Navy Space and Astronautics Orientation. INSTITUTION Bureau of Naval Personnel, Washington, D
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Small Spacecraft Programs
Planetary Science Deep Space SmallSat Studies Small Spacecraft Programs Carolyn Mercer Program Officer, PSDS3 Program Executive, SIMPLEx NASA Glenn Research Center Briefing to the Mars Exploration Program Analysis Group (MEPAG) April 4, 2018 Crystal City, VA NOTE ADDED BY JPL WEBMASTER: This content has not been approved or adopted by NASA, JPL, or the California Institute of Technology. This document is being made available for information purposes only, and any views and opinions expressed herein do not necessarily state or reflect those of NASA, JPL, or the 1 California Institute of Technology. SMD CubeSat/SmallSat Approach Planetary Science Deep Space SmallSat Studies National Academies Report (2016) concluded that CubeSats have proven their ability to produce high- value science: • Useful as targeted investigations to augment the capabilities of larger missions • Useful to make highly-specific measurements • Constellations of 10-100 CubeSat/SmallSat spacecraft have the potential to enable transformational science SMD is developing a directorate-wide approach to: • Identify high-priority science objectives in each discipline that can be addressed with CubeSats/SmallSats • Manage program with appropriate cost and risk • Establish a multi-discipline approach and collaboration that helps science teams learn from experiences and grow capability, while avoiding unnecessary duplication • Leverage and partner with a growing commercial sector to collaboratively drive instrument and sensor innovation 2 PLANETARY SCIENCE DEEP SPACE SMALLSAT -
Istanbul Technical University Institute of Science And
İSTANBUL TECHNICAL UNIVERSITY « INSTITUTE OF SCIENCE AND TECHNOLOGY DESIGN STUDY OF A COMMUNICATION SUBSYSTEM AND GROUND STATION FOR ITU-pSAT II M.Sc. Thesis by Melih FİDANOĞLU Department : Institue of Science and Technology Programme : Defence Technologies JANUARY 2011 İSTANBUL TECHNICAL UNIVERSITY « INSTITUTE OF SCIENCE AND TECHNOLOGY DESIGN STUDY OF A COMMUNICATION SUBSYSTEM AND GROUND STATION FOR ITU-pSAT II M.Sc. Thesis by Melih FİDANOĞLU (514071013) Date of submission : 20 December 2010 Date of defence examination: 24 January 2011 Supervisor (Chairman) : Assoc. Prof. Dr. Gökhan İNALHAN (ITU) Members of the Examining Committee : Prof. Dr. İbrahim ÖZKOL (ITU) Prof. Dr. Metin Orhan KAYA (ITU) JANUARY 2011 İSTANBUL TEKNİK ÜNİVERSİTESİ « FEN BİLİMLERİ ENSTİTÜSÜ ITU-pSAT II İÇİN İLETİŞİM ALTSİSTEMİ VE YER İSTASYONU TASARIM ÇALIŞMASI YÜKSEK LİSANS TEZİ Melih FİDANOĞLU (514071013) Tezin Enstitüye Verildiği Tarih : 20 Aralık 2010 Tezin Savunulduğu Tarih : 24 Ocak 2011 Tez Danışmanı : Doç. Dr. Gökhan İnalhan (İTÜ) Diğer Jüri Üyeleri : Prof. Dr. İbrahim Özkol (İTÜ) Prof. Dr. Metin Orhan Kaya (İTÜ) OCAK 2011 FOREWORD First of all, I would like to thank my advisor, Gökhan İnalhan for the opportunity to work in the fantastic setup of Control and Avionics Laboratory and to work with the research team here. I would like to thank ITU-pSAT II project team including Emre Koyuncu, Melahat Cihan, Elgiz Başkaya and Soner Işıksal for being my project teammates. Also, my sincere thanks goes to Control and Avionics Lab's fellow labmates, including, but not limited to, Serdar Ateş, Oktay Arslan and Nazım Kemal Üre. A special thanks goes to TÜBİTAK. Without their contributions, this project would not be possible. -
Maxar Technologies with Respect to Future Events, Financial Performance and Operational Capabilities
Leading Innovation in the New Space Economy Howard L. Lance President and Chief Executive Officer Forward-Looking Statement This presentation contains forward-looking statements and information, which reflect the current view of Maxar Technologies with respect to future events, financial performance and operational capabilities. The forward-looking statements in this presentation include statements as to managements’ expectations with respect to: the benefits of the transaction and strategic and integration opportunities; the company’s plans, objectives, expectations and intentions; expectations for sales growth, synergies, earnings and performance; shareholder value; and other statements that are not historical facts. Although management