State of the Art Small Spacecraft Technology 2018
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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, -
Minimum Dietary Diversity for Women a Guide to Measurement
FANTA III FOOD AND NUTRITION TECHNICAL A SSISTANCE Minimum Dietary Diversity for Women A Guide to Measurement Minimum Dietary Diversity for Women A Guide to Measurement Published by the Food and Agriculture Organization of the United Nations and USAID’s Food and Nutrition Technical Assistance III Project (FANTA), managed by FHI 360 Rome, 2016 Recommended citation: FAO and FHI 360. 2016. Minimum Dietary Diversity for Women: A Guide for Measurement. Rome: FAO. The designations employed and the presentation of material in this information product do not imply the expression of any opinion whatsoever on the part of the Food and Agriculture Organization of the United Nations (FAO), or of FANTA/FHI 360 concerning the legal or development status of any country, territory, city or area or of its authorities, or concerning the delimitation of its frontiers or boundaries. The mention of specific companies or products of manufacturers, whether or not these have been patented, does not imply that these have been endorsed or recommended by FAO, or FHI 360 in preference to others of a similar nature that are not mentioned. Additional funding for this publication was made possible by the generous support of the American people through the support of the Office of Health, Infectious Diseases, and Nutrition, Bureau for Global Health, U.S. Agency for International Development (USAID), under terms of Cooperative Agreement AID-OAA-A-12-00005 through the Food and Nutrition Technical Assistance III Project (FANTA), managed by FHI 360. The views expressed in this information product are those of the author(s) and do not necessarily reflect the views or policies of FAO, FHI 360, UC Davis, USAID or the U.S. -
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. -
LCROSS (Lunar Crater Observation and Sensing Satellite) Observation Campaign: Strategies, Implementation, and Lessons Learned
Space Sci Rev DOI 10.1007/s11214-011-9759-y LCROSS (Lunar Crater Observation and Sensing Satellite) Observation Campaign: Strategies, Implementation, and Lessons Learned Jennifer L. Heldmann · Anthony Colaprete · Diane H. Wooden · Robert F. Ackermann · David D. Acton · Peter R. Backus · Vanessa Bailey · Jesse G. Ball · William C. Barott · Samantha K. Blair · Marc W. Buie · Shawn Callahan · Nancy J. Chanover · Young-Jun Choi · Al Conrad · Dolores M. Coulson · Kirk B. Crawford · Russell DeHart · Imke de Pater · Michael Disanti · James R. Forster · Reiko Furusho · Tetsuharu Fuse · Tom Geballe · J. Duane Gibson · David Goldstein · Stephen A. Gregory · David J. Gutierrez · Ryan T. Hamilton · Taiga Hamura · David E. Harker · Gerry R. Harp · Junichi Haruyama · Morag Hastie · Yutaka Hayano · Phillip Hinz · Peng K. Hong · Steven P. James · Toshihiko Kadono · Hideyo Kawakita · Michael S. Kelley · Daryl L. Kim · Kosuke Kurosawa · Duk-Hang Lee · Michael Long · Paul G. Lucey · Keith Marach · Anthony C. Matulonis · Richard M. McDermid · Russet McMillan · Charles Miller · Hong-Kyu Moon · Ryosuke Nakamura · Hirotomo Noda · Natsuko Okamura · Lawrence Ong · Dallan Porter · Jeffery J. Puschell · John T. Rayner · J. Jedadiah Rembold · Katherine C. Roth · Richard J. Rudy · Ray W. Russell · Eileen V. Ryan · William H. Ryan · Tomohiko Sekiguchi · Yasuhito Sekine · Mark A. Skinner · Mitsuru Sôma · Andrew W. Stephens · Alex Storrs · Robert M. Suggs · Seiji Sugita · Eon-Chang Sung · Naruhisa Takatoh · Jill C. Tarter · Scott M. Taylor · Hiroshi Terada · Chadwick J. Trujillo · Vidhya Vaitheeswaran · Faith Vilas · Brian D. Walls · Jun-ihi Watanabe · William J. Welch · Charles E. Woodward · Hong-Suh Yim · Eliot F. Young Received: 9 October 2010 / Accepted: 8 February 2011 © The Author(s) 2011. -
Constellation Program Overview
Constellation Program Overview October 2008 hris Culbert anager, Lunar Surface Systems Project Office ASA/Johnson Space Center Constellation Program EarthEarth DepartureDeparture OrionOrion -- StageStage CrewCrew ExplorationExploration VehicleVehicle AresAres VV -- HeavyHeavy LiftLift LaunchLaunch VehicleVehicle AltairAltair LunarLunar LanderLander AresAres II -- CrewCrew LaunchLaunch VehicleVehicle Lunar Capabilities Concept Review EstablishedEstablished Lunar Lunar Transportation Transportation EstablishEstablish Lunar Lunar Surface SurfaceArchitecturesArchitectures ArchitectureArchitecture Point Point of of Departure: Departure: StrategiesStrategies which: which: Satisfy NASA NGO’s to acceptable degree ProvidesProvides crew crew & & cargo cargo delivery delivery