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Brazil's Accession to the Mtcr
Wyn Q. Bowen Report: BRAZIL’S ACCESSION TO THE MTCR by Wyn Q. Bowen Wyn Q. Bowen is a Senior Research Associate of the Center for Nonproliferation Studies at the Monterey Institute of International Studies. He is also a Ph.D. candidate in International Relations at the University of Birmingham and is completing a dissertation on U.S. missile nonproliferation policy during the Bush administration. n October 1995, Brazil’s membership in the Mis- the design and construction of a center from which to sile Technology Control Regime (MTCR) was ap- launch the VLS at Alcantara (CLA), in the northern proved unanimously at the regime’s 10th plenary state of Maranhao.1 The VLS was to be developed us- I 2 meeting in Bonn, Germany. Acceptance in the MTCR ing technology derived from the Sonda rocket series. was the outcome of a series of policy changes initi- The central role of the military in the MECB during ated by Brazil in early 1994 to address international the 1980s, however, cast doubt over the true nature of missile proliferation concerns. This report consid- the space program. The Brazilian Commission for Space ers the past Brazilian rocket and missile activities that Activities (COBAE), responsible for overseeing and generated these concerns and the policy changes running the MECB, was chaired by the armed forces which Brazil undertook to gain acceptance in the chief of staff.3 The prominent role of the Air Force’s MTCR. The implications of Brazil’s membership in Aerospace Technical Center (CTA) in developing the the regime are also considered, along with some of VLS also suggested the military might have other rea- the missile proliferation concerns which continue to sons for developing space launch vehicles. -
Suborbital Platforms and Range Services (SPARS)
Suborbital Capabilities for Science & Technology Small Missions Workshop @ Johns Hopkins University June 10, 2019 Mike Hitch, Giovanni Rosanova Goddard Space Introduction Flight Center AGENDAWASP OPIS ▪ Purpose ▪ History & Importance of Suborbital Carriers to Science ▪ Suborbital Platforms ▪ Sounding Rockets ▪ Balloons (brief) ▪ Aircraft ▪ SmallSats ▪ WFF Engineering ▪ Q & A P-3 Maintenance 12-Jun-19 Competition Sensitive – Do Not Distribute 2 Goddard Space Purpose of the Meeting Flight Center Define theWASP OPISutility of Suborbital Carriers & “Small” Missions ▪ Sounding rockets, balloons and aircraft (manned and unmanned) provide a unique capability to scientists and engineers to: ▪ Allow PIs to enhance and advance technology readiness levels of instruments and components for very low relative cost ▪ Provide PIs actual science flight opportunities as a “piggy-back” on a planned mission flight at low relative cost ▪ Increase experience for young and mid-career scientists and engineers by allowing them to get their “feet wet” on a suborbital mission prior to tackling the much larger and more complex orbital endeavors ▪ The Suborbital/Smallsat Platforms And Range Services (SPARS) Line Of Business (LOB) can facilitate prospective PIs with taking advantage of potential suborbital flight opportunities P-3 Maintenance 12-Jun-19 Competition Sensitive – Do Not Distribute 3 Goddard Space Value of Suborbital Research – What’s Different? Flight Center WASP OPIS Different Risk/Mission Assurance Strategy • Payloads are recovered and refurbished. • Re-flights are inexpensive (<$1M for a balloon or sounding rocket vs >$10M - 100M for a ELV) • Instrumentation can be simple and have a large science impact! • Frequent flight opportunities (e.g. “piggyback”) • Development of precursor instrument concepts and mature TRLs • While Suborbital missions fully comply with all Agency Safety policies, the program is designed to take Higher Programmatic Risk – Lower cost – Faster migration of new technology – Smaller more focused efforts, enable Tiger Team/incubator experiences. -
Measurements of Auroral Particles by Means of Sounding Rockets of Mother-Daughter Type A
