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ATLAS II | At-Large Summit London 2014
EN AL-ATLAS-02-DCL-01-01-EN ORIGINAL: English DATE: 26 June 2014 STATUS: Final The 2nd At-Large Summit (ATLAS II) FINAL DECLARATION Introductory Text By the Staff of ICANN Representatives of approximately one hundred and fifty (150) At-Large Structures (“ALSes”) from five Regional At-Large Organizations (“RALOs”) representing ICANN's global At-Large Community met at the 2nd At-Large Summit (ATLAS II) as part of the 50th ICANN meeting in London, United Kingdom between 21-26 June 2014. Amongst the various activities of the Summit were five Thematic Groups on issues of concern to the At-Large Community. The subjects for the Thematic Groups were selected by the representatives of ALSes. Each Summit participant was allocated to the Thematic Group according to his/her preference. The five Thematic Groups were: Thematic Group 1 (TG1): Future of Multi-Stakeholder Models Thematic Group 2 (TG2): The Globalization of ICANN Thematic Group 3 (TG3): Global Internet: The User Perspective Thematic Group 4 (TG4): ICANN Transparency and Accountability Thematic Group 5 (TG5): At-Large Community Engagement in ICANN All Thematic Groups commenced their work on Saturday 21 June 2014, the opening day of the Summit, and then each met in four individual breakout sessions during the Summit to finalize their statements. The text that follows, including the appendix which is an integral part of the Final Declaration, was endorsed by approximately 150 ALSes on the morning of Thursday, 26 June 2014 and then endorsed by the At-Large Advisory Committee (ALAC) by acclamation on the same day. The Final Declaration is to be presented to the Board of ICANN at its public session in London, United Kingdom on Thursday, 26 June 2014. -
Launch Options for the Future: a Buyer's Guide (Part 7 Of
— Chapter 3 Enhanced Baseline CONTENTS , Page Improving the Shuttle . 27 Advanced Solid Rocket Motors (ASRMs) . 27 Liquid Rocket Boosters (LRBs) . 28 Lighter Tanks . 29 Improving Shuttle Ground Operations . 29 Improving Existing ELVs . 29 Delta . 30 Atlas-Centaur . ● ● . .* . 30 Titan . ● . ✎ ✎ . 30 Capability . ✎ . ✎ ✎ . ● ✎ ✎ . 30 Table 3-1. Theoretical Lift Capability of Enhanced U.S. Launch Systems. 31 Chapter 3 Enhanced Baseline The ENHANCED BASELINE option is the U.S. Government’s “Best Buy” if . it desires a space program with current or slightly greater levels of activity. By making in- cremental improvements to existing launch vehicles, production and launch facilities, the U.S. could increase its launch capacity to about 1.4 million pounds per year to LEO. The investment required would be low compared to building new vehicles; however, the ade- quacy of the resulting fleet resiliency and dependability is uncertain. This option would not provide the low launch costs (e.g. 10 percent of current costs) sought for SDI deploy- ment or an aggressive civilian space initiative, like a piloted mission to Mars, IMPROVING THE SHUTTLE The Shuttle, though a remarkable tech- . reducing the number of factory joints and nological achievement, never achieved its in- the number of parts, tended payload capacity and recent safety . designing the ASRMs so that the Space modifications have further degraded its per- Shuttle Main Engines no longer need to formance by approximately 4,800 pounds. be throttled during the region of maxi- Advanced Solid Rocket Motors (ASRMs) or mum dynamic pressure, Liquid Rocket Boosters (LRBs) have the potential to restore some of this perfor- ● replacing asbestos-bearing materials, mance; studies on both are underway. -
Jacques Tiziou Space Collection
Jacques Tiziou Space Collection Isaac Middleton and Melissa A. N. Keiser 2019 National Air and Space Museum Archives 14390 Air & Space Museum Parkway Chantilly, VA 20151 [email protected] https://airandspace.si.edu/archives Table of Contents Collection Overview ........................................................................................................ 1 Administrative Information .............................................................................................. 1 Biographical / Historical.................................................................................................... 1 Scope and Contents........................................................................................................ 2 Arrangement..................................................................................................................... 2 Names and Subjects ...................................................................................................... 2 Container Listing ............................................................................................................. 4 Series : Files, (bulk 1960-2011)............................................................................... 4 Series : Photography, (bulk 1960-2011)................................................................. 25 Jacques Tiziou Space Collection NASM.2018.0078 Collection Overview Repository: National Air and Space Museum Archives Title: Jacques Tiziou Space Collection Identifier: NASM.2018.0078 Date: (bulk 1960s through -
