Final Delta II Rocket Carries NASA's Icesat-2 to Measure Earth's
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General Assembly Distr.: General 29 January 2001
United Nations A/AC.105/751/Add.1 General Assembly Distr.: General 29 January 2001 Original: English Committee on the Peaceful Uses of Outer Space National research on space debris, safety of space objects with nuclear power sources on board and problems of their collisions with space debris Note by the Secretariat* Addendum Contents Chapter Paragraphs Page I. Introduction........................................................... 1-2 2 Replies received from Member States and international organizations .................... 2 United States of America ......................................................... 2 European Space Agency.......................................................... 7 __________________ * The present document contains replies received from Member States and international organizations between 25 November 2000 and 25 January 2001. V.01-80520 (E) 020201 050201 A/AC.105/751/Add.1 I. Introduction 1. At its forty-third session, the Committee on the Peaceful Uses of Outer Space agreed that Member States should continue to be invited to report to the Secretary- General on a regular basis with regard to national and international research concerning the safety of space objects with nuclear power sources, that further studies should be conducted on the issue of collision of orbiting space objects with nuclear power sources on board with space debris and that the Committee’s Scientific and Technical Subcommittee should be kept informed of the results of such studies.1 The Committee also took note of the agreement of the Subcommittee that national research on space debris should continue and that Member States and international organizations should make available to all interested parties the results of that research, including information on practices adopted that had proved effective in minimizing the creation of space debris (A/AC.105/736, para. -
European Space Surveillance and Tracking
2ndEuropean EU SST Webinar: Space Operations in Space Surveillance and Tracking 16Surveillance November 2020 –and14h CETTracking The EU SST activities received funding from the European Union programmes, notably from the Horizon 2020 research and innovation programme under grant agreements No 760459, No 785257, No 713630, No 713762 and No 634943, and the Copernicus and Galileo programme under grant agreements No 299/G/GRO/COPE/19/11109, No 237/GRO/COPE/16/8935 and No 203/G/GRO/COPE/15/7987. This Portal reflects only the SST Cooperation’s actions and the European Commission and the Research Executive Agency are not responsible for any use that may be made of the information it contains. 2nd EU SST Webinar Operations in Space Surveillance and Tracking Speakers Pascal María Antonia Cristina Florian João FAUCHER (CNES) RAMOS (CDTI) PÉREZ (CDTI) DELMAS (CNES) ALVES (EU SatCen) Pier Luigi Lt. Moreno Juan Christophe Rodolphe RIGHETTI PERONI (IT MoD) ESCALANTE MORAND (EEAS) MUÑOZ (EUMETSAT) (EC – DG ECHO) (EC-DG DEFIS) 2nd EU SST Webinar: Operations in Space Surveillance and Tracking 16 November 2020 3 Agenda (1/2) 14h00-14h10: Welcome to the 2nd EU SST Webinar [Moderator: Mr Oliver Rajan (EU SatCen)] 14h10-14h50: SST Support Framework: Safeguarding European space infrastructure • Overview, governance model, security relevance and future perspectives [SST Cooperation Chair: Dr Pascal Faucher (CNES)] EU SST Architecture & Service Provision Model • Sensors network • Database and Catalogue precursor • Services [Chair of the SST Technical Committee: -
The Sky This Month – Sept 12 to Oct 10, 2018 (Times in EDT) by Chris Vaughan
