Airspace Integration in an Era of Growing Launch Operations
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Selection of Favorite Reusable Launch Vehicle Concepts by Using the Method of Pairwise Comparison
Selection of Favorite Reusable Launch Vehicle Concepts by using the Method of Pairwise Comparison Robert A. Goehlich Keio University, Department of System Design Engineering, Ohkami Laboratory, 3-14-1 Hiyoshi, Kohoku-ku, Yokohama 223-8522, JAPAN, Mobile: +81-90-1767-1667, Fax: +81-45-566-1778 email: [email protected], Internet: www.Robert-Goehlich.de Abstract The attempt of this paper is to select promising Reusable Launch Vehicle (RLV) concepts by using a formal evaluation procedure. The vehicle system is divided into design features. Every design feature can have alternative characteristics. All combinations of design features and characteristics are compared pairwise with each other with respect to relative importance for a feasible vehicle concept as seen from technical, economic, and political aspects. This valuation process leads to a ranked list of design features for suborbital and orbital applications. The result is a theoretical optimized suborbital and orbital vehicle each. The method of pairwise comparison allows to determine not only ranking but also assessing the relative weight of each feature compared to others. Keywords: Pairwise Comparison, Reusable Launch Vehicle, Space Tourism Introduction The potential for an introduction of reusable launch vehicles is derived from an expected increasing demand for transportation of passengers in the decades to come. The assumed future satellite market does not justify to operate reusable launch vehicles only for satellites due to a low launch rate. Finding feasible vehicle concepts, which satisfy operator’s, passenger’s, and public’s needs, will be a challenging task. Since it is not possible to satisfy all space tourism markets by one vehicle, different vehicles that are capable to serve one particular segment (suborbital or orbital) are needed. -
Launcherone Success Opens New Space Access Gateway Guy Norris January 22, 2021
1/22/21 7:05 1/6 LauncherOne Success Opens New Space Access Gateway Guy Norris January 22, 2021 With San Nicolas Island far below, LauncherOne headed for polar orbit. Credit: Virgin Orbit Virgin Orbit had barely tweeted news of the successful Jan. 17 space debut of its LauncherOne vehicle on social media when new launch contracts began arriving in the company’s email inbox. A testament to the pent-up market demand for small-satellite launch capability, the speedy reaction to the long-awaited demonstration of the new space-access vehicle paves the way for multiple follow-on Virgin Orbit missions by year-end and a potential doubling of the rate in 2022. First successful privately developed air-launched, liquid-fueled rocket Payloads deployed for NASA’s Venture Class Launch Services program The glitch-free !ight of LauncherOne on its second demonstration test was a critical and much-welcomed milestone for the Long Beach, California-based company. Coming almost nine years a"er the air-launch concept was #rst unveiled by Virgin founder Richard Branson, and six years a"er the start of full-scale development, the !ight followed last May’s #rst demonstration mission, which ended abruptly when the rocket motor shut o$ a"er just 4 sec. 1/22/21 7:05 2/6 A"er an exhaustive analysis and modi#cations to beef up the oxidizer feed line at the heart of the #rst !ight failure, the path to the Launch Demo 2 test was then delayed until January 2021 by the COVID-19 pandemic. With the LauncherOne system now proven, design changes veri#ed and the #rst 10 small satellites placed in orbit, Virgin Orbit is already focusing on the next steps to ramp up its production and launch-cadence capabilities. -
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. -
Redalyc.Status and Trends of Smallsats and Their Launch Vehicles
Journal of Aerospace Technology and Management ISSN: 1984-9648 [email protected] Instituto de Aeronáutica e Espaço Brasil Wekerle, Timo; Bezerra Pessoa Filho, José; Vergueiro Loures da Costa, Luís Eduardo; Gonzaga Trabasso, Luís Status and Trends of Smallsats and Their Launch Vehicles — An Up-to-date Review Journal of Aerospace Technology and Management, vol. 9, núm. 3, julio-septiembre, 2017, pp. 269-286 Instituto de Aeronáutica e Espaço São Paulo, Brasil Available in: http://www.redalyc.org/articulo.oa?id=309452133001 How to cite Complete issue Scientific Information System More information about this article Network of Scientific Journals from Latin America, the Caribbean, Spain and Portugal Journal's homepage in redalyc.org Non-profit academic project, developed under the open access initiative doi: 10.5028/jatm.v9i3.853 Status and Trends of Smallsats and Their Launch Vehicles — An Up-to-date Review Timo Wekerle1, José