Atlas As a Human Rated LV
AtlasAtlas As As A A Human Human RatedRated LV LV STAIF Conference 2006 Lockheed Martin Space Systems Company Atlas for Human Spaceflight 15 Feb 2006 1 © 2006 Lockheed Martin Corporation. All Rights Reserved Reliable and Versatile Launch Vehicle Family Atlas I Atlas II Atlas IIA Atlas IIAS Atlas IIIA Atlas IIIB Atlas V-400 Atlas V-500 AC-69 AC-102 AC-105 AC-108 AC-201 AC-204 AV-001 AV-003 Jul 1990 Dec 1991 Jun 1992 Dec 1993 May 2000 Feb 2002 Aug 2002 Jul 2003 8/11 10/10 23/23 30/30 2/2 4/4 4/4 3/3 Legend: First Flight X/Y X successes in Y flights •8 of 8 First Flight Successes •78 Consecutive Successful Atlas Centaur Flights •100% Mission Success Atlas II, IIA, IIAS, III & V Families •487 Total Launch Successes Since Atlas Program Inception Mission Success—One Launch at a Time Atlas for Human Spaceflight 15 Feb 2006 2 AV-010 Launch • January 19, 2006 • NASA Pluto New Horizons Spacecraft • First 551 configuration • First Block 2 Fault Tolerant Avionics • First Block B SRB • Nuclear certified • Nominal flight profile • Injection conditions well within 1 sigma – C3, RLA, DLA Fastest Spacecraft Ever Launched Atlas for Human Spaceflight 15 Feb 2006 3 Atlas Evolution History Atlas I/II Family Atlas III Family Atlas V Family 5-m PLF ) 30 GSO Kit T m ( y 26 t i l Avionics i Single Common Upgrade b Engine a 22 Centaur Centaur p a C 3.8-m . Common c 18 r LO2 Core i Tank Booster C Stretch ) 14 m n 0 2 10 Liquid 2 SRBs ( Strap-ons m RD-180 SRBs k 6 Engine 7 0 Atlas I Atlas IIAS Atlas IIIA Atlas IIIB Atlas V Atlas V Atlas V 4 2 Atlas II (SEC) (DEC) -
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 . -
ATLAS I/O Overview Peter Van Gemmeren (ANL) [email protected] for Many in ATLAS
ATLAS I/O Overview Peter van Gemmeren (ANL) [email protected] for many in ATLAS 8/23/2018 Peter van Gemmeren (ANL): ATLAS I/O Overview 1 High level overview of ATLAS Input/Output framework and data persistence. Athena: The ATLAS event processing framework The ATLAS event data model Persistence: Writing Event Data: OutputStream and OutputStreamTool Overview Reading Event Data: EventSelector and AddressProvider ConversionSvc and Converter Timeline Run 2: AthenaMP, xAOD Run 3: AthenaMT Run 4: Serialization, Streaming, MPI, ESP 8/23/2018 Peter van Gemmeren (ANL): ATLAS I/O Overview 2 Simulation, reconstruction, and analysis/derivation are run as part of the Athena framework: Using the most current (transient) version of the Event Data Model Athena software architecture belongs to the blackboard family: Athena: The StoreGate is the Athena implementation of the blackboard: A proxy defines and hides the cache-fault ATLAS event mechanism: Upon request, a missing data object processing instance can be created and added to the transient data store, retrieving it from framework persistent storage on demand. Support for object identification via data type and key string: Base-class and derived-class retrieval, key aliases, versioning, and inter-object references. 8/23/2018 Peter van Gemmeren (ANL): ATLAS I/O Overview 3 Athena is used for different workflows in Reconstruction, Simulation and Analysis (mainly Derivation). Total CPU Total Read (incl. Total Write (w/o evt-loop Step ROOT compression ROOT and P->T) compression) time -
Exploring Space
EXPLORING SPACE: Opening New Frontiers Past, Present, and Future Space Launch Activities at Cape Canaveral Air Force Station and NASA’s John F. Kennedy Space Center EXPLORING SPACE: OPENING NEW FRONTIERS Dr. Al Koller COPYRIGHT © 2016, A. KOLLER, JR. All rights reserved. No part of this book may be reproduced without the written consent of the copyright holder Library of Congress Control Number: 2016917577 ISBN: 978-0-9668570-1-6 e3 Company Titusville, Florida http://www.e3company.com 0 TABLE OF CONTENTS Page Foreword …………………………………………………………………………2 Dedications …………………………………………………………………...…3 A Place of Canes and Reeds……………………………………………….…4 Cape Canaveral and The Eastern Range………………………………...…7 Early Missile Launches ...……………………………………………….....9-17 Explorer 1 – First Satellite …………………….……………………………...18 First Seven Astronauts ………………………………………………….