PHONESAT IN-FLIGHT EXPERIENCE RESULTS V4
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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. -
A Sample AMS Latex File
Riot, V. J. et al. (2021): JoSS, Vol. 10, No. 1, pp. 995–1006 (Peer-reviewed article available at www.jossonline.com) www.adeepakpublishing.com www. JoSSonline.com Lessons Learned Using Iridium to Com- municate with a CubeSat in Low Earth Orbit Vincent J. Riot, Lance M. Simms, and Darrell Carter Lawrence Livermore National Laboratory Livermore, CA, USA Abstract This paper presents the design and approval process for operating an Iridium transceiver on orbit and provide on-orbit performance data obtained from a CubeSat platform in Low Earth Orbit (LEO) (500 km orbit). On-orbit data demonstrates that use of a commercial, low-cost Iridium transceiver can serve as a valuable communication approach for low volume telemetry with less than a 30-minute lag for approximately 90% of the time. We also demonstrate that a radial differential velocity of 7 km/sec corresponding to about a 37.5kHz doppler shift and a distance of less than 2,000 km can be used for mission planning. Introduction Setting up a dedicated radio communication link tion is about 5-15 minutes per day per ground station, with a CubeSat in Low Earth Orbit (LEO) presents depending on the altitude and inclination of the satel- several challenges, especially for institutions with lim- lite, as well as the latitude of the ground station. This ited funding or resources. The traditional approach of means the operator is oblivious to the current state of using one or more dedicated radio ground stations to the satellite most of the time, even if multiple ground communicate directly with the satellite is often prohib- stations distributed across the Earth are used. -
March 21–25, 2016
FORTY-SEVENTH LUNAR AND PLANETARY SCIENCE CONFERENCE PROGRAM OF TECHNICAL SESSIONS MARCH 21–25, 2016 The Woodlands Waterway Marriott Hotel and Convention Center The Woodlands, Texas INSTITUTIONAL SUPPORT Universities Space Research Association Lunar and Planetary Institute National Aeronautics and Space Administration CONFERENCE CO-CHAIRS Stephen Mackwell, Lunar and Planetary Institute Eileen Stansbery, NASA Johnson Space Center PROGRAM COMMITTEE CHAIRS David Draper, NASA Johnson Space Center Walter Kiefer, Lunar and Planetary Institute PROGRAM COMMITTEE P. Doug Archer, NASA Johnson Space Center Nicolas LeCorvec, Lunar and Planetary Institute Katherine Bermingham, University of Maryland Yo Matsubara, Smithsonian Institute Janice Bishop, SETI and NASA Ames Research Center Francis McCubbin, NASA Johnson Space Center Jeremy Boyce, University of California, Los Angeles Andrew Needham, Carnegie Institution of Washington Lisa Danielson, NASA Johnson Space Center Lan-Anh Nguyen, NASA Johnson Space Center Deepak Dhingra, University of Idaho Paul Niles, NASA Johnson Space Center Stephen Elardo, Carnegie Institution of Washington Dorothy Oehler, NASA Johnson Space Center Marc Fries, NASA Johnson Space Center D. Alex Patthoff, Jet Propulsion Laboratory Cyrena Goodrich, Lunar and Planetary Institute Elizabeth Rampe, Aerodyne Industries, Jacobs JETS at John Gruener, NASA Johnson Space Center NASA Johnson Space Center Justin Hagerty, U.S. Geological Survey Carol Raymond, Jet Propulsion Laboratory Lindsay Hays, Jet Propulsion Laboratory Paul Schenk, -
SGAC-Annual-Report-2014.Pdf