MEASUREMENTS OF AURORAL PARTICLES BY MEANS OF SOUNDING ROCKETS OF MOTHER-DAUGHTER TYPE A. Falck KGI REPORT 192 NOVEMBER 1985 KIRUNA U-OI'HYSICAL INSTITITK MKINA N\X|1>I\ MEASUREMENTS OF AURORAL PARTICLES BY MEANS OF SOUNDING ROCKETS OF MOTHER-DAUGHTER TYPE by A. Falck Kiruna Geophysical Institute P.O. Box 704, S-981 27 KIRUNA, Sweden KGI Report 192 November 1985 Printed in Sweden Kiruna Geophysical Institute Kiruna 19^5 ISSN 034/-f 405 Contents Page 1. Presentation of the S17 payioads 3 1.1 The scientific objective of the sounding rockets S17 3 1.2 S17 experiments 3 1.3 Physical characteristics of the payioads 3 1.4 Physical characteristics of the Nike-Tomahawk rocket 5 1.5 Nominal characteristics of flight events 7 1.6 Attitude measurements 8 1.7 Separation of the two payload units 20 1.8 Telemetry and data analyzing technique 33 2. Description of the instrumentation for the particle experiments in the S17 payioads 38 2.1 General theory of CEM - detectors 38 2.2 Calibration of th* CEM - detectors 42 2.3 Solid state detectors in SI7 payioads 44 2.4 Mounting of the detectors 48 2.5 The efficiency of channel multipliers 48 3. Review of the geophysical conditions during the SI7 flights and presentation of some supporting observations 51 j.1 The auroral situation during S17 flights 51 :• 2 Magnetic activity 51 .'.3 Other supporting observations 56 .4 The lowlightlevel-TV-system 56 'K Particle fluxes and electric currents coupling the magnetosphere and the ionosphere during a magnetospheric substorm 66 4.1 Review of some substorm terminology and definitions 66 4.2 Reference and comparisons of SI7-2 measure- ments with the results of the IMS-study 75 4.3 Comparison of simultaneous particle observa- tions at low ionospheric altitude (S17-1) and at the magnetic equatorial region (ATS-6) 91 4.4 Summary and conclusions 99 5. -
Colorado Space Grant Consortium
CO_FY16_Year2_APD Colorado Space Grant Consortium Lead Institution: University of Colorado Boulder Director: Chris Koehler Telephone Number: 303.492.3141 Consortium URL: http://spacegrant.colorado.edu Grant Number: NNX15AK04H Lines of Business (LOBs): NASA Internships, Fellowships, and Scholarships; Stem Engagement; Institutional Engagement; Educator Professional Development A. PROGRAM DESCRIPTION The National Space Grant College and Fellowship Program consists of 52 state-based, university- led Space Grant Consortia in each of the 50 states plus the District of Columbia and the Commonwealth of Puerto Rico. Annually, each consortium receives funds to develop and implement student fellowships and scholarships programs; interdisciplinary space-related research infrastructure, education, and public service programs; and cooperative initiatives with industry, research laboratories, and state, local, and other governments. Space Grant operates at the intersection of NASA’s interest as implemented by alignment with the Mission Directorates and the state’s interests. Although it is primarily a higher education program, Space Grant programs encompass the entire length of the education pipeline, including elementary/secondary and informal education. The Colorado Space Grant Consortium is a Designated Consortium funded at a level of $760,000 for fiscal year 2016. B. PROGRAM GOALS • Population of students engaged in COSGC hands-on programs (awardees and non- awardees) will be at least 40% women and 23.7% from ethnic minority populations underrepresented in STEM fields. • Maintain student hands-on programs at all 8 COSGC Minority Serving Institutions and engaged at least 30 students on MSI campuses. • 30% of COSGC NASA funds will be awarded directly to students. • Award 80 scholarships to support students working on hands-on projects. -
Intelligent Building Blocks for On-Orbit Satellite Servicing and Assembly
DLR at a glance DLR is the national aeronautics and space research centre of the Federal Republic of Germany. iBOSS_GB_3/2017 Its extensive research and development work in aeronautics, space, energy, transport and security is integrated into national and international cooperative ventures. In addition to its own research, as Germany’s space agency, DLR has been given responsibility by the federal government for the planning and implementation of the German space programme. DLR is also the umbrella organisation for the nation’s largest project management agency. DLR has approximately 8000 employees at 20 locations in Germany: Cologne (headquarters), Augsburg, Berlin, Bonn, Braunschweig, Bremen, Bremerhaven, Dresden, Goettingen, Ham- burg, Jena, Juelich, Lampoldshausen, Neustrelitz, Oberpfaffenhofen, Oldenburg, Stade, Stuttgart, Trauen, and Weilheim. DLR also has offices in Brussels, Paris, Tokyo and Washington D.C. DLR’s mission comprises the exploration of Earth and the Solar System and research for pro- tecting the environment. This includes the development of environment-friendly technologies for energy supply and future mobility, as well as for communications and security. DLR’s research portfolio ranges from fundamental research to the development of products for tomorrow. In this way, DLR contributes the scientific and technical expertise that it has ac- quired to the enhancement of Germany as a location for industry and technology. DLR oper- ates major research facilities for its own projects and as a service for clients and partners. It also fosters the development of the next generation of researchers, provides expert advisory services to government and is a driving force in the regions where its facilities are located. -