Bezerra Pessoa Filho2, Luís Eduardo Vergueiro Loures da Costa1, Luís Gonzaga Trabasso1 ABSTRACT: This paper presents an analysis of the scenario of small satellites and its correspondent launch vehicles. The INTRODUCTION miniaturization of electronics, together with reliability and performance increase as well as reduction of cost, have During the past 30 years, electronic devices have experienced allowed the use of commercials-off-the-shelf in the space industry, fostering the Smallsat use. An analysis of the enormous advancements in terms of performance, reliability and launched Smallsats during the last 20 years is accomplished lower prices. In the mid-80s, a USD 36 million supercomputer and the main factors for the Smallsat (r)evolution, outlined. -
Sustainable Planning for Space Tourism
Vertaisarviointitunnuksen merkitseminen julkaisuihin Käyttöoikeuden saanut tiedekustantaja merkitsee tunnuksella vertais- arvioinnin läpikäyneet kirjat ja artikkelit. Tunnus tulee asetella julkai- suun siten, että käy yksiselitteisesti ilmi, mitkä kirjoituksista on vertai- sarvioitu. Tunnuksesta on olemassa kaksi versiota: tekstillä varustettu ja tekstitön. ARTIKKELI 1. Tunnuksen tekstiä sisältävä versio liitetään aina vertaisarvioitu- ja kirjoituksia sisältävän lehden tai kirjan nimiölehdelle tai muualle julkaisutietojen yhteyteen. Jos julkaisu on kokonaan vertaisarvioitu, merkintä nimiösivuilla tai vastaavalla riittää. 2. Kun julkaisu sisältää sekä arvioituja että arvioimattomia kirjoituk- sia, tunnus merkitään myös: • sisällysluetteloon (tekstitön versio) Sustainable• yksittäisten vertaisarvioitujen lukujen/artikkelien planning yhteyteen for space tourism (kumpi tahansa versio) Annette3. Elektronisissa Toivonen julkaisuissa on suositeltavaa merkitä tunnuksen teks- tillä varustettu versio kaikkien vertaisarvioitujen artikkelien etusivul- Universityle, jotta kuvan merkitys of Lapland, käy ilmi yksittäistä Multidimensional artikkelia tarkastelevalle Tourism Institute (MTI) lukijalle. Alla on esitetty, miten tunnus merkitään julkaisun nimiösivulle, sisäl- lysluetteloon sekä painettuun ja elektroniseen artikkeliin. Esimerkkejä merkintätavoista voi katsoa myös tunnusta käyttävien kustantajien julkaisuista. Abstract This article concentrates on planning and development for future space tourism. It focuses on environmentally oriented sustainable -
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. -
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 . -
International Legal Regulation of Space Tourism
International Legal Regulation of Space Tourism Irina Rуzhenko1 Ph.D. in Law, Associate Professor, Kherson State University (Kherson, Ukraine) E-mail: [email protected] https://orcid.org/0000-0002-9208-2132 Olena Halahan2 Senior lecturer, Kherson State Maritime Academy (Kherson, Ukraine) E-mail: [email protected] https://orcid.org/0000-0001-8392-6965 Rуzhenko, Irina, and Olena Halahan (2020) International Legal Regulation of Space Tourism. Advanced Space Law, Volume 5, 83-90. https://doi.org/10.29202/asl/2020/5/8 The article analyzes the state of legal regulation of the process of organization and implementation of space tourism, defines the features of its application and its place in modern international space law. The legal norms in the field of space travel and the legal bases of their organization were analyzed. An attempt to analyze the legal status of persons taking part in space missions was made. The issue of the international legal personality of the participants of the space tourist service contract was investigated. Particular attention was paid to the legal status of space tourists. The content of the definition of “cosmonauts as messengers of humanity into space” was analyzed. The issues of the risks inherent in space tourism activities and the international legal liability of the parties to the space tourist services contract were considered. It has been stated that a space traveler has a certain amount of rights and obligations throughout the period, from the beginning of preparation to the journey and ending with the period after returning to Earth. An indicative list of space tourists’ rights has been restated, and examples of their obligations and limitations in time and space have been provided. -
Sale Price Drives Potential Effects on DOD and Commercial Launch Providers