ANNUAL REPORT SPACE GENERATION ADVISORY COUNCIL 2014 In support of the United Nations Programme on Space Applications A. TABLE OF CONTENTS A. Table of Contents 2 In support of the United Nations Programme B. Sponsors and Partners 4 on Space Applications 1. Introduction 10 1.1 About the SGAC 12 14 c/o European Space Policy Institute (ESPI) 1.2 Letter from the Co-chairs 15 Schwarzenbergplatz 6 1.3 Letter from the Executive Director 16 Vienna A-1030 1.4 SGAC output at a glance AUSTRIA 2. SGAC Background 22 2.1 History of the SGAC 24 26 [email protected] 2.2 Leadership and Structure 27 www.spacegeneration.org 2.3 Programme +41 1 718 11 18 30 3. The organisation in 2014 30 32 +43 1 718 11 18 99 3.1 Goal Achievement Review 3.2 SGAC Activity Highlights 36 42 © 2015 Space Generation Advisory Council 3.3 Space Generation Fusion Forum Report 3.4 Space Generation Congress Report 50 3.5 United Nations Report 62 3.6 SGAC Regional Workshops 66 3.7 SGAC Supported Events 68 3.8 Financial Summary 72 Acknowledgements 4. Projects 78 4.1 Project Outcomes and Highlights 80 The SGAC 2014 Annual Report was compiled and 4.2 Space Technologies for Disaster Management Project Group 81 edited by Minoo Rathansabapathy (South Africa/ 4.3 Near Earth Objects Project Group 82 Australia), Andrea Jaime (Spain), Laura Rose (USA) 4.4 Space Law and Policy Project Group 84 and Arno Geens (Belgium) with the assistance of 4.5 Commercial Space Project Group 86 Candice Goodwin (South Africa), Justin Park (USA), 4.6 Space Safety and Sustainability Project Group 88 Nikita Marwaha (United Kingdom), Dario Schor 4.7 Small Satellites Project Group 90 (Argentina/Canada), Leo Teeney (UK) and Abhijeet 4.8 Space Exploration Project Group 92 Kumar (Australia) in editing. -
Commercial Orbital Transportation Services
National Aeronautics and Space Administration Commercial Orbital Transportation Services A New Era in Spaceflight NASA/SP-2014-617 Commercial Orbital Transportation Services A New Era in Spaceflight On the cover: Background photo: The terminator—the line separating the sunlit side of Earth from the side in darkness—marks the changeover between day and night on the ground. By establishing government-industry partnerships, the Commercial Orbital Transportation Services (COTS) program marked a change from the traditional way NASA had worked. Inset photos, right: The COTS program supported two U.S. companies in their efforts to design and build transportation systems to carry cargo to low-Earth orbit. (Top photo—Credit: SpaceX) SpaceX launched its Falcon 9 rocket on May 22, 2012, from Cape Canaveral, Florida. (Second photo) Three days later, the company successfully completed the mission that sent its Dragon spacecraft to the Station. (Third photo—Credit: NASA/Bill Ingalls) Orbital Sciences Corp. sent its Antares rocket on its test flight on April 21, 2013, from a new launchpad on Virginia’s eastern shore. Later that year, the second Antares lifted off with Orbital’s cargo capsule, (Fourth photo) the Cygnus, that berthed with the ISS on September 29, 2013. Both companies successfully proved the capability to deliver cargo to the International Space Station by U.S. commercial companies and began a new era of spaceflight. ISS photo, center left: Benefiting from the success of the partnerships is the International Space Station, pictured as seen by the last Space Shuttle crew that visited the orbiting laboratory (July 19, 2011). More photos of the ISS are featured on the first pages of each chapter. -
COMPACT) Joe Mrozinski JPL, Michael Saing JPL, Mary Covert Aerospace Corp., Tim Anderson Aerospace Corp
CubeSat Or Microsat Probabilistic + Analogies Cost Tool (COMPACT) Joe Mrozinski JPL, Michael Saing JPL, Mary Covert Aerospace Corp., Tim Anderson Aerospace Corp. Copyright 2016 California Institute of Technology. Government sponsorship acknowledged. What is a CubeSat? CubeSat = Extremely small (i.e. Nanosat scale 1- 10kg) spacecraft of standard dimensions that hitchhikes to space with a traditional spacecraft. • Standard Form Factors: how many “U’s” is your Cubesat? 1 to 6 U’s: A “1U” A “2U” Cubesat is Cubesat is 3U: roughly twice as big 10x10x10 cm 6U! 11/16/16 COMPACT 2 jpl.nasa.gov What is a Microsat? A Microsat is simply a satellite with mass between 10 kg and 100 kg. Most 1-3U CubeSats are 1 - 10 kg, and fall into the “Nanosat” range. But a 6U Cubesat likely has a mass >10 kg and thus would be a microsat. CubeSat Or Microsat Probabilistic + Analogies Cost Tool (COMPACT) COMPACT is exploring CubeSats first. 