Performance Modelling and Simulation of a 100 Km Hybrid Sounding Rocket
PERFORMANCE MODELLING AND SIMULATION OF A 100 KM HYBRID SOUNDING ROCKET Fiona Kay Leverone Submitted in fulfilment of the academic requirements for the degree of Master of Science in Mechanical Engineering, College of Agriculture, Engineering and Science, University of KwaZulu-Natal Supervisor: Mr Michael Brooks Co-Supervisor: Mr Jean-François Pitot de la Beaujardiere Co-Supervisor: Prof Lance Roberts December 2013 2. DECLARATION 1 - PLAGIARISM I, Fiona Leverone, declare that 1. The research reported in this thesis, except where otherwise indicated, is my original research. 2. This thesis has not been submitted for any degree or examination at any other university. 3. This thesis does not contain other persons’ data, pictures, graphs or other information, unless specifically acknowledged as being sourced from other persons. 4. This thesis does not contain other persons’ writing, unless specifically acknowledged as being sourced from other researchers. Where other written sources have been quoted, then: a. Their words have been re-written but the general information attributed to them has been referenced b. Where their exact words have been used, then their writing has been placed inside quotation marks, and referenced. 5. This thesis does not contain text, graphics or tables copied and pasted from the Internet, unless specifically acknowledged, and the source being detailed in the thesis and in the References sections. Signed ________________________ Date ___________ Miss Fiona Leverone As the candidate’s supervisor I have approved this dissertation for submission. Signed ________________________ Date ___________ Mr. Michael Brooks As the candidates co-supervisor I have approved this dissertation for submission. Signed ________________________ Date ___________ Mr. -
What's Inside... in Brief
National Aeronautics and Space Administration What’s inside... 2 Features 5 Integration and Testing 4 1 3 2 2015 6 Picture Place 7 Other News 8 Schedule & Miscellanea Sounding Rockets Program Office 46.012 UO Koehler - RockSat-X was succesfully launched In Brief... from Wallops Island on August 12, 2015. The new Black Brant Mk 4 vehicle will fly for the first time in October 2015 from Wallops Island. The payload carries several technology test experi- ments and instruments. Payload teams are preparing for the coming Norway campaign. Two rockets will be launched from Andoya with the launch window opening on November 27. The Multiple User Suborbital Instru- ment Carrier (MUSIC) payload will be launched from Wallops Island in Oc- tober on a Terrier-Improved Malemute rocket. The sounding rockets program will cel- ebrate 45-years at Wallops on Novem- ber 30, 2015. More on page 7. A very busy flight schedule is in prog- ress. The Sounding Rockets Program has 11 missions on schedule during the Students from Hawaii with their experiment after the successful flight. period September through November. The 46.012 UO RockSat-X mission was launched from Wallops Island, VA on Au- Three have been successfully complet- gust 12, 2015. RockSat-X is the most advanced of three student flight programs ed and eight remain. managed by Colorado Space Grant Consortium and supported by NASA. RockSat- X provides participating University faculty and students an opportunity to build, RockSat-X continued... test and fly an experiment of their own University Of Hawaii Community College design onboard a Terrier-Improved System University of Nebraska Lincoln (UNL) Malemute sounding rocket and in- Project Imua The experiment from the University of cludes full featured sounding rocket The primary mission goal for Project Nebraska Lincoln compared buoyant support systems, such as telemetry, Imua is to encourage UHCC students to convection on the ground in the pres- attitude control and recovery. -