RASC Toronto Centre – www.rascto.ca The Sky This Month – Sept 12 to Oct 10, 2018 (times in EDT) by Chris Vaughan NEWS Space Exploration – Public and Private Ref. http://spaceflightnow.com/launch-schedule/ Launches Sept 13 at 5:21 pm EDT – Japanese H-2B rocket from Tanegashima Space Center, Japan, payload unmanned cargo vehicle to deliver equipment and supplies to ISS. Sept 15 at 8:46-11:20 am EDT - ULA Delta 2 rocket from Vandenberg Air Force Base, payload NASA’s ICESat 2 investigating ice-sheet elevation change, sea-ice freeboard, and vegetation canopy height. Sept 16 at TBD - India’s Polar Satellite Launch Vehicle from Satish Dhawan Space Center, Sriharikota, India, payload NovaSAR-S radar imaging instrument and SSTL-S1 Earth observation satellites. Sept 25 at TBD - Ariane 5 ECA rocket from Kourou, French Guiana, payload Horizons 3e and Azerspace 2/Intelsat 38 communications satellites. Oct TBD - India’s Geosynchronous Satellite Launch Vehicle Mk. 3 from Satish Dhawan Space Center, Sriharikota, India, payload GSAT 29 communications satellite. Oct 6 at 4:00-5:30 am EDT - Air-launched Northrop Grumman Pegasus XL rocket from Cape Canaveral Air Force Station, payload NASA’s Ionospheric Connection Explorer (ICON) satellite to study the ionosphere. Oct 7 at TBD - SpaceX Falcon 9 rocket from Vandenberg Air Force Base, payload SAOCOM 1A Earth observation satellite for Argentina’s space agency. JUNO at Jupiter Juno is presently executing a series of 53 day orbits. The 15th perijove close pass occurred on September 7. News at https://www.missionjuno.swri.edu/news/ DAWN at Ceres The DAWN spacecraft will exhaust its manoeuvring hydrazine supply any time now, and then remain in orbit around Ceres for decades (at least) to protect Ceres against Earth-contamination. -
Model Based Systems Engineering for a Venture Class Launch Facility
Old Dominion University ODU Digital Commons Mechanical & Aerospace Engineering Theses & Dissertations Mechanical & Aerospace Engineering Fall 11-2020 Model Based Systems Engineering for a Venture Class Launch Facility Walter McGee Taraila Old Dominion University, [email protected] Follow this and additional works at: https://digitalcommons.odu.edu/mae_etds Part of the Mechanical Engineering Commons, and the Systems Engineering and Multidisciplinary Design Optimization Commons Recommended Citation Taraila, Walter M.. "Model Based Systems Engineering for a Venture Class Launch Facility" (2020). Master of Science (MS), Thesis, Mechanical & Aerospace Engineering, Old Dominion University, DOI: 10.25777/ b713-zf77 https://digitalcommons.odu.edu/mae_etds/326 This Thesis is brought to you for free and open access by the Mechanical & Aerospace Engineering at ODU Digital Commons. It has been accepted for inclusion in Mechanical & Aerospace Engineering Theses & Dissertations by an authorized administrator of ODU Digital Commons. For more information, please contact [email protected]. MODEL BASED SYSTEMS ENGINEERING FOR A VENTURE CLASS LAUNCH FACILITY by Walter McGee Taraila B.Sc. May 2012, University of Maryland, College Park A Thesis Submitted to the Faculty of Old Dominion University in Partial Fulfillment of the Requirements for the Degree of MASTER OF SCIENCE MECHANICAL AND AEROSPACE ENGINEERING OLD DOMINION UNIVERSITY December 2020 Approved by: Sharan Asundi (Director) Holly Handley (Member) Miltos Kotinis (Member) ABSTRACT MODEL BASED SYSTEMS ENGINEERING FOR A VENTURE CLASS LAUNCH FACILITY Walter McGee Taraila Old Dominion University, 2020 Director: Dr. Sharan Asundi A study of Model-Based Systems Engineering (MBSE) applied to a small-lift launch facility is presented. The research uses Systems Modeling Language (SysML) products and functional diagrams to document the structure, controls, electrical power, hydraulic, safety mechanisms, softWare, and fluid ground systems on a launch pad. -
The Evolving Launch Vehicle Market Supply and the Effect on Future NASA Missions