11/16/16 COMPACT 3 jpl.nasa.gov NASA does not have a CubeSat Cost Estimating …But NASA Capability… clearly needs one -- ASAP! Graphic from: “CubeSat Most of Technology and Systems,” these Janson, S., Presentation to “Nanosats” USGIF Small Satellite are Working Group, 27 Cubesats May 2015 11/16/16 COMPACT 4 jpl.nasa.gov COMPACT just completed Phase 1 to begin addressing this cost estimating capability gap Phase 1 Requirement: Collect & Normalize Key Cost Driver Data for 10 CubeSats 11/16/16 COMPACT 5 jpl.nasa.gov Phase 1 Delivery: Normalized Data for 18 CubeSats 11/16/16 COMPACT 6 jpl.nasa.gov O_OREOS CINEMA EDSN GRIFEX LMRST KickSat Phase 1 Delivery: Normalized Data for: IPEX Firefly 18 CubeSats M-Cubed 2 PSSC-2 SkyCube SporeSat-1 MarCO NanoSail-D RACE RAX 1 11/16/16 M-Cubed COMPACT PharmaSat 7 jpl.nasa.gov Key Data i.e. -
Phonesat: Modeling a Spacecraft for Remote Imaging
MIT Space Exploration Initiative Outreach PhoneSat: Modeling a spacecraft for remote imaging Avery Normandin Published on: Apr 02, 2020 License: Creative Commons Attribution 4.0 International License (CC-BY 4.0) MIT Space Exploration Initiative Outreach PhoneSat: Modeling a spacecraft for remote imaging Activity: creating a small satellite to protect your cell phone in outer-space environments! Background: Small satellites are constantly orbiting Earth, providing useful data about the planet over time. These satellites are designed and built by engineers to withstand the harsh space environment. A “cubesat” is a specific type of small satellite that has very particular specifications, making it easier for people around the world to design and launch. Today, you’ll be turning your phone into a mock-satellite! Mission: It’s your first visit to space as NASA’s newest astronaut - congratulations! Your first mission is to deploy a 1U (10 x 10 x 10 cm) small satellite that takes pictures of the plants and trees in your neighborhood. Your plan is to thrust the satellite into orbit by throwing it outside the International Space Station (ISS). However, during launch, you hear a loud crash - the satellite you have spent the last year designing and building has fallen and broken! Mission control informs you that you are still responsible for getting a satellite into orbit upon your arrival to the ISS. Your new mission is to rebuild the satellite and test a prototype first at home -- one that takes. The only ‘computer’ available to run your satellite? Your smartphone! Using the constraints defined by a cubesat, you will be creating a prototype structure that nests your phone as a “satellite payload”. -
Communications for the Techedsat/Phonesat Missions NASA Ames Research Center
Communications for the TechEdSat/PhoneSat Missions NASA Ames Research Center Presentation to Small Satellite Pre-Conference Workshop August 5, 2017 Marcus Murbach, PI Rick Alena, Co-I Ali Guarneros-Luna, Co-I Jon Wheless, Engineer SOAREX/TechEdSat/PhoneSat Teams Flight Experiments of Recent Years (2008-2017): 9 Flights SOAREX-6 (2008) SOAREX-7 TES-1 TES-2 (2009) Oct 4, 2012 TES-3 PhoneSat Aug 3, 2013 Iridium-test (6 wk de- Aug 21, 2013 TES-4 orbit) Mar 3, 2015 TES-5 (4 wk de-orbit) Mar 6, 2017 (deorbited Jul 29) TES/PS Team, 2014 SOAREX-8 (2015) SOAREX-9 (2016) TES/PS Team, Summer 2017 What is an Exo-Brake…? Simple, drag-modulated de-orbit system based on tension elements TechEdSat5 was deployed from ISS on March 6, 2017 by NanoRacks The TechEdSat 5 Exo-Brake Experiment • The Exo-Brake is an exo-atmospheric braking and de-orbit device which has successfully flown twice before in a fixed configuration on TechEdSat-3 and 4 • The TechEdSat rapid prototype