Space Planes and Space Tourism: the Industry and the Regulation of Its Safety
Space Planes and Space Tourism: The Industry and the Regulation of its Safety A Research Study Prepared by Dr. Joseph N. Pelton Director, Space & Advanced Communications Research Institute George Washington University George Washington University SACRI Research Study 1 Table of Contents Executive Summary…………………………………………………… p 4-14 1.0 Introduction…………………………………………………………………….. p 16-26 2.0 Methodology…………………………………………………………………….. p 26-28 3.0 Background and History……………………………………………………….. p 28-34 4.0 US Regulations and Government Programs………………………………….. p 34-35 4.1 NASA’s Legislative Mandate and the New Space Vision………….……. p 35-36 4.2 NASA Safety Practices in Comparison to the FAA……….…………….. p 36-37 4.3 New US Legislation to Regulate and Control Private Space Ventures… p 37 4.3.1 Status of Legislation and Pending FAA Draft Regulations……….. p 37-38 4.3.2 The New Role of Prizes in Space Development…………………….. p 38-40 4.3.3 Implications of Private Space Ventures…………………………….. p 41-42 4.4 International Efforts to Regulate Private Space Systems………………… p 42 4.4.1 International Association for the Advancement of Space Safety… p 42-43 4.4.2 The International Telecommunications Union (ITU)…………….. p 43-44 4.4.3 The Committee on the Peaceful Uses of Outer Space (COPUOS).. p 44 4.4.4 The European Aviation Safety Agency…………………………….. p 44-45 4.4.5 Review of International Treaties Involving Space………………… p 45 4.4.6 The ICAO -The Best Way Forward for International Regulation.. p 45-47 5.0 Key Efforts to Estimate the Size of a Private Space Tourism Business……… p 47 5.1. -
Global Urban Observation and Information GUOI
Global Urban Observation and Information, 2020-2022 Implementation Plan 1. Executive Summary • Full title of the Initiative: Global Urban Observation and Information, 2020-2022 • Short title or acronym: GUOI 2020 • Existing or proposed category: GEO Initiative • Overview: GUOI 2020 intends to improve urban monitoring and assessment by developing a series of satellite based essential urban variables and indicators of sustainable cities through international cooperation and collaboration, to provide datasets, information, technologies to pertinent urban users in World Bank, UN, Africa, South America, and planning and environmental management agencies in other developing countries, and to support UN SDG Goal 11: Make cities inclusive, safe, resilient and sustainable. The pertinent government agencies that would most likely use our datasets include city authorities and resilient offices, departments of urban and regional planning, environmental management, natural resources, metropolitan transit authority, and office of sustainability, and regional statistics. These agencies need to use the datasets to obtain information about urban land use/land cover, urban form and growth patterns, infrastructure and transport needs, ecosystems and biodiversity, human health, thermal comfort, food security, and socioeconomic development. Further, the World Bank Platform for Urban Mapping and Analysis can be greatly benefited from the datasets, products, and services that this project offers. For scientific community, GUOI 2020 will provide new knowledge on global urbanization process and innovations on urban observation. While some activities are extensions of the GEO SB-04 and GI-17 activities, others are proposed anew. These activities of different organizations and countries are coalesced as one single GEO initiative through collaborative and affiliated projects, annual symposia, international summer school, joint field works, publications, and coordinated user engagement efforts. -
Methods of Oabservation at Sea Meteorological Soundings in The
WORLD METEOROLOGICAL ORGANIZATION WORLD METEOROLOGICAL ORGANIZATION TECHNICAL NOTE No. 2 TECHNICAL NOTE No. 60 METHODS OF OABSERVATION AT SEA METEOROLOGICAL SOUNDINGS IN THE PARTUPPER I – SEA SURFACEATMOSPHERE TEMPERATURE by W.W. KELLOGG WMO-No.WMO-No. 153. 