United States Government Accountability Office Report to Congressional Addressees August 2017 SURPLUS MISSILE MOTORS Sale Price Drives Potential Effects on DOD and Commercial Launch Providers Accessible Version GAO-17-609 August 2017 SURPLUS MISSILE MOTORS Sale Price Drives Potential Effects on DOD and Commercial Launch Providers Highlights of GAO-17-609, a report to congressional addressees Why GAO Did This Study What GAO Found The U.S. government spends over a The Department of Defense (DOD) could use several methods to set the sale billion dollars each year on launch prices of surplus intercontinental ballistic missile (ICBM) motors that could be activities as it strives to help develop a converted and used in vehicles for commercial launch if current rules prohibiting competitive market for space launches such sales were changed. One method would be to determine a breakeven and assure its access to space. Among price. Below this price, DOD would not recuperate its costs, and, above this others, one launch option is to use price, DOD would potentially save. GAO estimated that DOD could sell three vehicles derived from surplus ICBM Peacekeeper motors—the number required for one launch, or, a “motor set”—at motors such as those used on the Peacekeeper and Minuteman missiles. a breakeven price of about $8.36 million and two Minuteman II motors for about The Commercial Space Act of 1998 $3.96 million, as shown below. Other methods for determining motor prices, such prohibits the use of these motors for as fair market value as described in the Federal Accounting Standards Advisory commercial launches and limits their Board Handbook, resulted in stakeholder estimates ranging from $1.3 million per use in government launches in part to motor set to $11.2 million for a first stage Peacekeeper motor. -
The Right Rocket for the Job: Small Launch Providers Target Small Satellites
The Right Rocket for the Job: Small Launch Providers Target Small Satellites An STS Research Paper presented to the faculty of the School of Engineering and Applied Science University of Virginia by Gabriel Norris May 11, 2020 On my honor as a University student, I have neither given nor received unauthorized aid on this assignment as defined by the Honor Guidelines for Thesis-Related Assignments. Signed: _________________________________________________ Approved: _______________________________________ Date ________________________ Peter Norton, Department of Engineering and Society 2 The University of Virginia Department of Mechanical and Aerospace Engineering has its first satellite, Libertas, now in orbit and plans to launch two more within the next three years. This sudden activity is representative of the vastly increased smallsat1 launch cadence by a variety of groups around the world. The trend is facilitated by the reduced cost and relative ease of assembly conferred by CubeSats, which collectively make up 70 percent of satellites launched today (Halt & Wieger, 2019). Startups, underdeveloped countries, and universities that, just ten years ago, would have been incapable of any kind of space mission are now launching several. From 2012 to 2019, 663 CubeSats were manufactured by private companies, nearly 300 by governments or militaries, and 371 by academic institutions. Yearly satellite launches have increased six-fold in this time (Halt & Wieger, 2019; fig. 1). This marked increase in customers underscores a sociotechnical problem in the rocketry industry: most rockets are fairly large and cater primarily to large satellites, leaving behind a large number of customers in the smallsat domain. Satellites broadly fall within four categories of use: remote sensing, communication, technology demonstration, and scientific investigation. -
LSP Brochure
National Aeronautics and Space Administration There’s a reason challenging endeavours are called ‘rocket science’... Table of Contents Introduction NASA’s Launch Services Program (LSP) assists customers who Table of Contents ................................................................................1 need specialized, high-technology support world-wide, and Introduction & Objective .......................................................................2 enables some of NASA’s greatest scientific missions and technical achievements. Let’s explore LSP’s ‘earth’s bridge to space.’ Rocket Science 411~Take 1 ............................................................ 3-4 Strategy ........................................................................................... 5-6 Services .......................................................................................... 7-8 Rocket Science 411~Take 2 ...............................................................9 Objective Launch Fleet ......................................................................................10 This portfolio is intended to educate and connect you to some of Launch Vehicle Capabilities, Primary Missions ............................. 11-14 NASA’s most significant unmanned missions, and to highlight the Small Satellite Missions ............................................................... 15-18 contributions made by LSP. Through enriching your understanding of LSP’s benefit to NASA, you may also realize its benefit to you LSP Launch Sites ........................................................................