Twenty (Plus) Years of University-Class Spacecraft: a Review of What Was, an Understanding of What Is, and a Look at What
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Amateur-Satellite Service
Amateur-Satellite Service 1 26/11/2012 Some facts about the amateur-satellite service • Began in 1961 • Pioneered low-cost satellite technology • First privately funded space satellites • First satellite search & rescue (OSCAR 6 & 7) • First inter-satellite transmissions • Early tele-medicine transmissions • Pioneered distributed engineering 2 26/11/2012 Amateur-satellite organizations (by country) • Argentina AMSAT-LU • Australia AMSAT-Australia • Austria AMSAT-OE • Bermuda AMSAT-BDA • Brazil BRAMSAT • Chile AMSAT-CE • Denmark AMSAT-OZ • Germany AMSAT-DL • Finland AMSAT-OH • France AMSAT-France • Israel AMSAT-Israel • Italy AMSAT-Italia 3 26/11/2012 Amateur-satellite organizations (by country)…continued • Korea KITSAT Project • Mexico AMSAT-Mexico • New Zealand AMSAT-ZL • Qatar AMSAT-Qatar • Japan JAMSAT • North America AMSAT-NA • Russia AMSAT-R • South Africa AMSAT-SA • Spain AMSAT-URE • Sweden AMSAT-Sweden • United Kingdom AMSAT-UK • USA, Canada AMSAT-NA 4 26/11/2012 Co-operation with universities to develop & construct amateur-satellites Amateur satellites have been designed and constructed by university students with the help of local amateurs and amateur-satellite organizations. Some examples: ◊ Stellenbosch University (South Africa) ◊ University of Surrey (UK) ◊ University of Mexico ◊ Weber State University (USA) 5 26/11/2012 Student satellite project 6 26/11/2012 Orbiting Satellite Carrying Amateur Radio (OSCARs) Early satellite projects • April 1959 Concept of a satellite built by and for amateurs • OSCAR I Dec 1961 - Jan 1962, -
Peter Gülzow, DB2OS 2020-06-05 © AMSAT-DL OSCAR-10 (P3-B) OSCAR-13 (P3-C) OSCAR-40 (P3-D)
Peter Gülzow, DB2OS 2020-06-05 © AMSAT-DL OSCAR-10 (P3-B) OSCAR-13 (P3-C) OSCAR-40 (P3-D) OSCAR-100 (P4-A) AMSAT Phase 4 = GEO The meaning of Es'hail “The story behind the name Es’hail (Canopus) is the name of a star which becomes visible in the night sky of the Middle East as summer turns to autumn. Traditionally, the sighting of Es’hail brings happiness as it means that winter is coming and that good weather will soon be with us. We hope that the arrival of Es’hailSat will equally be beneficial for the satellite community.” (from Es’hailSat: Follow the star) Canopus /kəˈnoʊpəs is the brightest star in the southern constellation of Carina, and is located near the western edge of the constellation around 310 light-years from the Sun. Its proper name is generally considered to originate from the mythological Canopus, who was a navigator for Menelaus, king of Sparta. H E Abdullah bin Hamad Al Attiyah, A71AU, Chairman of the Administrative Control and Time line Transparency Authority, who is also the Chairman of the Qatar Amateur Radio 1001+ arabian nights… Society (QARS) during the Qatar international amateur radio festival in December 2012. 2012 AMSAT-DL meets QARS | (DB2OS @ International Amateur Radio Festival in Qatar) | 2013 Es’hailSat - | Qatar Satellite Company | (idea, concept, design requirements, RFI, meetings with potential | suppliers, RFP, finalisiation of requirements) | 2016 Kick-Off at MELCO Japan | (Technical presentations, Requirements review, Critical Design Review, | Design Validation) | 2018 November 15th launch with SpaceX Falcon 9 2012 Qatar Ham Radio Festival Executives from Qatar’s Es’hailSat and Japan’s Mitsubishi Electric Space Systems (MELCO) in Kamakura, outside of Tokyo, Japan, to observe the vacuum chamber test of Es'hail-2. -
Naval Postgraduate School Petite Amateur Navy Satellite
f NAVAL POSTGRADUATE SCHOOL PETITE AMATEUR NAVY SATELLITE (PANSAT) NASA/USRA University Advanced Design Program i Final Design Report i L Summer 1989 Naval Postgraduate School Space Systems Academic Group Monterey, California (NA_A-CR-18_049) PETIT? AMATEUR NAVY N90-I1800 _TFLLIT_: (pANSAT) Find1 _eport (N_v;_i Postgrdduate School) ;1 o CSCL 22B ,i TABLE OF CONTENTS A. BACKGROUND ........................................................................... 2 B. DESIGN SUMMARY .................................................................... 3 1. Communications (COMM) ...................................................... 3 2. Data Processor & Sequencer (DP&S) ...................................... 3 Figure 1. PANSAT DP&S System Concept ................................................... 6 3. Power .................................................................................. 7 4. Structure Subsystem ............................................................... 8 Figure 2. PANSAT Structural Configuration .............................................. 10 5. Experiment Payload ............................................................. l0 ,, C. CONCLUSION ................................................... !........................ 11 [ APPENDIX ...................................................................... , ....................... 12 ! Fig. A1. Processor Main Board ................................................................. 12 Fig. A2. Telemetry Section, (A/D converters) ............................................ -