26. TP. 738 Secretariat of the World Meteorological Organization – Geneva – Switzerland THE WMO The WOTld :Meteol'ological Organization (Wl\IO) is a specialized agency of the United Nations of which 125 States and Territories arc Members. It was created: to facilitate international co~operation in the establishment of networks of stations and centres to provide meteorological services and observationsI to promote the establishment and maintenance of systems for the rapid exchange of meteorological information, to promote standardization of meteorological observations and ensure the uniform publication of observations and statistics. to further the application of rneteol'ology to Rviatioll, shipping, agricultul"C1 and other human activities. to encourage research and training in meteorology. The machinery of the Organization consists of: The World Nleteorological Congress, the supreme body of the o.rganization, brings together the delegates of all Members once every four years to determine general policies for the fulfilment of the purposes of the Organization, to adopt Technical Regulations relating to international meteorological practice and to determine the WMO programme, The Executive Committee is composed of 21 dil'cetors of national meteorological services and meets at least once a yeae to conduct the activities of the Organization and to implement the decisions taken by its Members in Congress, to study and make recommendations Oll matters affecting international meteorology and the opel'ation of meteorological services. -
Importance Oi Thermistor Mount Configuration to Meteorological
James F. Morrissey importance oi and Andrew S. Carten, Jr. thermistor mount configuration A. F. Cambridge Research Laboratories to meteorological rocket Bedford, Mass. temperature measurements Abstract tions. Thus, we are receiving more data than ever be- A description is given of the original rocketsonde ther- fore—thanks to more successful firings and improved mistor mount, consisting of a 10-mil bead suspended signal reception—but data quality has stayed at a low between two metal posts. The difficulties encountered to medium level. Recent evidence, described later in this with this mount and the subsequent development of article, confirms our belief that caution is in order. the superior "thin-film" mount are also described. The Today's rocketsonde is, for the most part, a more uncertainties associated with the use of the latter mount rugged version of the standard radiosonde. This is only are outlined along with their effect on data acceptance. natural, considering both the effort which has gone into A different approach to the original problem is de- refining radiosonde and associated ground equipment scribed, which employs longer leads for dissipation of design and the success which has crowned that effort. heat conducted to the bead. The uncertainty associated In choosing a sensor for the rocketsonde, it was recog- with the long lead is shown to be minimal. Preliminary nized that the small bead thermistor has the necessary results of a series of 10 rocket flights are presented. response time to provide useful measurements to about These results tend to confirm the advantages of the 60 km. A 10-mil diameter bead, aluminized to minimize long lead mount. -
Desind Finding
NATIONAL AIR AND SPACE ARCHIVES Herbert Stephen Desind Collection Accession No. 1997-0014 NASM 9A00657 National Air and Space Museum Smithsonian Institution Washington, DC Brian D. Nicklas © Smithsonian Institution, 2003 NASM Archives Desind Collection 1997-0014 Herbert Stephen Desind Collection 109 Cubic Feet, 305 Boxes Biographical Note Herbert Stephen Desind was a Washington, DC area native born on January 15, 1945, raised in Silver Spring, Maryland and educated at the University of Maryland. He obtained his BA degree in Communications at Maryland in 1967, and began working in the local public schools as a science teacher. At the time of his death, in October 1992, he was a high school teacher and a freelance writer/lecturer on spaceflight. Desind also was an avid model rocketeer, specializing in using the Estes Cineroc, a model rocket with an 8mm movie camera mounted in the nose. To many members of the National Association of Rocketry (NAR), he was known as “Mr. Cineroc.” His extensive requests worldwide for information and photographs of rocketry programs even led to a visit from FBI agents who asked him about the nature of his activities. Mr. Desind used the collection to support his writings in NAR publications, and his building scale model rockets for NAR competitions. Desind also used the material in the classroom, and in promoting model rocket clubs to foster an interest in spaceflight among his students. Desind entered the NASA Teacher in Space program in 1985, but it is not clear how far along his submission rose in the selection process. He was not a semi-finalist, although he had a strong application.