.[3] firt the functional and financial constrainls. Review of previous work Introduction Thorough surveys of other international activities involv- This paper describes the mechanical design and manufac- ittg small spacecraft have been given in previous papers.[4; ture of the trays that form the main structure of Sut{sAT, 5] Only a brief summary of relevant aspects will be given as well as the horizon sensor housings and the imager bear- here. -
The Pcsat Mission and Cubesat Design Notes
SSC01-VIIIb-1 The PCsat Mission and Cubesat Design Notes Bob Bruninga, WB4APR, ENS Boutros, ENS Nolan, ENS Schwenzer, ENS Lawrence, LTCL B. Smith, Dr. D. Boden US Naval Academy Satellite Lab 590 Holloway Rd, Annapolis, MD 21402 [email protected] 410-293-6417 FAX 410-239-2591 Abstract There are growing opportunities for Universities to gain educational access to Space. The Naval Academy has used the Department of Defense Space Test Program for its PCsat and Sapphire projects and the Stanford Cubesat program offers a unique opportunity to get numerous small student satellite payloads into space. As a spin-off of our PCsat project, we have investigated several off-the-shelf solutions to the Telemetry, Command and control portion of small satellites that can greatly simplify small satellite and CubeSat designs. This permits students to concentrate on the various payloads and other aspects of the project without starting from scratch with a comm. system. This simple comm. System based on AX.25 packet radio is being flown this summer in the Naval Academy’s Personal Communications Satellite (PCsat) which will demonstrate downlinks receivable on Hand Held Transceivers (HT’s) with only a whip antenna. Further these simple downlinks can be easily fed into the Internet for live worldwide distribution of data. These designs are all based on the amateur radio standard on-air AX.25 packet network protocol that is implemented in a number of off-the-shelf modems (called Terminal Node Controllers or TNC’s). The following paragraphs describe three such hardware devices and the remainder of this paper describes how TNC’s and the AX.25 protocol were used on PCsat. -
Report of Contributions
SAIP 2011 Report of Contributions https://events.saip.org.za/e/saip2011 SAIP 2011 / Report of Contributions Defects and Reconstructions in El … Contribution ID: 2 Type: Poster Presentation Defects and Reconstructions in Electron Beam Irradiated Graphene Sheets Wednesday, 13 July 2011 17:00 (2 hours) <p>Graphene characterization and device fabrication often require extensive use of the scanning electron microscopy (SEM) and tunneling electron microscopy (TEM). These techniques involve electron beam irradiation that usually causes defects in materials under investigation. The radia- tion induced defects may lead to significant damage to the material which may alter its properties, normally an undesirable phenomenon. However, recent experiments show that electron radiation can have beneficial effects in materials. Graphenic materials have the ability to reorganize their structures under irradiation like no other materials. This property can find application in radiation hard electronics owing to the technological importance of graphenic materials. Here we report the Raman and scanning tunneling microscopy (STM) results of pristine and heat treated electron -beam irradiated graphene sheets (mono-layer and double layers) to demonstrate graphenic recon- structions. STM creates images of the charge density of electrons at the Fermi level such that all surface atoms can be visible. Level (Hons, MSc, <br> PhD, other)? PhD Consider for a student <br> award (Yes / No)? Yes Would you like to <br> submit a short paper <br> for the Conference -
Space Security 2010
SPACE SECURITY 2010 spacesecurity.org SPACE 2010SECURITY SPACESECURITY.ORG iii Library and Archives Canada Cataloguing in Publications Data Space Security 2010 ISBN : 978-1-895722-78-9 © 2010 SPACESECURITY.ORG Edited by Cesar Jaramillo Design and layout: Creative Services, University of Waterloo, Waterloo, Ontario, Canada Cover image: Artist rendition of the February 2009 satellite collision between Cosmos 2251 and Iridium 33. Artwork courtesy of Phil Smith. Printed in Canada Printer: Pandora Press, Kitchener, Ontario First published August 2010 Please direct inquires to: Cesar Jaramillo Project Ploughshares 57 Erb Street West Waterloo, Ontario N2L 6C2 Canada Telephone: 519-888-6541, ext. 708 Fax: 519-888-0018 Email: [email protected] iv Governance Group Cesar Jaramillo Managing Editor, Project Ploughshares Phillip Baines Department of Foreign Affairs and International Trade, Canada Dr. Ram Jakhu Institute of Air and Space Law, McGill University John Siebert Project Ploughshares Dr. Jennifer Simons The Simons Foundation Dr. Ray Williamson Secure World Foundation Advisory Board Hon. Philip E. Coyle III Center for Defense Information Richard DalBello Intelsat General Corporation Theresa Hitchens United Nations Institute for Disarmament Research Dr. John Logsdon The George Washington University (Prof. emeritus) Dr. Lucy Stojak HEC Montréal/International Space University v Table of Contents TABLE OF CONTENTS PAGE 1 Acronyms PAGE 7 Introduction PAGE 11 Acknowledgements PAGE 13 Executive Summary PAGE 29 Chapter 1 – The Space Environment: