Global Trends in Space Access and Utilization
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By Tamman Montanaro
4 Reusable First Stage Rockets y1 = 15.338 m m1 = 2.047 x 10 kg 5 y2 = 5.115 m m2 = 1.613 x 10 kg By Tamman Montanaro What is the moment of inertia? What is the force required from the cold gas thrusters if we assume constancy. Figure 1. Robbert Goddard’s design of the first ever rocket to fly in 1926. Source: George Edward Pendray. The moment of inertia of a solid disk: rper The Rocket Formula Now lets stack a bunch of these solid disk on each other: Length = l Divide by dt Figure 2: Flight path for the Falcon 9; After separation, the first stage orientates itself and prepares itself for landing. Source: SpaceX If we do the same for the hollow cylinder, we get a moment of inertia Launch of: Specific impulse for a rocket: How much mass is lost? What is the mass loss? What is the moment of inertia about the center of mass for these two objects? Divide by m Figure 3: Falcon 9 first stage after landing on drone barge. Source: SpaceX nd On December 22 2015, the Falcon 9 Orbcomm-2 What is the constant force required for its journey halfway (assuming first stage lands successfully. This is the first ever orbital- that the force required to flip it 90o is the equal and opposite to class rocket landing. From the video and flight logs, we Flip Maneuver stabilize the flip). can gather specifications about the first stage. ⃑ How much time does it take for the first stage to descend? We assume this is the time it takes � Flight Specifications for the first stage to reorientate itself. -
Cape Canaveral Air Force Station Support to Commercial Space Launch
The Space Congress® Proceedings 2019 (46th) Light the Fire Jun 4th, 3:30 PM Cape Canaveral Air Force Station Support to Commercial Space Launch Thomas Ste. Marie Vice Commander, 45th Space Wing Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Ste. Marie, Thomas, "Cape Canaveral Air Force Station Support to Commercial Space Launch" (2019). The Space Congress® Proceedings. 31. https://commons.erau.edu/space-congress-proceedings/proceedings-2019-46th/presentations/31 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Cape Canaveral Air Force Station Support to Commercial Space Launch Colonel Thomas Ste. Marie Vice Commander, 45th Space Wing CCAFS Launch Customers: 2013 Complex 41: ULA Atlas V (CST-100) Complex 40: SpaceX Falcon 9 Complex 37: ULA Delta IV; Delta IV Heavy Complex 46: Space Florida, Navy* Skid Strip: NGIS Pegasus Atlantic Ocean: Navy Trident II* Black text – current programs; Blue text – in work; * – sub-orbital CCAFS Launch Customers: 2013 Complex 39B: NASA SLS Complex 41: ULA Atlas V (CST-100) Complex 40: SpaceX Falcon 9 Complex 37: ULA Delta IV; Delta IV Heavy NASA Space Launch System Launch Complex 39B February 4, 2013 Complex 46: Space Florida, Navy* Skid Strip: NGIS Pegasus Atlantic Ocean: Navy Trident II* Black text – current programs; -
Intelsat, Ltd. (Exact Name of Registrant As Specified in Charter)
SECURITIES AND EXCHANGE COMMISSION Washington, D.C. 20549 FORM 8-K CURRENT REPORT Pursuant to Section 13 or 15(d) of the Securities Exchange Act of 1934 Date of report (Date of earliest event reported): August 12, 2009 Intelsat, Ltd. (Exact Name of Registrant as Specified in Charter) Bermuda 000-50262 98-0346003 (State or Other Jurisdiction (Commission File Number) (IRS Employer of Incorporation) Identification Number) Wellesley House North, 2nd Floor, 90 Pitts Bay Road, Pembroke, Bermuda HM 08 (Address of Principal Executive Offices) (Zip Code) (441) 294-1650 Registrant’s telephone number, including area code n/a (Former Address, If Changed Since Last Report) Check the appropriate box below if the Form 8-K filing is intended to simultaneously satisfy the filing obligation of the registrant under any of the following provisions (see General Instruction A.2. below): ☐ Written communications pursuant to Rule 425 under the Securities Act (17 CFR 230.425) ☐ Soliciting material pursuant to Rule 14a-12 under the Exchange Act (17 CFR 240.14a-12) ☐ Pre-commencement communications pursuant to Rule 14d-2(b) under the Exchange Act (17 CFR 240.14d-2(b)) ☐ Pre-commencement communications pursuant to Rule 13e-4(c) under the Exchange Act (17 CFR 240.13e-4(c)) Item 2.02 Results of Operations and Financial Condition On August 12, 2009, Intelsat, Ltd. issued a press release entitled “Intelsat Reports Second Quarter 2009 Results.” A copy of such press release is furnished as an exhibit to this Current Report on Form 8-K. Item 9.01 Financial Statements and Exhibits (d) Exhibits 99.1 Press Release dated August 12, 2009 entitled “Intelsat Reports Second Quarter 2009 Results” -2- SIGNATURE Pursuant to the requirements of the Securities Exchange Act of 1934, the registrant has duly caused this report to be signed on its behalf by the undersigned hereunto duly authorized. -
“Where Do I Start?” Rides to Space for Scientific and Academic Payloads
SSC02-VII-06 “WHERE DO I START?” RIDES TO SPACE FOR SCIENTIFIC AND ACADEMIC PAYLOADS Matt Bille Tony Williams Tracy Martin Booz, Allen & Hamilton Booz, Allen & Hamilton Booz, Allen & Hamilton 1050 S. Academy Blvd. #148 1050 S. Academy Blvd. #148 1050 S. Academy Blvd. #148 Colorado Springs, CO 80910 Colorado Springs, CO 80910 Colorado Springs, CO 80910 719-570-3172 719-570-3109 719-570-3105 [email protected] [email protected] [email protected] ABSTRACT. The launch problem for small payloads is nowhere as serious as it is for scientific and academic users, who cannot tap the purchasing power available to spacecraft funded by the military and large corporations. The options available for the researcher at a university who has an instrument or a spacecraft are limited, sometimes depressingly so. Dedicated vehicles are usually unaffordable, and secondary payload opportunities require meeting a host of requirements, from payload design to timing to integration, dependent on the needs of the primary payload. In this paper, the authors survey the options available and answer the question, “Where do I start?” Sources of potential rides, including NASA, military, commercial, and non-U.S. programs and organizations were surveyed. The results are presented here, along with recommendations for an improved process which, at low cost, could improve the “matchmaking” system and simplify the obstacle course faced by spacecraft and instrument developers today. Introduction Who To Call First While the technology to reduce the size and The payload developer can start by approaching increase the capability of small scientific and two government programs which aim to help in academic satellites continues to advance, the providing rides to space. -
Space Business Review 11, BSAT-3B Will Be Launched by an Kazakhstan on a Russian Soyuz Vehicle
April 2008 A monthly round-up of space industry developments for the information of our clients and friends. EADS Astrium to Acquire SSTL DISH Selects SS/L for EchoStar XV EADS Astrium announced on April 7 that it On April 22, Space Systems/Loral (SS/L), had entered into an agreement with the announced a contract to build the EchoStar University of Surrey to acquire its 80% XV direct broadcast satellite for DISH stake in Surrey Satellite Technology Network Corporation. Scheduled for launch Limited (SSTL) for an estimated £40-50 in 2010, the spacecraft will be based on million. Based in the United Kingdom, SSTL SS/L’s proven 1300 platform and is designed specializes in the design and manufacture of to support the expansion of DISH Network’s small and micro satellites, including the programming and services. Giove-A test satellite for Europe's Other April Launch Services forthcoming Galileo satellite navigation On April 14, Lockheed Martin Commercial system. The transaction, which remains Launch Services successfully launched the subject to regulatory approvals, will provide ICO G1 satellite for ICO Global the financial and industrial resources Communications (Holdings) Ltd’ from Cape required for SSTL’s expansion and future Canaveral Air Force Station in Florida on an development. It is expected that SSTL will Atlas V 421 vehicle. Built by SS/L based on remain an independent UK company. its 1300 platform, ICO G1 weighed BSAT-3b Contract Awards approximately 6,634 kg at launch, is equipped On April 15, Lockheed Martin Commercial with a 12-meter S-band reflector capable of Space Systems announced its selection by ground-based beam forming that, along with a Japanese satellite operator Broadcasting complementary network of terrestrial Satellite System Corporation (B-SAT) to repeaters, will provide between 10-15 build its next broadcast satellite, designated channels of live television, enhanced BSAT-3b. -