of the Company believes that the expectations and assumptions on which such forward-looking statements are based are reasonable, undue reliance should not be placed on the forward-looking statements because the Company can give no assurance that they will prove to be correct. Any such forward-looking statements are subject to various risks and uncertainties which could cause actual results and experience to differ materially from the anticipated results or expectations expressed in this presentation. Additional information concerning these risk factors can be found in the Company’s filings with Canadian securities regulatory authorities, which are available online under the Company’s profile at www.sedar.com, the Company’s filings with the United States Securities and Exchange Commission, or on the Company’s website at www.maxar.com, and in DigitalGlobe’s filings with the SEC, including Item 1A of DigitalGlobe’s Annual Report on Form 10-K for the year ended December 31, 2016. The forward-looking statements contained in this presentation are expressly qualified in their entirety by the foregoing cautionary statements and are based upon data available as of the date of this release and speak only as of such date. -
Sistema De Evaluación De Aprendizajes Para Alumnos En Situación De Extraedad
Estrategia Integral para la Mejora del Logro Educativo Alianza por la Calidad de la Educación Sistema de evaluación de aprendizajes para alumnos en situación de extraedad Colección Hacia el Logro Educativo Programa para el Fortalecimiento del Logro Educativo Sistema de evaluación de aprendizajes para alumnos en situación de extraedad Colección Hacia el Logro Educativo Sistema de evaluación de aprendizajes para alumnos en situación de extraedad,es una publicación de la Dirección General de Desarrollo de la Gestión e Innovación Educativa de la Subsecretaría de Educación Básica, realizada a través del Proyecto para Atender a la Población en Situación de Extraedad, por encargo a la Organización de Estados Iberoamericanos para la Educación, la Ciencia y la Cultura (OEI) y con la colaboración del Centro de Estudios Educativos (CEE). Alonso Lujambio Secretario de Educación Pública José Fernando González Sánchez Subsecretario de Educación Básica Coordinación general Alma Rosa Cuervo González Juan Martín Martínez Becerra Cuidado de la edición Director General de Desarrollo de la Gestión Esteban Manteca Aguirre e Innovación Educativa Jorge Humberto Miranda Vázquez Tonatiuh Arroyo Cerezo Ernesto Adolfo Ponce Rodríguez Coordinador General de Innovación Colaboradores de la Ofi cina de la Organización de Estados Iberoamericanos para la Educación, la Ciencia y la Cultura y autores de esta obra Lilia Dalila López Salmorán Coordinadora Nacional para el Fortalecimiento Coordinación del Logro Educativo Carlos Niembro Acosta Colaboradores Teresa Zamudio Gisela Santiago Benítez Maura Pompa Mancilla D.R. © Secretaría de Educación Pública, 2011 Diana Gómez Mayén Argentina 28 Col. Centro Histórico C.P. 06020, México, D.F. ISBN: 978-607-8017-53-9 Diseño y formación Constantine Editores, S. -
Explore Science
SMALL SATELLITE MISSIONS FOR PLANETARY SCIENCE Carolyn R. Mercer, Ph.D. Program Executive, Small Innovative Missions for Planetary Exploration (SIMPLEx) AIAA Small Spacecraft Missions Conference August 4, 2019 Logan, Utah Apollo 15 Particles and Fields Subsatellite (PFS-1) • 35 kg spacecraft flown with Apollo 15 in 1971 • Orbited the Moon for 6 months • Science mission: • Measured the strength and direction of interplanetary and terrestrial magnetic fields • Detected variations in the lunar gravity field • Measured proton and electron flux 2 NASA SCIENCE AN INTEGRATED PROGRAM Helio- Earth physics Science Planetary Astrophysics Science Joint Agency Satellite Division 4 Small Spacecraft for Planetary Science Astrobiology Science and Technology Instrument Development (ASTID) 2008 • O/OREOS (2010 launch) Small Innovative Missions for Planetary Exploration (SIMPLEx-1) 2014 • LunaH-Map, Q-PACE Directed and Partnered Secondary Payloads • MarCO (2018 launch) • LICIA Cube (2021) – potential ASI contribution Planetary Science Deep Space SmallSat Studies (PSDS3) 2017 • 19 Studies – Presented March 2018 at LPSC Small Innovative Missions for Planetary Exploration (SIMPLEx-2) 2018 • Janus, Escapade, Lunar Trailblazer • Next proposals due no earlier than June 2020 5 Planetary Science Deep Space SmallSat Studies Solicitation requested: • Concepts for planetary science missions • 180 kg total spacecraft mass limit • $100M cost cap • No constraints on rides, infrastructure, etc. Solicitation sought answers to: • Can deep space missions be credibly done -