flight series is conducted as a hands-on training environment for young professionals and university partners • The project helps verify Entry Systems Modeling by gathering real-world data aboard sounding rockets and CubeSats • In the future, passive Exo-Brake systems may be used for small-sat disposal and the development of technologies to permit on-demand sample return from Low Earth Orbit (LEO) scientific/manufacturing platforms TechEdSat 5 (TES5) Avionics, Software and Communications • The 3.5 U CubeSat contains a low-level AVR microprocessor for power control and a high-level Atom processor for fast data processing • The primary Command and Telemetry (C&T) link is provided by the Iridium constellation through on-board Short Burst Data (SBD) modems. -
Britain Back in Space
Spaceflight A British Interplanetary Society Publication Britain back in Space Vol 58 No 1 January 2016 £4.50 www.bis-space.com 1.indd 1 11/26/2015 8:30:59 AM 2.indd 2 11/26/2015 8:31:14 AM CONTENTS Editor: Published by the British Interplanetary Society David Baker, PhD, BSc, FBIS, FRHS Sub-editor: Volume 58 No. 1 January 2016 Ann Page 4-5 Peake on countdown – to the ISS and beyond Production Assistant: As British astronaut Tim Peake gets ready for his ride into space, Ben Jones Spaceflight reviews the build-up to this mission and examines the Spaceflight Promotion: possibilities that may unfold as a result of European contributions to Suszann Parry NASA’s Orion programme. Spaceflight Arthur C. Clarke House, 6-9 Ready to go! 27/29 South Lambeth Road, London, SW8 1SZ, England. What happens when Tim Peake arrives at the International Space Tel: +44 (0)20 7735 3160 Station, where can I watch it, listen to it, follow it, and what are the Fax: +44 (0)20 7582 7167 broadcasters doing about special programming? We provide the Email: [email protected] directory to a media frenzy! www.bis-space.com 16-17 BIS Technical Projects ADVERTISING Tel: +44 (0)1424 883401 Robin Brand has been busy gathering the latest information about Email: [email protected] studies, research projects and practical experiments now underway at DISTRIBUTION the BIS, the first in a periodic series of roundups. Spaceflight may be received worldwide by mail through membership of the British 18 Icarus Progress Report Interplanetary Society. -
Wubbo Ockels Spaceup NL Chinese Raketten Van De Hoofdredacteur
Ruimteweer Wubbo Ockels SpaceUp NL Chinese raketten Van de hoofdredacteur: Een van de uitkomsten van de ledenenquête was dat er interesse is voor speciale uitgaven van Ruimtevaart rond een bepaald thema. De uitslag gaf aan dat 36% van de respondenten het leuk zou vinden als er een speciale uitgave kwam bij bijzondere gelegenheden en 44% was voor één speciale uitgave per jaar. Binnen de redactie hebben we uitgebreid besproken hoe we deze wens kunnen invullen met in achtneming van de keuze uit 2012 om dikkere Ruimtevaartnummers te maken met een lagere uitgavefrequentie. We zijn tot de conclusie gekomen dat dit het beste kan door middel van een Dossier: een aantal Bij de voorplaat artikelen rond een bepaald thema die in een reguliere uitgave opgenomen wordt. In dit nummer vindt u het eerste Dossier met Het noorderlicht is een spectaculair aspect van ruimteweer. De foto als bedroevende aanleiding het overlijden van Wubbo Ockels. is gemaakt door Ole Salomonsen in het Noorse Kattfjordeidet op We hebben een aantal mensen gevraagd om hun herinneringen 30 oktober 2013 toen de aarde geraakt werd door een Coronal Mass aan Wubbo op te schrijven. Ejection. De foto is genomineerd voor de astronomische foto van het jaar 2014. Op 2 september heeft de NVR ook een event in het Een andere uitslag van de enquête was dat onze leden interesse Omniversum over SolarMax & het poollicht georganiseerd. hebben in wat er gebeurt op ruimtevaartgebied buiten Europa en in het bijzonder China werd dan vaak genoemd. Oud- hoofdredacteur Henk Smid heeft daarom een tweedelig artikel geschreven wat een overzicht geeft van het verleden, heden en toekomst van de Chinese draagraketten. -