Photo Release -- Space Systems/Loral-Built Telstar 11N Satellite on Track with Post Launch Maneuvers
Photo Release -- Space Systems/Loral-Built Telstar 11N Satellite On Track With Post Launch Maneuvers Solar Arrays Deployed On Schedule Following Successful Launch PALO ALTO, Calif., Feb 27, 2009 (GlobeNewswire via COMTEX News Network) -- Space Systems/Loral (SS/L), a subsidiary of Loral Space & Communications (Nasdaq:LORL) and the leading provider of commercial satellites, today announced that the Telstar 11N satellite built for Telesat, one of the world's leading fixed satellite services operators, is performing post launch maneuvers according to plan. The satellite's solar arrays deployed on schedule several hours after separation, following yesterday's successful launch aboard a Zenit-3SLB rocket from the Baikonur Space Center in Kazakhstan. Tomorrow the satellite will begin firing its thrusters to maneuver into its final geosynchronous orbit. A photo accompanying this release is available at http://www.globenewswire.com/newsroom/prs/?pkgid=5941 "We are proud to know that this high-power satellite will help make information and entertainment more accessible around the world," said John Celli, President and Chief Operating Officer of Space Systems/Loral. "Telstar 11N demonstrates the flexibility of our standard 1300 satellite platform, which in this case was engineered to accommodate a smaller launch vehicle. It is this flexibility together with long term proven reliability that have helped SS/L achieve more than 40 percent market share over the past five years." When it reaches its final geosynchronous orbit, Telstar 11N will support video and data applications in North America, Western Europe, and Africa. Space Systems/Loral designed the satellite with a unique Atlantic Ocean beam, which will help Telesat meet growing demand for mobile broadband from both commercial and government customers in shipping and aviation. -
ESPA Ring Datasheet
PAYLOAD ADAPTERS | ESPA ESPA THE EVOLVED SECONDARY PAYLOAD ADAPTER ESPA mounts to the standard NSSL (formerly EELV) interface bolt pattern (Atlas V, Falcon 9, Delta IV, OmegA, Vulcan, Courtesy of Lockheed Martin New Glenn) and is a drop-in component in the launch stack. Small payloads mount to ESPA ports featuring either a Ø15-inch bolt circle with 24 fasteners or a 4-point mount with pads at each corner of a 15-inch square; both of these interfaces have become small satellite standards. ESPA is qualified to carry 567 lbs (257 kg), and a Heavy interface Courtesy of NASA (with Ø5/16” fastener hardware) has been introduced with a capacity of 991 lbs (450 kg). All small satellite mass capabilities require the center of gravity (CG) to be within 20 inches (50.8 cm) of the ESPA port surface. Alternative configurations can be accommodated. ESPA GRANDE ESPA Grande is a more capable version of ESPA with Ø24-inch ports; the ring height is typically 42 inches. The Ø24-inch port has been qualified by test to Courtesy of ORBCOMM & Sierra Nevada Corp. carry small satellites up to 1543 lb (700 kg). ESPA ESPA IS ADAPTABLE TO UNIQUE MISSION REQUIREMENTS • The Air Force’s STP-1 mission delivered multiple small satellites on an Atlas V. • NASA’s Lunar Crater Observation and Sensing Satellite (LCROSS): ESPA was the spacecraft hub for the LCROSS shepherding satellite in 2009. • ORBCOMM Generation 2 (OG2) launched stacks of two and three ESPA Grandes on two different Falcon 9 missions and in total deployed 17 satellites. -
GLONASS Spacecraft
INNO V AT IO N The task of designing and developing the GLONASS GLONASS spacecraft fell to the Scientific Production Association of Applied Mechan ics (Nauchno Proizvodstvennoe Ob"edinenie Spacecraft Prikladnoi Mekaniki or NPO PM) , located near Krasnoyarsk in Siberia. This major aero Nicholas L. Johnson space industrial complex was established in 1959 as a division of Sergei Korolev 's Kaman Sciences Corporation Expe1imental Design Bureau (Opytno Kon struktorskoe Byuro or OKB). (Korolev , among other notable achievements , led the Fourteen years after the launch of the effort to develop the Soviet Union's first first test spacecraft, the Russian Global Nav launch vehicle - the A launcher - which igation Satellite System (Global 'naya Navi placed Sputnik 1 into orbit.) The founding gatsionnaya Sputnikovaya Sistema or and current general director and chief GLONASS) program remains viable and designer is Mikhail Fyodorovich Reshetnev, essentially on schedule despite the economic one of only two still-active chief designers and political turmoil surrounding the final from Russia's fledgling 1950s-era space years of the Soviet Union and the emergence program. of the Commonwealth of Independent States A closed facility until the early 1990s, (CIS). By the summer of 1994, a total of 53 NPO PM has been responsible for all major GLONASS spacecraft had been successfully Russian operational communications, navi Despite the significant economic hardships deployed in nearly semisynchronous orbits; gation, and geodetic satellite systems to associated with the breakup of the Soviet Union of the 53 , nearly 12 had been normally oper date. Serial (or assembly-line) production of and the transition to a modern market economy, ational since the establishment of the Phase I some spacecraft, including Tsikada and Russia continues to develop its space programs, constellation in 1990. -
The Annual Compendium of Commercial Space Transportation: 2012
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2012 February 2013 About FAA 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 (2013) 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. • i • Federal Aviation Administration’s Office of Commercial Space Transportation Dear Colleague, 2012 was a very active year for the entire commercial space industry. In addition to all of the dramatic space transportation events, including the first-ever commercial mission flown to and from the International Space Station, the year was also a very busy one from the government’s perspective. It is clear that the level and pace of activity is beginning to increase significantly. -
In Flight Research on Aerothermodynamics (Atd) and Thermal Protection Systems (Tps) for Space Transportation Systems
1 IN FLIGHT RESEARCH ON AEROTHERMODYNAMICS (ATD) AND THERMAL PROTECTION SYSTEMS (TPS) FOR SPACE TRANSPORTATION SYSTEMS Jean Muylaert (1) , M. Ivanov (2) ,V. A. Danilkin (2), C. Park (3), H. Ritter (1), G. Ortega (1) (1)ESA/ESTEC, Keplerlaan 1, 2200 AG Noordwijk, The Netherlands, Email: [email protected], [email protected], [email protected] (2) ITAM Email : [email protected] (3) SRC-MDB Email: [email protected] (4) KAIST Email:CPark216 @kaist.ac.kr ABSTRACT The paper addresses a strategy to perform in flight such as wake closure, capsule shoulder heating and TPS gap / step micro aero effects could be analysed. research on Aerothermodynamics (ATD) and Thermal Protection Systems (TPS) taking advantage of the low 4. Aero-assist Hopping being a General Study cost VOLNA and SHTIL class of launchers. Programme (GSP) internal activity to assess the A series of flight test beds will be addressed and their feasibility of a low cost flight gathering data on aero- relevance discussed as to the gathering of critical braking and aero-assist strategies. Aerothermodynamic and TPS related data for design It is concluded that these low cost class of in flight tool qualification and associated physical model research initiatives are “the” way forwards to improve validation. the tools to be used for design of future re-entry space transportation systems. The paper reviews 4 initiatives, all of them of the class flying test beds and launched by the VOLNA launcher: 1. BACKGROUND 1. The EXPERT (European Experimental re-entry Test bed) project where the objective is to acquire hypersonic The design of space transportation systems is always flight data for improved understanding of natural and driven by worst case scenario’s involving estimations of roughness induced boundary layer transition, catalysis uncertainties associated with critical phenomena. -