Appendix I Radio Regulations Provisions
Appendix I Radio Regulations Provisions E. D'Andria I. Introduction We summarize the Radio Regulations provisions and pertinent CCIR recommen dations and reports which give a more complete description of frequency sharing. To permit development of the fixed-satellite service (FSS), one of the last services introduced into the Radio Regulations, several technical and administra tive rules have been established to guarantee the compatibility of this new service with existing ones having the same frequency allocations. The very first rules were evolved by the Extraordinary Administrative Radio Conference for space radio communications, held in Geneva in 1963, and included in the Radio Regulations. The growing demand for space radio-communication services led the World Administrative Radio Conference for Space Telecommunications, WARC ST 1971, to revise and broaden previous frequency allocations and to produce improved technical criteria for frequency-sharing and coordination procedures. The WARC-1979 revision produced the provisions now in force; WARC- 1979 also resolved to hold a conference on the use of the GEO and planning of the space services utilizing it. The first session, held in 1985 (WARC-ORB '85), identified the frequency bands allocated to space services, plus principles and methods for planning to guarantee to all countries equal access to the GEO. The second session, held in 1988 (WARC-ORB '88), defined an allotment plan which specifies for each country the satellite nominal orbital position within a predetermined arc, the satellite beam characteristics, including geographical coordinates of the bore sight , and the satellite and earth stations EIRP densities. Each allotment is to have an aggregate C / I of at least 26 dB, although, when considering existing systems, in some cases this value is not reached. -
Orbital Debris: a Chronology
NASA/TP-1999-208856 January 1999 Orbital Debris: A Chronology David S. F. Portree Houston, Texas Joseph P. Loftus, Jr Lwldon B. Johnson Space Center Houston, Texas David S. F. Portree is a freelance writer working in Houston_ Texas Contents List of Figures ................................................................................................................ iv Preface ........................................................................................................................... v Acknowledgments ......................................................................................................... vii Acronyms and Abbreviations ........................................................................................ ix The Chronology ............................................................................................................. 1 1961 ......................................................................................................................... 4 1962 ......................................................................................................................... 5 963 ......................................................................................................................... 5 964 ......................................................................................................................... 6 965 ......................................................................................................................... 6 966 ........................................................................................................................ -
Les Puissances Spatiales Qui Montent