……20 Mercury Program …………………………………………………….……23-27 Gemini Program ……………………………………………..….…………….28 Air Force Titan Program …………………………………………………..29-30 Apollo Program …………………………………………………………....31-35 Skylab Program ……………………………………………………………….35 Space Shuttle Program …………………………………………………..36-40 Evolved Expendable Launch Program ……………………………………..41 Constellation Program ………………………………………………………..42 International Space Station ………………………………...………………..42 Cape Canaveral Spaceport Today………………………..…………………43 ULA – Atlas V, Delta IV ………………………………………………………44 Boeing X-37B …………………………………………………………………45 SpaceX Falcon 1, Falcon 9, Dragon Capsule .………….........................46 Boeing CST-100 Starliner …………………………………………………...47 Sierra -
N AS a Facts
National Aeronautics and Space Administration NASA’s Launch Services Program he Launch Services Program (LSP) manufacturing, launch operations and rockets for launching Earth-orbit and Twas established at Kennedy Space countdown management, and providing interplanetary missions. Center for NASA’s acquisition and added quality and mission assurance in In September 2010, NASA’s Launch program management of expendable lieu of the requirement for the launch Services (NLS) contract was extended launch vehicle (ELV) missions. A skillful service provider to obtain a commercial by the agency for 10 years, through NASA/contractor team is in place to launch license. 2020, with the award of four indefinite meet the mission of the Launch Ser- Primary launch sites are Cape Canav- delivery/indefinite quantity contracts. The vices Program, which exists to provide eral Air Force Station (CCAFS) in Florida, expendable launch vehicles that NASA leadership, expertise and cost-effective and Vandenberg Air Force Base (VAFB) has available for its science, Earth-orbit services in the commercial arena to in California. and interplanetary missions are United satisfy agencywide space transporta- Other launch locations are NASA’s Launch Alliance’s (ULA) Atlas V and tion requirements and maximize the Wallops Flight Facility in Virginia, the Delta II, Space X’s Falcon 1 and 9, opportunity for mission success. Kwajalein Atoll in the South Pacific’s Orbital Sciences Corp.’s Pegasus and facts The principal objectives of the LSP Republic of the Marshall Islands, and Taurus XL, and Lockheed Martin Space are to provide safe, reliable, cost-effec- Kodiak Island in Alaska. Systems Co.’s Athena I and II. -
Atlas Packaging Server III TELCO Datasheet
TM ATLAS III Packaging Server: TELCO Linux® based live or VOD Media Distribution Server designed to serve 80+ channels with support for up to 42,000 users at 1 mbps. Works with most STBs and mobile devices expecting HLS and DASH. Supports live streams from IRDs, IP cameras, origin servers, and H.265 or H.264 encoders or transcoders. Used as an Origin (Main) or Edge server for live or VOD. Supports HLS Timeshift or Catch- up TV, to rewind, pause, and fast forward live streams. Converts TS, DASH, RTMP, or HLS to UDP unicast or multicast TS wrapped with HLS or DASH when needed. We provide 3 TB of SSD, network speed of 20 Gbps (up to 40 Gbps with optional fiber card), and up to 128 GB of RAM on board for sustained performance. Results affected by your bandwidth. Features Overview Media distribution server designed for both Live and Stored (VOD) applications Packagers are the newly respected Swiss Army Knife of the Ingests H.265 or H.264 live streams over IP, then adds wrappers streaming industry. They are designed to segment H.264 such as MPEG-DASH, HLS, or RTMP transport streams into pre-determined chunks and package or Supports both HD and SD H.265/HEVC and H.264/MPEG-4 AVC wrap the segmented streams into HLS or DASH. A third Packaging or Origin or Edge server function they are tasked with is serving these streams to thousands of users simultaneously. Packagers often also apply Inbound Protocols: Multi-bitrate File, RTMP, RTSP, MPEG-TS, HLS DRM or content protection keys to secure the streams. -
Space Transportation Atlas V / Auxiliary Payload Overview Space
