The Future of Cubesat Communications
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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 2009 Mars Telecom Orbier Mission
The 2009 Mars Telecom Orbiter Mission1,2 Stephen F. Franklina, John P. Slonski, Jr.a, Stuart Kerridgea, Gary Noreena, Joseph E. Riedela, Tom Komareka, Dorothy Stosica, Caroline Rachoa, Bernard Edwardsb, Don Borosonc a-Jet Propulsion Laboratory, California Institute of Technology; Pasadena, Ca. 91109; b-NASA Goddard Spaceflight Center, Greenbelt, Md. 20771 USA c-MIT-Lincoln Laboratory, Lexington, Ma, 02420 Abstract—This paper provides an overview of the Mars Mission and flight system requirements have been written. Telecom Orbiter (MTO) mission, and is an update to the The flight system requirements define the flight system paper presented at last year’s conference. Launched in performance and functionality to the competing system 2009, MTO will provide Mars-to-Earth relay services for contract proposers. NASA missions arriving at Mars between 2010 and 2020, enabling far higher science data return and lowering the A Rendezvous and Autonomous Navigation (RAN) telecom and operations costs for these missions. MTO demonstration has been added. An orbiting sample canister carries an optical communications payload, which will will be released and tracked by the ground using on-board demonstrate downlink bit rates from 1 Mbps up to and cameras. The spacecraft will then rendezvous with the possibly exceeding 30 Mbps. MTO will also demonstrate canister using its autonomous navigation capability, coming the ability to autonomously navigate, and to search for and to within ten meters of (but not capturing) the canister. This rendezvous with an orbiting sample, in preparation for operation demonstrates capabilities that the proposed NASA NASA’s proposed Mars Sample Return Mission. A to-be- Mars Sample Return orbiter will require to capture the Mars defined science instrument will also be carried. -
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. -
In This Issue
Vol. 38 No.12, September 2013 Editor: Jos Heyman FBIS In this issue: Satellite Update 4 Cancelled projects: Conestoga 5 News Ardusat 3 Arirang-5 7 Dnepr 1 7 Dream Chaser 7 Eutelsat and Satmex 2 Fermi 7 Gsat-14 7 HTV-4 3 iBall 3 Kepler 4 Orion 7 PicoDragon 3 Proton M 2 RCM 2 Russian EVAs 2 SARah 4 SGDC-1 4 SPRINT A 4 TechEdSat-3 3 WGS-6 4 HTV-4 Unpressurised Logistics Carrier with STP-H4 TIROS SPACE INFORMATION Eutelsat and Satmex 86 Barnevelder Bend, Southern River WA 6110, Australia Tel + 61 8 9398 1322 Eutelsat has acquired Mexico’s Satmex, a major communicaions satellite operator in the Latin (e-mail: [email protected]) American region. o o The Tiros Space Information (TSI) - News Bulletin is published to promote the scientific exploration and Satmex has currently three satellites in orbit at 113 W (Satmex-6), 114.9 W (Satmex-5) and commercial application of space through the dissemination of current news and historical facts. 116.8 oW (Satmex-8) and it can be expected that, once the acquisition has been completed, In doing so, Tiros Space Information continues the traditions of the Western Australian Branch of the these satellites will be renamed as part of the Eutelsat family. In addition Satmex has the Astronautical Society of Australia (1973-1975) and the Astronautical Society of Western Australia (ASWA) Satmex-7 and -9 satellites on order from Boeing. It is not clear whether these satellites will (1975-2006). remain on order. The News Bulletin can be received worldwide by e-mail subscription only. -
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. -
Starttabelle 2013 2013-01A 2013-01B 2013-01C 2013-02A 2013-02B 2013-03A 2013-04A NOA-01 2013-05A 2013-05B 2013-05C 2013-05D 2013-05E 2013-05F 2013-06A 2013-06B