SOMMAIRE Les puissances spatiales qui montent Par Philippe VOLVERT 1 SOMMAIRE 2 SOMMAIRE Les puissances spatiales qui montent Par Philippe VOLVERT 3 SOMMAIRE SOMMAIRE SOMMAIRE ..................................................................................................................................................... 4 INTRODUCTION ............................................................................................................................................. 5 L’ESPACE AU PAYS DU SOLEIL LEVANT ..................................................................................................... 6 LES AMBITIONS CHINOISES ........................................................................................................................ 14 L’INDEPENDANCE SPATIALE INDIENNE ................................................................................................... 24 L’ESPACE ET LE RESTE DU MONDE ........................................................................................................... 29 LES GRANDES DATES DE L’ASTRONAUTIQUE JAPONAISE .................................................................... 36 LES GRANDES DATES DE L’ASTRONAUTIQUE CHINOISE ....................................................................... 39 LES GRANDES DATES DE L’ASTRONAUTIQUE INDIENNE........................................................................ 41 LES VOLS HABITES ...................................................................................................................................... -
A Low-Cost Launch Assistance System for Orbital Launch Vehicles
Hindawi Publishing Corporation International Journal of Aerospace Engineering Volume 2012, Article ID 830536, 10 pages doi:10.1155/2012/830536 Review Article A Low-Cost Launch Assistance System for Orbital Launch Vehicles Oleg Nizhnik ERATO Maenaka Human-Sensing Fusion Project, 8111, Shosha 2167, Hyogo-ken, Himeji-shi, Japan Correspondence should be addressed to Oleg Nizhnik, [email protected] Received 17 February 2012; Revised 6 April 2012; Accepted 16 April 2012 Academic Editor: Kenneth M. Sobel Copyright © 2012 Oleg Nizhnik. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. The author reviews the state of art of nonrocket launch assistance systems (LASs) for spaceflight focusing on air launch options. The author proposes an alternative technologically feasible LAS based on a combination of approaches: air launch, high-altitude balloon, and tethered LAS. Proposed LAS can be implemented with the existing off-the-shelf hardware delivering 7 kg to low-earth orbit for the 5200 USD per kg. Proposed design can deliver larger reduction in price and larger orbital payloads with the future advances in the aerostats, ropes, electrical motors, and terrestrial power networks. 1. Introduction point to the progress in the orbital delivery systems for these additional payload classes. Spaceflight is the mature engineering discipline—54 years old as of 2012. But seemingly paradoxically, it still relies solely 2. Overview of Previously Proposed LAS on the hardware and methodology developed in the very beginning of the spaceflight era. Modernly, still heavily-used A lot of proposals have been made to implement nonrocket Soyuz launch vehicle systems (LVSs) are the evolutionary LASandarelistedinTable 1. -
Photographs Written Historical and Descriptive
CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY HAER FL-8-B BUILDING AE HAER FL-8-B (John F. Kennedy Space Center, Hanger AE) Cape Canaveral Brevard County Florida PHOTOGRAPHS WRITTEN HISTORICAL AND DESCRIPTIVE DATA HISTORIC AMERICAN ENGINEERING RECORD SOUTHEAST REGIONAL OFFICE National Park Service U.S. Department of the Interior 100 Alabama St. NW Atlanta, GA 30303 HISTORIC AMERICAN ENGINEERING RECORD CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY BUILDING AE (Hangar AE) HAER NO. FL-8-B Location: Hangar Road, Cape Canaveral Air Force Station (CCAFS), Industrial Area, Brevard County, Florida. USGS Cape Canaveral, Florida, Quadrangle. Universal Transverse Mercator Coordinates: E 540610 N 3151547, Zone 17, NAD 1983. Date of Construction: 1959 Present Owner: National Aeronautics and Space Administration (NASA) Present Use: Home to NASA’s Launch Services Program (LSP) and the Launch Vehicle Data Center (LVDC). The LVDC allows engineers to monitor telemetry data during unmanned rocket launches. Significance: Missile Assembly Building AE, commonly called Hangar AE, is nationally significant as the telemetry station for NASA KSC’s unmanned Expendable Launch Vehicle (ELV) program. Since 1961, the building has been the principal facility for monitoring telemetry communications data during ELV launches and until 1995 it processed scientifically significant ELV satellite payloads. Still in operation, Hangar AE is essential to the continuing mission and success of NASA’s unmanned rocket launch program at KSC. It is eligible for listing on the National Register of Historic Places (NRHP) under Criterion A in the area of Space Exploration as Kennedy Space Center’s (KSC) original Mission Control Center for its program of unmanned launch missions and under Criterion C as a contributing resource in the CCAFS Industrial Area Historic District. -