SpaceSpace TransportationTransportation AtlasAtlas VV // AuxiliaryAuxiliary PayloadPayload OverviewOverview LockheedLockheed MartinMartin SpaceSpace SystemsSystems CompanyCompany JimJim EnglandEngland (303)(303) 977-0861977-0861 ProgramProgram Manager,Manager, AtlasAtlas GovernmentGovernment ProgramsPrograms BusinessBusiness DevelDevelopmentopment andand AdvancedAdvanced ProgramsPrograms 33 AugustAugust 20062006 1 Video – Take a Ride 2 ReliableReliable && VersatileVersatile LaunchLaunch VehicleVehicle FamilyFamily RReettiirreedd RReettiirreedd Atlas I AC-69 RReettiirreedd Jul 1990 Atlas II AC-102 RReettiirreedd 8/11 Dec 1991 Atlas IIA 10/10 AC-105 RReettiirreedd Jun 1992 • Consecutive Successful Atlas CentaurAtlas Flights: IIAS 79 Retired • First Flight Successes: 823/23 of 8 AC-108 Retired • Mission Success: 100% Atlas II, IIA, IIAS,Dec 1993 IIIA, IIIB, and V Families Atlas IIIA First Flight • Retired Variants: A, B, C, D, E, F, G, H,30/30 I, II, IIA, IIAS,AC-201 IIIA, IIIB May 2000 Atlas IIIB X/Y AC-204 2/2 X Successes / Y FlightsFeb 2002 Atlas V-400 AV-001 4/4 Mission Success: One Launch at a Time 4/4 Aug 2002 Atlas V-500 AV-003 4/4 Jul 2003 3/3 3 RecentRecent AtlasAtlas // CentaurCentaur EvolutionEvolution Atlas I / II Family Atlas III Family Atlas V Family dd dd iirree iirree eett eett RR RR 5-m PLF 30 GSO Kit 26 Single Avionics Engine Common Upgrade 22 Centaur Centaur 3.8-m 18 Common LO2 Core Tank Booster Stretch 14 10 Liquid SRBs Strap-ons RD-180 SRBs 6 Engine Atlas I Atlas IIAS Atlas IIIA Atlas IIIB Atlas V Atlas V Atlas V 407 -
Titan Iv Requirements
OFFICE OF THE INSPECTOR GENERAL TITAN IV REQUIREMENTS Report No. 94-089 April 21, 1994 Department of Defense Additional Copies To obtain additional copies of this report, contact the Secondary Reports Distribution Unit, Audit Planning and Technical Support Directorate, at (703) 614-6303 (DSN 224-6303) or FAX (703) 614-8542. Suggestions for Future Audits To suggest ideas for or to request future audits, contact the Planning and Coordination Branch, Audit Planning and Technical Support Directorate, at (703) 614-1868 (DSN 224-1868) or FAX (703) 614-8542. Ideas and requests can also be mailed to: Inspector General, Department of Defense OAIG-AUD (ATTN: APTS Audit Suggestions) 400 Army Navy Drive (Room 801) Arlington, Virginia 22202-2884 DoD Hotline To report fraud, waste, or abuse, call the DoD Hotline at (800) 424-9098 (DSN 223-5080) or write to the DoD Hotline, The Pentagon, Washington, D.C. 20301-1900. The identity of writers and callers is fully protected. Acronyms FYDP Future Years Defense Program IV&V Independent Verification and Validation OSD Office of the Secretary of Defense RFP Request for Proposal SLAG Space Launch Advisory Group SPO System Program Office SRM Solid Rocket Motor SRMU Solid Rocket Motor Upgrade INSPECTOR GENERAL DEPARTMENT OF DEFENSE 400 ARMY NAVY DRIVE ARLINGTON, VIRGINIA 22202-2884 April 21, 1994 MEMORANDUM FOR ASSISTANT SECRETARY OF THE AIR FORCE (FINANCIAL MANAGEMENT AND COMPTROLLER) SUBJECT: Audit Report on Titan IV Requirements (Report No. 94-089) We are providing this audit report for your review and comments. It discusses requirements for the Titan IV expendable launch vehicle and for independent validation and verification of critical computer resources. -
Masa Hashimoto
Public-Private Partnerships in Space Projects: An Analysis of Stakeholder Dynamics by Masafumi Hashimoto Master of Science in Physics Osaka University, 2002 Bachelor of Science in Physics Osaka University, 1999 Submitted to the Engineering Systems Division in Partial Fulfillment of the Requirements for the Degree of Master of Science in Technology and Policy at the Massachusetts Institute of Technology June 2009 2009 Masafumi Hashimoto. All rights reserved. The author hereby grants to MIT permission to reproduce and to distribute publicly paper and electronic copies of this thesis document in whole or in part in any medium now know or hereafter created. Signature of Author ………………………………………………………………………… Technology and Policy Program, Engineering Systems Division May 8, 2009 Certified by ………………………………………………………………………………… Annalisa L. Weigel Jerome C. Hunsacker Assistant Professor of Aeronautics and Astronautics and Engineering Systems Thesis Supervisor Accepted by ……………………………………………………………………………….. Dava J. Newman Professor of Aeronautics and Astronautics and Engineering Systems Director, Technology and Policy Program Public-Private Partnerships in Space Projects: An Analysis of Stakeholder Dynamics by Masafumi Hashimoto Submitted to the Engineering Systems Division on May 8, 2009 in Partial Fulfillment of the Requirements for the Degree of Master of Science in Technology and Policy Abstract In Public-Private Partnerships (PPPs), private partners assume more responsibility for public projects than in traditional approaches. The larger responsibility of the private partner is expected to improve efficiencies of the project. However, it also increases potential challenges such as conflicts of interest. If the dynamic structures which cause challenges in PPPs are identified, they will help to predict potential challenges in future PPP projects. Therefore, this research develops a dynamics model of which challenges arise in the application of PPP approaches to space projects.