Presented at the 2007 ISPA/SCEA Joint Annual International Conference and Workshop - www.iceaaonline.com The Evolving Launch Vehicle Market Supply and the Effect on Future NASA Missions Presented at the 2007 ISPA/SCEA Joint International Conference & Workshop June 12-15, New Orleans, LA Bob Bitten, Debra Emmons, Claude Freaner 1 Presented at the 2007 ISPA/SCEA Joint Annual International Conference and Workshop - www.iceaaonline.com Abstract • The upcoming retirement of the Delta II family of launch vehicles leaves a performance gap between small expendable launch vehicles, such as the Pegasus and Taurus, and large vehicles, such as the Delta IV and Atlas V families • This performance gap may lead to a variety of progressions including – large satellites that utilize the full capability of the larger launch vehicles, – medium size satellites that would require dual manifesting on the larger vehicles or – smaller satellites missions that would require a large number of smaller launch vehicles • This paper offers some comparative costs of co-manifesting single- instrument missions on a Delta IV/Atlas V, versus placing several instruments on a larger bus and using a Delta IV/Atlas V, as well as considering smaller, single instrument missions launched on a Minotaur or Taurus • This paper presents the results of a parametric study investigating the cost- effectiveness of different alternatives and their effect on future NASA missions that fall into the Small Explorer (SMEX), Medium Explorer (MIDEX), Earth System Science Pathfinder (ESSP), Discovery, -
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. -
National Reconnaissance Office Review and Redaction Guide
NRO Approved for Release 16 Dec 2010 —Tep-nm.T7ymqtmthitmemf- (u) National Reconnaissance Office Review and Redaction Guide For Automatic Declassification Of 25-Year-Old Information Version 1.0 2008 Edition Approved: Scott F. Large Director DECL ON: 25x1, 20590201 DRV FROM: NRO Classification Guide 6.0, 20 May 2005 NRO Approved for Release 16 Dec 2010 (U) Table of Contents (U) Preface (U) Background 1 (U) General Methodology 2 (U) File Series Exemptions 4 (U) Continued Exemption from Declassification 4 1. (U) Reveal Information that Involves the Application of Intelligence Sources and Methods (25X1) 6 1.1 (U) Document Administration 7 1.2 (U) About the National Reconnaissance Program (NRP) 10 1.2.1 (U) Fact of Satellite Reconnaissance 10 1.2.2 (U) National Reconnaissance Program Information 12 1.2.3 (U) Organizational Relationships 16 1.2.3.1. (U) SAF/SS 16 1.2.3.2. (U) SAF/SP (Program A) 18 1.2.3.3. (U) CIA (Program B) 18 1.2.3.4. (U) Navy (Program C) 19 1.2.3.5. (U) CIA/Air Force (Program D) 19 1.2.3.6. (U) Defense Recon Support Program (DRSP/DSRP) 19 1.3 (U) Satellite Imagery (IMINT) Systems 21 1.3.1 (U) Imagery System Information 21 1.3.2 (U) Non-Operational IMINT Systems 25 1.3.3 (U) Current and Future IMINT Operational Systems 32 1.3.4 (U) Meteorological Forecasting 33 1.3.5 (U) IMINT System Ground Operations 34 1.4 (U) Signals Intelligence (SIGINT) Systems 36 1.4.1 (U) Signals Intelligence System Information 36 1.4.2 (U) Non-Operational SIGINT Systems 38 1.4.3 (U) Current and Future SIGINT Operational Systems 40 1.4.4 (U) SIGINT -
Summary of Meteorological Satellites
Technical Summary of Meteorological Satellites TIROS – Television and Infra-Red Observation Satellite series Parameter TIROS I TIROS II TIROS III TIROS IV TIROS V TIROS VI TIROS VII TIROS VIII12 TIROS IX5 TIROS X 9 Launch Date 1/4/1960 23/11/1960 12/7/1961 8/2/1962 19/6/1962 18/9/1962 19/6/1963 21/12/1963 22/1/1965 2/7/1965 Deactivated 19/6/1960 1/2/1961 30/10/1961 30/6/1962 5/5/1963 11/10/1963 3/2/19661 1/7/19672 15/2/19673 3/7/19674 Lifetime 79 days 69 days 108 days 125 days 320 days 388 days 978 days 1258 days 754 days 732 days Pictures 19389 25574 24000 23370 48547 59830 111047 88662 76604 59119 Launcher Thor-Able Thor-Delta Thor-Delta Thor-Delta Thor-Delta Thor-Delta Thor-Delta Thor-Delta Thor-Delta Thor-Delta Site ETR ETR ETR ETR ETR ETR ETR ETR WTR ETR