Fiscal Year 1973, and Are the EROS Program Also Supports the ERTS Data Proiected at Almost $1 Million for Fiscal Year 1974
Aeronautics and Space Report of the President r973 Activities NOTE TO READERS: ALL PRINTED PAGES ARE INCLUDED, UNNUMBERED BLANK PAGES DURING SCANNING AND QUALITY CONTROL CHECK HAVE BEEN DELETED Aeronautics and Space Report of the President 1973 A c tivities National Aeronautics and Space Administration Washington, D.C. 20546 President’s Message of Transmittal To the Congress of the United States: the European Space Conference has agreed to con- struct a space laboratory-Spacelab-for use with the I am pleased to transmit this report on our Nation’s Shuttle. progress in aeronautics and space activities during Notable progress has also been made with the Soviet 1973. Union in preparing the Apollo-Soyuz Test Project This year has been particularly significant in that scheduled for 1975. We are continuing to cooperate many past efforts to apply the benefits of space tech- with other nations in space activities and sharing of nology and information to the solution of problems on scientific information. These efforts contribute to global Earth are now coming to fruition. Experimental data peace and prosperity. from the manned Skylab station and the unmanned While we stress the use of current technology to solve Earth Resources Technology Satellite are already being current problems, we are employing unmanned space- used operationally for resource discovery and manage- craft to stimulate further advances in technology and ment, environmental information, land use planning, to obtain knowledge that can aid us in solving future and other applications. problems. Pioneer 10 gave us our first closeup glimpse Communications satellites have become one of the of Jupiter and transmitted data which will enhance principal methods of international communication our knowledge of Jupiter, the solar system, and ulti- and are an important factor in meeting national de- mately our own planet. -
Reliability Considerations for Communication Satellites
Copyright Warning & Restrictions The copyright law of the United States (Title 17, United States Code) governs the making of photocopies or other reproductions of copyrighted material. Under certain conditions specified in the law, libraries and archives are authorized to furnish a photocopy or other reproduction. One of these specified conditions is that the photocopy or reproduction is not to be “used for any purpose other than private study, scholarship, or research.” If a, user makes a request for, or later uses, a photocopy or reproduction for purposes in excess of “fair use” that user may be liable for copyright infringement, This institution reserves the right to refuse to accept a copying order if, in its judgment, fulfillment of the order would involve violation of copyright law. Please Note: The author retains the copyright while the New Jersey Institute of Technology reserves the right to distribute this thesis or dissertation Printing note: If you do not wish to print this page, then select “Pages from: first page # to: last page #” on the print dialog screen The Van Houten library has removed some of the personal information and all signatures from the approval page and biographical sketches of theses and dissertations in order to protect the identity of NJIT graduates and faculty. RELIABILITY CONSIDERATIONS FOR COMMUNICATION SATELLITES BY FRANK POLIZZI A THESIS PRESENTED IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE OF MASTER OF SCIENCE IN MANAGEMENT ENGINEERING AT NEWARK COLLEGE OF ENGINEERING This thesis is to be used only with due regard to the rights of the author(s). Bibliographical references may be noted, but passages must not be copied without permission of the College and without credit being given in subsequent written or published work.