Raumfahrer.net Starttabelle 2013 Bahnnähe Bahnferne Inklination LandLandLand bzw.bzw.bzw. WiederWieder---- COSPAR Satellit StartStartStart (GMT) Trägerrakete Startort Umläuft Bemerkungen Bemannt (km)(km)(km) (km)(km)(km) (Grad) Organisation eintritt 2013-01A Kosmos 2482 15.01.2013 Rokot Plesezk 1.484 1.523 82,504 Erde Russland - Militärischer Datenrelais- Nein (Strela-3M 4) 16.25 satellit 2013-01B Kosmos 2483 15.01.2013 Rokot Plesezk 1.485 1.510 82,505 Erde Russland - Militärischer Datenrelais- Nein (Strela-3M 5) 16.25 satellit 2013-01C Kosmos 2484 15.01.2013 Rokot Plesezk 1.484 1.523 82,504 Erde Russland - Militärischer Datenrelais- Nein (Strela-3M 6) 16.25 satellit 2013-02A IGS-Radar 4 27.01.2013 H2-A Tanegashima 480 500 97 Erde Japan - Radar-Aufklärungssatellit Nein 4.40 2013-02B IGS-Optik 5V 27.01.2013 H2-A Tanegashima 480 500 97 Erde Japan - Optischer Aufklärungs- Nein 4.40 satellit 2013-03A STSat 2C 30.01.2013 Naro 1 Naro-Raumfahrt- 304 1.509 80,275 Erde Südkorea - Forschungs- und Technolo- Nein 7.00 zentrum giesatellit; ca. 100 kg 2013-04A TDRS K 31.01.2013 Atlas 5 Cape Canaveral 35.744 35.845 6,998 Erde USA - Bahnverfolgungs- und Nein 1.48 Datenrelaissatellit; 3.454 kg NOA-01 Intelsat 27 01.02.2013 Zenit 3 Sea-Launch-Plattform - - - - USA - Fehlfunktion der ersten Nein 7.56 Stufe und Absturz 2013-05A Globalstar M78 06.02.3013 Sojus 2 Baikonur 1.420 1.421 52,004 Erde USA - Sprach- und Datenkommu- Nein 16.04 nikationssatellit; 700 kg 2013-05B Globalstar M93 06.02.3013 Sojus 2 Baikonur 1.420 1.421 51,980 Erde USA - Sprach- und Datenkommu- -
Changes to the Database Document
Additions and Deletions for the 12-1-18 Release This version of the Database includes launches through November 30, 2018. There are currently 1,957 active satellites in the database. The changes to this version of the database include: • The addition of 141satellites • The deletion of 71 satellites • The addition of and corrections to some satellite data Satellites Removed Echostar-1 – 1995-073A Palapa C2 -- 1996-030A Measat-2 – 1996-063B Iridium 12 – 1997-030B Iridium 10 – 1997-030D Iridium 15 – 1997-034A Iridium 18 -- 1997-034D ABS-3 -- 1997-042A Iridium 25 – 1997-043B Iridium 37 – 1997-056D Iridium 41 – 1997-069B JCSat-1B – 1997-075A Iridium 47 – 1997-082C Globalstar FM4 – 1998-008B Iridium 52 – 1998-010A Iridium 56 – 1998-010B Iridium 50 – 1998-010D Iridium 53 – 1998-010E Iridium 62 -- 1998-021A Iridium 65 – 1998-021D Iridium 66 – 1998-021E Iridium 67 – 1998-021F Iridium 68 – 1998-021G Iridium 72 – 1998-032B Iridium 75 – 1998-032E Iridium 76 – 1998-048B Iridium 81 – 1998-051B Iridium 80 – 1998-051C Iridium 86 – 1998-066B Iridium 84 – 1998-066D Iridium 83 – 1998-066E Dove 2e-1 – 1998-067JD Dove 2e-5 – 1998-067JN Dove 2ep-5 – 1998-067JR Dove 2ep-14 – 1998-067KJ Dove 2ep-15 – 1998-067KL Dove 2ep-17 – 1998-067KN Dove 2ep-18 – 1998-067KM Dove 23p-20 – 1998-067KP Dove 2ep-19 – 1998-067KQ Lemur-2F20 -- 1998-067LD i-INSPIRE-2 – 1998-067ML Tomsk-TPU-120 -- 1998-067MZ Tanyusha 1 -- 1998-067NA Tanyusha 2 -- 1998-067NB TNS-0-2 Nanosputnik -- 1998-067ND SIMPL – 1998-067NF Iridium 20A – 1998-074A Iridium 11A – 1998-074B Globalstar M023 – 1999-004A -
The Annual Compendium of Commercial Space Transportation: 2017
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2017 January 2017 Annual Compendium of Commercial Space Transportation: 2017 i Contents 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 (2017) Publication produced for FAA AST by The Tauri Group under contract. 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. ii Annual Compendium of Commercial Space Transportation: 2017 GENERAL CONTENTS Executive Summary 1 Introduction 5 Launch Vehicles 9 Launch and Reentry Sites 21 Payloads 35 2016 Launch Events 39 2017 Annual Commercial Space Transportation Forecast 45 Space Transportation Law and Policy 83 Appendices 89 Orbital Launch Vehicle Fact Sheets 100 iii Contents DETAILED CONTENTS EXECUTIVE SUMMARY . -
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.