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. -
The Future of Amateur Radio Satellites in the Cubesat
The Future of Amateur Radio Satellites in the CubeSat Era The Radio Amateur Satellite Corporation (AMSAT) seeks to place an ongoing series of 3U or 6U satellites into highly elliptical orbits to provide long duration communications service to the worldwide amateur radio community. AMSAT's technical challenges in preparing a HEO satellite mission are very similar to what is required for Lunar or Interplanetary CubeSat missions, including harsh thermal and radiation environments, little or no magnetic field to torque against, and challenging communications links, which make this mission very different from the many LEO CubeSats that have been built and launched by other organizations. AMSAT is seeking partnerships with other organizations to demonstrate new technologies in High Earth Orbit, to carry low cost scientific instruments into HEO and to qualify for NASA sponsored launches into Geosynchronous Transfer Orbit or other high altitude orbits whenever such an opportunity occurs. Radio Amateurs have been building and launching small satellites for over 50 years. OSCAR-1 was launched on December 12, 1961 as a secondary payload on the Thor- Agena rocket that launched the US Air Force Discoverer-36 mission. OSCAR-1 was the first satellite to be deployed as a secondary payload from a launch vehicle. The bureaucratic efforts required to secure permission to launch OSCAR-1 greatly exceeded the effort required to build the satellite and established a precedent for all subsequent secondary payload launches of the past five decades. OSCAR stands for “Orbiting Satellite Carrying Amateur Radio”. Today many agencies, laboratories, universities and high schools are building and launching dozens of small satellites every year, but it all started with OSCAR-1 in 1961. -
Igor AFANASYEV, Dmitry VORONTSOV Cosmonautics | Event
cosmonautics | event Andrey Morgunov Igor AFANASYEV, Dmitry VORONTSOV AANGARA’SNGARA’S FFIRSTIRST BBLASTOFFLASTOFF At 16.04 hrs Moscow time on 9 July 2014, the Plesetsk space launch centre saw the launching facility in February 2014 to the first launch of the Angara-1.2PP launch vehicle of the advanced space rocket practice its fuelling and the nose fairing was family being developed by the Khrunichev state space research and production fitted on the rocket in March. The successful ground tests were followed by the prelaunch centre. The maiden blastoff conducted as part of the Angara flight test programme preparations. was aimed at testing the solutions embodied in the design of the URM-1 and URM-2 The date of the launch was put off for versatile rocket modules and the Angara’s launch and technical facilities as well. 27 June 2014 due to extra checks required. In this connection, orbiting an actual spacecraft had not been considered, with On 9 June, Khrunichev hosted a session of an inseparable full-scale mock-up used as payload. The flight was suborbital to the Chief Designers Council, dedicated to prevent cluttering near-Earth orbit with space junk. the preparation of the Angara to its flight tests. The session pronounced the rocket fit To say the Angara’s first launch had been In spite of the hurdles, the developer, for the trials. anticipated for a long time would be an nevertheless, got in the stretch with the Angara The LV had been taken out of the assembly understatement: it was slated for 2005 under programme. -
Commercial Space Transportation Year in Review
2007 YEAR IN REVIEW INTRODUCTION INTRODUCTION The Commercial Space Transportation: 2007 upon liftoff, destroying the vehicle and the Year in Review summarizes U.S. and interna- satellite. tional launch activities for calendar year 2007 and provides a historical look at the past five Overall, 23 commercial orbital launches years of commercial launch activity. occurred worldwide in 2007, representing 34 percent of the 68 total launches for the year. The Federal Aviation Administration’s This marked an increase over 2006, which Office of Commercial Space Transportation saw 21 commercial orbital launches (FAA/AST) licensed four commercial orbital worldwide. launches in 2007. Three of these licensed launches were successful, while one resulted Russia conducted 12 commercial launch in a launch failure. campaigns in 2007, bringing its international commercial launch market share to 52 per- Of the four orbital licensed launches, cent for the year, a record high for Russia. three used a U.S.