to to & & from from the the Satisfy NASA NGO’s to acceptable degree within acceptable schedule moonmoon within acceptable schedule Are consistent with capacity and capabilities ProvidesProvides capacity capacity and and ca capabilitiespabilities consistent consistent Are consistent with capacity and capabilities withwith candidate candidate surface surface architectures architectures ofof the the transportation transportation systems systems ProvidesProvides sufficient sufficient performance performance margins margins IncludeInclude set set of of options options fo for rvarious various prioritizations prioritizations of cost, schedule & risk RemainsRemains within within programmatic programmatic constraints constraints of cost, schedule & risk ResultsResults in in acceptable -
Imagining Outer Space Also by Alexander C
Imagining Outer Space Also by Alexander C. T. Geppert FLEETING CITIES Imperial Expositions in Fin-de-Siècle Europe Co-Edited EUROPEAN EGO-HISTORIES Historiography and the Self, 1970–2000 ORTE DES OKKULTEN ESPOSIZIONI IN EUROPA TRA OTTO E NOVECENTO Spazi, organizzazione, rappresentazioni ORTSGESPRÄCHE Raum und Kommunikation im 19. und 20. Jahrhundert NEW DANGEROUS LIAISONS Discourses on Europe and Love in the Twentieth Century WUNDER Poetik und Politik des Staunens im 20. Jahrhundert Imagining Outer Space European Astroculture in the Twentieth Century Edited by Alexander C. T. Geppert Emmy Noether Research Group Director Freie Universität Berlin Editorial matter, selection and introduction © Alexander C. T. Geppert 2012 Chapter 6 (by Michael J. Neufeld) © the Smithsonian Institution 2012 All remaining chapters © their respective authors 2012 All rights reserved. No reproduction, copy or transmission of this publication may be made without written permission. No portion of this publication may be reproduced, copied or transmitted save with written permission or in accordance with the provisions of the Copyright, Designs and Patents Act 1988, or under the terms of any licence permitting limited copying issued by the Copyright Licensing Agency, Saffron House, 6–10 Kirby Street, London EC1N 8TS. Any person who does any unauthorized act in relation to this publication may be liable to criminal prosecution and civil claims for damages. The authors have asserted their rights to be identified as the authors of this work in accordance with the Copyright, Designs and Patents Act 1988. First published 2012 by PALGRAVE MACMILLAN Palgrave Macmillan in the UK is an imprint of Macmillan Publishers Limited, registered in England, company number 785998, of Houndmills, Basingstoke, Hampshire RG21 6XS. -
ATHENA COMMUNITY NEWSLETTER #4 December 2017 Contents
ATHENA COMMUNITY NEWSLETTER #4 December 2017 Contents Welcome.......................................................................................... 1 Fourth Announcement of Opportunity to join the Athena Community Working Groups/Topical Panels .................................................... 1 Discovery of Electromagnetic Counterparts to Gravitational Waves .......... 2 Athena Project Status .......................................................................... 2 News from the Instruments ................................................................. 4 News from the WFI ......................................................................... 4 News from X-IFU ............................................................................ 4 The SKA-Athena Synergy Exercise Coming to the End.............................. 6 Athena End-to-End Simulations ............................................................ 7 Unveiling the Hot, High Redshift Universe with the Athena WFI ................. 8 Athena Community People .................................................................. 9 Conferences ................................................................................... 10 Athena in Conferences (January-July 2018) ....................................... 10 Coming conferences of interest ...................................................... 10 Edited by Athena Community Office: F.J. Carrera, M.T. Ceballos, S. Martínez-Núñez, M.P. Monterde Instituto de Física de Cantabria (CSIC-UC) Avda Los Castros s/n 39005 Santander -
Analysis of Atmosphere-Breathing Electric Propulsion