Pre-launch A1 A2 A3 A9 A50 A51 A52 A53 A54 OT-1 Designation 1960 2A 1960 16A 1961 17A 1962 2 A 1962 25A 1962 47A 1963 24A11 1963 54A 1965 4A 1965 51A 1960 β 2 1960 π 1 1961 ρ 1 1962 β 1 1962 αα 1 1962 αψ 1 Catalog No 29 63 162 226 309 397 604 716 978 1430 Apogee 867 km 837 937 972 1119 822 743 878 2967 957 Perigee 768 km 717 854 817 680 783 713 796 806 848 Inclination 48.392° 48.530° 47.898° 48.3° 58.1° 58.2° 58.2° 58.5° 96.4° 98.6° Period 99.24’ 98.26’ 100.4’ 100.4’ 100.5’ 98.7’ 97.4’ 99.3’ 119.2’ 100.6’ Mass 120 kg 125 129 129 129 127 135 119 138 127 Camera 1 TV-NA TV-NA TV-WA TV-WA TV-WA TV-WA TV-WA APT TV-WA TV-WA 3/5/62 14/5/63 21/10/63 31/8/64 Camera 2 TV-WA TV-WA TV-WA TV-MA TV-MA TV-MA TV-WA TV-WA TV-WA TV-WA 10/6/62 7/7/62 29/11/62 26/7/65 -/9/65 IR • • • • IRP • • • • HB -
2019 Ocean Surface Topography Science Team Meeting Convene
2019 Ocean Surface Topography Science Team Meeting Convene Chicago 16 West Adams Street, Chicago, IL 60603 Monday, October 21 2019 - Friday, October 25 2019 The 2019 Ocean Surface Topography Meeting will occur 21-25 October 2019 and will include a variety of science and technical splinters. These will include a special splinter on the Future of Altimetry (chaired by the Project Scientists), a splinter on Coastal Altimetry, and a splinter on the recently launched CFOSAT. In anticipation of the launch of Jason-CS/Sentinel-6A approximately 1 year after this meeting, abstracts that support this upcoming mission are highly encouraged. Abstracts Book 1 / 259 Abstract list 2 / 259 Keynote/invited OSTST Opening Plenary Session Mon, Oct 21 2019, 09:00 - 12:35 - The Forum 12:00 - 12:20: How accurate is accurate enough?: Benoit Meyssignac 12:20 - 12:35: Engaging the Public in Addressing Climate Change: Patricia Ward Science Keynotes Session Mon, Oct 21 2019, 14:00 - 15:45 - The Forum 14:00 - 14:25: Does the large-scale ocean circulation drive coastal sea level changes in the North Atlantic?: Denis Volkov et al. 14:25 - 14:50: Marine heat waves in eastern boundary upwelling systems: the roles of oceanic advection, wind, and air-sea heat fluxes in the Benguela system, and contrasts to other systems: Melanie R. Fewings et al. 14:50 - 15:15: Surface Films: Is it possible to detect them using Ku/C band sigmaO relationship: Jean Tournadre et al. 15:15 - 15:40: Sea Level Anomaly from a multi-altimeter combination in the ice covered Southern Ocean: Matthis Auger et al. -
Delta II Dawn Mission Booklet
Delta Launch Vehicle Programs Dawn United Launch Alliance is proud to launch the Dawn mission. Dawn will be launched aboard a Delta II 7925H launch vehicle from Cape Canaveral Air Force Station (CCAFS), Florida. The launch vehicle will deliver the Dawn spacecraft into an Earth- escape trajectory, where it will commence its journey to the solar system’s main asteroid belt to gather comparative data from dwarf planet Ceres and asteroid Vesta. United Launch Alliance provides the Delta II launch service under the NASA Launch Services (NLS) contract with the NASA Kennedy Space Center Expendable Launch Services Program. We are delighted that NASA has chosen the Delta II for this Discovery Mission. I congratulate the entire Delta team for their significant efforts that resulted in achieving this milestone and look forward to continued launches of scientific space missions aboard the Delta launch vehicle. Kristen T. Walsh Director, NASA Programs Delta Launch Vehicles 1 Dawn Mission Overview The Dawn spacecraft will make an eight-year journey to the main asteroid belt between Mars and Jupiter in an effort to significantly increase our understanding of the conditions and processes acting at the solar system’s earliest epoch by examining the geophysical properties of the asteroid Vesta and dwarf planet Ceres. Evidence shows that Vesta and Ceres have distinct characteristics and, therefore, must have followed different evolutionary paths. By observing both, with the same set of instruments, scientists hope to develop an understanding of the transition from the rocky inner regions, of which Vesta is characteristic, to the icy outer regions, of which Ceres is representative. -