-built vehicle: the United Europe attained a 26 percent market share, Launch Alliance Delta II operated by Boeing conducting six commercial Ariane 5 launches. Launch Services. Two of the Delta II vehi- FAA/AST-licensed orbital launch activity cles, in the 7420-10 configuration, deployed accounted for 17 percent of the worldwide the first two Cosmo-Skymed remote sensing commercial launch market in 2007. India satellites for the Italian government. The conducted its first ever commercial launch, third, a Delta II 7925-10, launched the for four percent market share. Of the 68 WorldView 1 commercial remote sensing worldwide orbital launches, there were three satellite for DigitalGlobe. launch failures, including one non-commer- cial launch and two commercial launches. -
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 European Launchers Between Commerce and Geopolitics
The European Launchers between Commerce and Geopolitics Report 56 March 2016 Marco Aliberti Matteo Tugnoli Short title: ESPI Report 56 ISSN: 2218-0931 (print), 2076-6688 (online) Published in March 2016 Editor and publisher: European Space Policy Institute, ESPI Schwarzenbergplatz 6 • 1030 Vienna • Austria http://www.espi.or.at Tel. +43 1 7181118-0; Fax -99 Rights reserved – No part of this report may be reproduced or transmitted in any form or for any purpose with- out permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “Source: ESPI Report 56; March 2016. All rights reserved” and sample transmission to ESPI before publishing. ESPI is not responsible for any losses, injury or damage caused to any person or property (including under contract, by negligence, product liability or otherwise) whether they may be direct or indirect, special, inciden- tal or consequential, resulting from the information contained in this publication. Design: Panthera.cc ESPI Report 56 2 March 2016 The European Launchers between Commerce and Geopolitics Table of Contents Executive Summary 5 1. Introduction 10 1.1 Access to Space at the Nexus of Commerce and Geopolitics 10 1.2 Objectives of the Report 12 1.3 Methodology and Structure 12 2. Access to Space in Europe 14 2.1 European Launchers: from Political Autonomy to Market Dominance 14 2.1.1 The Quest for European Independent Access to Space 14 2.1.3 European Launchers: the Current Family 16 2.1.3 The Working System: Launcher Strategy, Development and Exploitation 19 2.2 Preparing for the Future: the 2014 ESA Ministerial Council 22 2.2.1 The Path to the Ministerial 22 2.2.2 A Look at Europe’s Future Launchers and Infrastructure 26 2.2.3 A Revolution in Governance 30 3. -
Commercial Space Transportation Year in Review
Associate Administrator for Commercial Space Transportation (AST) January 2001 COMMERCIAL SPACE TRANSPORTATION: 2000 YEAR IN REVIEW Cover Photo Credits (from left): International Launch Services (2000). Image is of the Atlas 3A launch on May 24, 2000, from Cape Canaveral Air Force Station. It successfully orbited the Eutelsat W4 communications satellite for Eutelsat. Boeing Corporation (1999). Image is of the Delta 2 7420 launch on July 10, 1999, Cape Canaveral Air Force Station. It successfully orbited four Globalstar communications satellites for Globalstar, Inc. Orbital Sciences Corp. (1997). Image is of the Pegasus XL that launched August 1, 1997 and deployed the Orbview 2 (Seastar) remote sensing satellite. Sea Launch (1999). Image is of the inaugural Zenit 3SL launch on March 27, 1999, from the Odyssey Sea Launch Platform. 2000 YEAR IN REVIEW INTRODUCTION INTRODUCTION In 2000, there were ten commercial launches 3A vehicle, which deployed a communications licensed by the Federal Aviation Administration spacecraft for Eutelsat. (FAA) for revenue that totaled about $625 million. This total represents seven launches Several new commercial space applications from U.S. ranges for commercial and contributed to the worldwide commercial launch government customers plus three launches by the total. Three Proton rockets deployed satellites multinational Sea Launch venture. for Sirius Satellite Radio, a company that will offer direct radio broadcast services to the United Overall, 35 worldwide commercial launches States. Three Soyuz vehicles carried cargo and a occurred in 2000. This number is slightly less cosmonaut crew to the Mir space station with than prior years (39 in 1999 and 41 in 1998). private financing from MirCorp, a company that However, the U.S. -
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