Phonesat the Smartphone Nanosatellite
PhoneSat The Smartphone Nanosatellite NASA’s PhoneSat project tests whether To do this, the PhoneSat design makes spacecraft can be built using smartphones extensive use of commercial-off-the-shelf to launch the lowest-cost satellites ever components, including a smartphone. flown in space. Each PhoneSat nanosatellite Smartphones offer a wealth of capabilities is one cubesat unit - a satellite in a 10 cm needed for satellite systems such as fast cube (approx. 4 inches) or about the size of processors, versatile operating systems, a tissue box - and weighs approximately 1 multiple miniature sensors, high-resolution kg (2.2 pounds). Engineers believe PhoneSat technology will enable NASA to launch cameras, GPS receivers, and several radios. multiple new satellites capable of conducting PhoneSat engineers also are changing the science and exploration missions at a small way missions are designed by prototyping fraction of the cost of conventional satellites. and incorporating existing commercial The small teams of NASA engineers technologies and hardware to see what supporting PhoneSat at NASA’s Ames capabilities they can provide, rather than Research Center, Moffett Field, Calif., aim trying to custom-design technology to rapidly evolve satellite architecture and solutions to meet set requirements. incorporate the Silicon Valley approach PhoneSat 1.0 demonstrated that low-cost, of “release early, release often,” adding modern electronics can fly in space. It was new functionality to the satellite with each built around the Nexus One smartphone succeeding iteration. made by HTC Corp., running Google’s Left image: The PhoneSat 1.0 cubesat bus with a smartphone inside. Image credit: Ben Howard. -
IAC-17-#### Page 1 of 6 IAC-17-### Crowdfunding for Space Missions
68th International Astronautical Congress (IAC), Adelaide, Australia, 25-29 September 2017. Copyright ©2017 by the International Astronautical Federation (IAF). All rights reserved. IAC-17-### Crowdfunding For Space Missions Graham Johnsona a Inmarsat Global Ltd. [email protected] Abstract Crowdfunding (via websites such as kickstarter.com) has become an increasingly popular method for funding projects and start-up companies for a wide range of terrestrial products and services. A small, but not insignificant number of space projects have also used this method of fundraising, and there is potentially much greater scope for this type of funding. This paper presents an analysis of crowd-funding campaigns that have been used to fund space- related projects, and in particular, spaceflight missions. It assesses the relative success of these campaigns and proposes some insights as to what makes a successful space crowdfunding campaign. Keywords: Crowdfunding, Space, Mission Acronyms/Abbreviations have attempted to use crowdfunding as either their CAT Cubesat Ambipolar Thruster principle source of funding, or as a stepping stone to ISS International Space Station further progress their project. Kickstarter appears to be LEO Low Earth Orbit the most popular platform for space mission funding, although there have also been a small number of space projects on IndieGoGo, Rockethub and Gofundme. 1. Introduction In this paper a summary of space mission ‘Crowdfunding’ is a process by which the creator of crowdfunding campaigns is presented, an assessment is a product or service can appeal directly to the public for made of the typical level of funding which individuals cash funding. It is important to note that the contribute, and the potential for scale-up to future space contributors, or ‘funders’, are not actually investing in projects is discussed.