Analysis of Atmosphere-Breathing Electric Propulsion IEPC-2013-421 Presented at the 33rd International Electric Propulsion Conference, The George Washington University, Washington, D.C., USA October 6{10, 2013 Tony Sch¨onherr,∗ and Kimiya Komurasakiy The University of Tokyo, Bunkyo, Tokyo, 113-8656, Japan and Georg Herdrichz University of Stuttgart, Stuttgart, Baden-W¨urttemberg, 70569, Germany To extend lifetime of commercial and scientific satellites in LEO and below (100-250 km of altitude) the recent years showed an increased activity in the field of air-breathing electric propulsion as well as beamed-energy propulsion systems. However, preliminary studies showed that the propellant flow necessary for electrostatic propulsion exceeds the mass intake possible within reasonable limits, and that electrode erosion due to oxygen flow might limit the lifetime of eventual thruster systems. Pulsed plasma thruster can be successfully operated with smaller mass intake, and operate at relatively small power demands which makes them an interesting candidate for air-breathing application in LEO, and their feasibility is investigated within this study. Further, to avoid electrode erosion, inductive plasma generator technology is discussed to derive a possible propulsion system that can handle gaseous propellant with no harmful effects. Nomenclature E = discharge energy per pulse FD = drag force imposed on satellite f = discharge frequency h = orbital altitude mbit = mass shot per pulse n = number density t = orbital lifetime I. Introduction Carrying propellant for attitude and orbit control on satellites in an Earth orbit results in an increased satellite mass, and, therefore, yields higher costs for manufacturing and launch of the spacecraft. Electric space propulsion helped in the past to reduce the mass requirements compared to standard chemical propul- sion as a result of the superior specific impulse, but limitations remain with regards to lifetime and lower ∗Assistant Professor, Department of Aeronautics and Astronautics, [email protected]. -
Space Industry Bulletin January 2019
VOLUME 2 • ISSUE 1 www.spaceindustrybulletin.com Space Industry Bulletin Market analysis and business intelligence for the space community Space Industry Act heralds UK sovereign launch capability ith the granting of The SIA is intended to create Indeed, to this end, the bulk of Royal Assent to the the necessary legal framework the SIA resembles a piece of WSpace Industry Act for the expansion and growth of planning legislation. CONTENTS 2018, the UK is taking legislative the UK space industry. The However, turning to the new steps to regain sovereign launch drafters of the legislation have licencing and liability regime, Industry news 2 l Boeing invests in Isotropic capacity. The Space Industry tried to respond to the demands there is no detail in the Act ex - Systems Act (SIA) represents an of the space industry, sacrificing plaining how this will operate in l Contract to develop ambitious attempt to re- detail and scrutiny upfront for practice. It appears that such constellation satellite bus awarded establish independent launch flexibility in the future. operational matters will be to Airbus capacity and a launch facility Significantly the SIA provides fleshed out by means of dele - l Sector deal questions iraised in the House of Commons within the UK to complement its authority and the bare bones of gated legislation. l ‘Managed’ no-deal Brexit won’t burgeoning small satellite a regulatory framework for the The draft regulations for these be enough industry. authorisation of launches from delegated powers have not yet l First satellite capable of being within the UK. There is provision been promulgated and this lack reprogrammed after launch leaves the UK for assembly and test within the SIA for the creation of detail provoked some contro - l Global defence spending rises at and management of spaceports. -
Managing Supply Chain Risks in an International Organisation - European Space Agency
Managing Supply Chain Risks in an International Organisation - European Space Agency Britta Schade 23/10/2018 ESA UNCLASSIFIED - For Official Use ESA Facts and Figures . Over 50 years of experience . 22 Member States . Eight sites/facilities in Europe, about 2300 staff . 5.75 billion Euro budget (2017) . Over 80 satellites designed, tested and operated in flight ESA UNCLASSIFIED - For Official Use Britta Schade | ESA-TECQ-HO-011192 | ESTEC | 23/10/2018 | Slide 2 Purpose of ESA “To provide for and promote, for exclusively peaceful purposes, cooperation among European states in space research and technology and their space applications.” Article 2 of ESA Convention ESA UNCLASSIFIED - For Official Use Britta Schade | ESA-TECQ-HO-011192 | ESTEC | 23/10/2018 | Slide 3 Member States ESA has 22 Member States: 20 states of the European Union (Austria, Belgium, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Ireland, Italy, Luxembourg, Netherlands, Poland, Portugal, Romania, Sweden, United Kingdeom) plus Norway and Switzerland. Six other European Union (EU) states have Cooperation Agreements with ESA: Bulgaria, Cyprus, Latvia, Lithuania, Malta and Slovakia. Discussions are ongoing with Croatia. Slovenia is an Associate Member. Canada takes part in some programmes under a long-standing Cooperation Agreement. ESA UNCLASSIFIED - For Official Use Britta Schade | ESA-TECQ-HO-011192 | ESTEC | 23/10/2018 | Slide 4 ESA Locations Salmijaervi (Kiruna) Moscow Brussels ESTEC (Noordwijk) ECSAT (Harwell) EAC (Cologne) Washington Maspalomas Houston ESA HQ (Paris) ESOC (Darmstadt) Santa Maria Oberpfaffenhofen Kourou Toulouse New Norcia ESEC (Redu) Malargüe ESAC (Madrid) ESRIN (Rome) ESA sites Cebreros Offices ESA Ground Station + Offices ESA Ground Station ESA sites + ESA Ground Station ESA UNCLASSIFIED - For Official Use Britta Schade | ESA-TECQ-HO-011192 | ESTEC | 23/10/2018 | Slide 5 Activities space science human spaceflight exploration ESA is one of the few space agencies in the world to combine responsibility in nearly all areas of space activity. -
Herman IEPC-2019-651 PPE IPS Final
The Application of Advanced Electric Propulsion on the NASA Power and Propulsion Element (PPE) IEPC-2019-651 Presented at the 36th International Electric Propulsion Conference University of Vienna • Vienna • Austria September 15 – 20, 2019 Daniel A. Herman,1 Timothy Gray,2 NASA Glenn Research Center, Cleveland, OH, 44135, United States and Ian Johnson,3 Taylor Kerl,4 Ty Lee,5 and Tina Silva6 Maxar, Palo Alto, CA, 94303, United States Abstract: NASA is charGed with landinG the first American woman and next American man on the South Pole of the Moon by 2024. To meet this challenGe, NASA’s Gateway will develop and deploy critical infrastructure required for operations on the lunar surface and that enables a sustained presence on and around the moon. NASA’s Power and Propulsion Element (PPE), the first planned element of NASA’s cis-lunar Gateway, leveraGes prior and ongoing NASA and U.S. industry investments in high-power, long-life solar electric propulsion technoloGy investments. NASA awarded a PPE contract to Maxar TechnoloGies to demonstrate a 2,500 kg xenon capacity, 50 kW-class SEP spacecraft that meets Gateway’s needs, aligns with industry’s heritage spacecraft buses, and allows extensibility for NASA’s Mars exploration Goals. Maxar’s PPE concept desiGn, is based on their hiGh heritaGe, modular, and highly reliable 1300-series bus architecture. The electric propulsion system features two 13 kW Advanced Electric Propulsion (AEPS) strings from Aerojet Rocketdyne and a Maxar- developed system comprised of four Busek 6 kW Hall-effect thrusters mounted in pairs on larGe ranGe of motion mechanisms pointing arms with four 6 kW-class, Maxar-built PPUs derived from Geostationary Earth Orbit (GEO) heritage. -
List of Missions Using SPICE (PDF)
1/7/20 Data Restorations Selected Past Users Current/Pending Users Examples of Possible Future Users Apollo 15, 16 [L] Magellan [L] Cassini Orbiter NASA Discovery Program Mariner 2 [L] Clementine (NRL) Mars Odyssey NASA New Frontiers Program Mariner 9 [L] Mars 96 (RSA) Mars Exploration Rover Lunar IceCube (Moorehead State) Mariner 10 [L] Mars Pathfinder Mars Reconnaissance Orbiter LunaH-Map (Arizona State) Viking Orbiters [L] NEAR Mars Science Laboratory Luna-Glob (RSA) Viking Landers [L] Deep Space 1 Juno Aditya-L1 (ISRO) Pioneer 10/11/12 [L] Galileo MAVEN Examples of Users not Requesting NAIF Help Haley armada [L] Genesis SMAP (Earth Science) GOLD (LASP, UCF) (Earth Science) [L] Phobos 2 [L] (RSA) Deep Impact OSIRIS REx Hera (ESA) Ulysses [L] Huygens Probe (ESA) [L] InSight ExoMars RSP (ESA, RSA) Voyagers [L] Stardust/NExT Mars 2020 Emmirates Mars Mission (UAE via LASP) Lunar Orbiter [L] Mars Global Surveyor Europa Clipper Hayabusa-2 (JAXA) Helios 1,2 [L] Phoenix NISAR (NASA and ISRO) Proba-3 (ESA) EPOXI Psyche Parker Solar Probe GRAIL Lucy EUMETSAT GEO satellites [L] DAWN Lunar Reconnaissance Orbiter MOM (ISRO) Messenger Mars Express (ESA) Chandrayan-2 (ISRO) Phobos Sample Return (RSA) ExoMars 2016 (ESA, RSA) Solar Orbiter (ESA) Venus Express (ESA) Akatsuki (JAXA) STEREO [L] Rosetta (ESA) Korean Pathfinder Lunar Orbiter (KARI) Spitzer Space Telescope [L] [L] = limited use Chandrayaan-1 (ISRO) New Horizons Kepler [L] [S] = special services Hayabusa (JAXA) JUICE (ESA) Hubble Space Telescope [S][L] Kaguya (JAXA) Bepicolombo (ESA, JAXA) James Webb Space Telescope [S][L] LADEE Altius (Belgian earth science satellite) ISO [S] (ESA) Armadillo (CubeSat, by UT at Austin) Last updated: 1/7/20 Smart-1 (ESA) Deep Space Network Spectrum-RG (RSA) NAIF has or had project-supplied funding to support mission operations, consultation for flight team members, and SPICE data archive preparation.