Africa's Pulse 2017
APRIL 2017 | VOLUME 15 Public Disclosure Authorized An analysis of issues shaping Africa’s economic future Public Disclosure Authorized Public Disclosure Authorized Public Disclosure Authorized This report was produced by the Office of the Chief Economist for the Africa Region ACKNOWLEDGMENTS This report was prepared by a team led by Punam Chuhan-Pole and comprising Cesar Calderon, Gerard Kambou, Mapi M. Buitano, Vijdan Korman, Erina Iwami, and Catalina Cantu Canales. Contributions were also received from John Baffes, Moussa Blimpo, Paul Brenton, Andrew Dabalen, Massimo Mastruzzi, Fernanda Ruiz Nunes, and Christian Taelor Ueland. Richard Claudet, James Frederick Cust, Sebastien Dessus, Michael Gieger, Marek Hanusch, Katie Kibuuka, Emmanuel Lartey, Emmanuel Pinto Moreira, Cedric Mousset, Grace Kibuthu Ogola, Elliot Joseph Riordan, James Seward, Carlos Vincente, Yutaka Yoshino, and country teams provided valuable comments. The report was prepared under the general guidance of Albert G. Zeufack. Contents Summary ........................................................................... 7 Section 1: Recent Developments and Trends ........................................... 9 Global Developments 9 Sub-Saharan Africa 10 Recent Developments 10 Outlook 18 Risks 21 Challenges 21 Annex 1A: Growth after a Commodity Price Plunge: What to Expect? 29 Commodity Price Cycles 29 Evolution of Real Gross Domestic Product per Worker in Sub-Saharan Africa after a Plunge in International Energy Prices 29 Sources of Growth and the Energy Price Plunge in Sub-Saharan -
GEOS 657 - Lecture 10
GEOS 657 - Lecture 10 GEOS 657 – MICROWAVE REMOTE SENSING SPRING 2019 Lecturer: F.J. Meyer, Geophysical Institute, University of Alaska Fairbanks; [email protected] Lecture 10: SAR Image Acquisition Modes; Past, Current, & Future SAR Sensors; Basics of InSAR Image: DLR, CC-BY 3.0 UAF Class GEOS 657 AVAILABLE SAR SENSORS Franz J Meyer, UAF GEOS 657: Microwave RS - 2 Current and Future SAR Satellites TerraSAR-X & TanDEM-X PAZ SAR X-band Cosmo-SkyMed 1st and 2nd generation ERS-1/2 Envisat Sentinel RADARSAT-2 RCM C-band RADARSAT-1 JERS-1 ALOS-1 ALOS-2 SAOCOM L-band Seasat NISAR BIOMASS P-band 1978 1990 2000 2010 Present Day Future Franz J Meyer, UAF GEOS 657: Microwave RS - 3 1 GEOS 657 - Lecture 10 Current and Future SAR Satellites Accessible Through ASF TerraSAR-X & TanDEM-X PAZ SAR X-band Cosmo-SkyMed 1st and 2nd generation ERS-1/2 Envisat Sentinel-1 RADARSAT-1 RADARSAT-2 RCM C-band JERS-1 ALOS-1 ALOS-2 SAOCOM L-band Seasat NISAR BIOMASS P-band 1978 1990 2000 2010 Present Day Future Franz J Meyer, UAF GEOS 657: Microwave RS - 4 Resolution vs. Spatial Coverage • Medium (10m-class) resolution large-coverage systems: – Sensors: Current: ALOS-2; Sentinel-1; RADARSAT-2 Most of the medium-res Future: SAOCOM; NISAR; RCM; BIOMASS data are free or low cost (not ALOS-2 and R-2) – These sensors are suitable for applications such as: • Monitoring medium to large scale surface deformation (e.g., subsidence; slopes) • Assessing impacts of hazards (flooding; earthquakes) • General mapping and change detection • High (1m-class) limited-coverage resolution systems: – Sensors: Current: TerraSAR-X; TanDEM-X; COSMO-SkyMed constellation nd Future: PAZ SAR; COSMO-SkyMed 2 Gen High-res data is typically – These sensors are suitable for applications such as: more expensive • Mapping and analysis of urbanized environments (buildings, bridges) • Detecting localized hazards (sinkholes; small landslides) • As most high-res systems have higher repeat frequency tracking of things that change quickly Franz J Meyer, UAF GEOS 657: Microwave RS - 5 Free of Charge vs.