Space Industry
Spring 2013 Industry Study Final Report Space Industry Dwight D. Eisenhower School for National Security and Resource Strategy National Defense University Fort McNair, Washington, D.C. 20319-5062 ii i 1 SPACE 2013 ABSTRACT: Today’s U.S. national security space systems enable vital functions such as strategic warning, global command and control, intelligence, and communications while also touching nearly every aspect of modern life - from personal navigation systems to receiving near real-time information from across the globe. However, American space power is not guaranteed – particularly as the nation enters an era of fiscal austerity and conflicting budget priorities. Significant challenges that must be addressed include limited federal funds, rising costs, and a fragile supply chain. Additionally, as the U.S. rebalances strategic focus to the Asia-Pacific, limited regional satellite communication capacity and potential vulnerabilities to U.S. space systems also pose a threat. To mitigate these challenges, this study recommends the U.S. Department of Defense implement a policy of selective disaggregation to improve space system resiliency and maintain a steady funding profile for national security satellites. However, such a strategy is not without costs: hoped for increases in national security space program affordability will likely not materialize over the long-term as savings realized in satellite manufacturing will simply shift cost and complexity to the ground equipment and launch segments. CDR Vince Baker, U.S. Navy Mr. Stephen Burke, Department of the Air Force Mr. Patrick Dunn, Department of State COL John Eggert, U.S. Army Dr. Ivy Estabrooke, Department of the Navy COL Gregory Graves, U.S. -
The European Launchers Between Commerce and Geopolitics
The European Launchers between Commerce and Geopolitics Report 56 March 2016 Marco Aliberti Matteo Tugnoli Short title: ESPI Report 56 ISSN: 2218-0931 (print), 2076-6688 (online) Published in March 2016 Editor and publisher: European Space Policy Institute, ESPI Schwarzenbergplatz 6 • 1030 Vienna • Austria http://www.espi.or.at Tel. +43 1 7181118-0; Fax -99 Rights reserved – No part of this report may be reproduced or transmitted in any form or for any purpose with- out permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “Source: ESPI Report 56; March 2016. All rights reserved” and sample transmission to ESPI before publishing. ESPI is not responsible for any losses, injury or damage caused to any person or property (including under contract, by negligence, product liability or otherwise) whether they may be direct or indirect, special, inciden- tal or consequential, resulting from the information contained in this publication. Design: Panthera.cc ESPI Report 56 2 March 2016 The European Launchers between Commerce and Geopolitics Table of Contents Executive Summary 5 1. Introduction 10 1.1 Access to Space at the Nexus of Commerce and Geopolitics 10 1.2 Objectives of the Report 12 1.3 Methodology and Structure 12 2. Access to Space in Europe 14 2.1 European Launchers: from Political Autonomy to Market Dominance 14 2.1.1 The Quest for European Independent Access to Space 14 2.1.3 European Launchers: the Current Family 16 2.1.3 The Working System: Launcher Strategy, Development and Exploitation 19 2.2 Preparing for the Future: the 2014 ESA Ministerial Council 22 2.2.1 The Path to the Ministerial 22 2.2.2 A Look at Europe’s Future Launchers and Infrastructure 26 2.2.3 A Revolution in Governance 30 3.