The Regulatory Role of the Federal Aviation Administration
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Small Launch Vehicles a 2015 State of the Industry Survey Carlos Niederstrasser
Small Launch Vehicles A 2015 State of the Industry Survey Carlos Niederstrasser An update to this survey will be presented at the 2016 Internaonal Astronau9cal Congress 1 Agenda Overview of Small Launch Vehicles Launch Method/Locations Launch Performance Projected Launch Costs Individual Rocket Details Copyright © 2015 by Orbital ATK, Inc. 2 Listing Criteria Have a maximum capability to LEO of 1000 kg (definition of LEO left to the LV provider). The effort must be for the development of an entire launch vehicle system (with the exception of carrier aircraft for air launch vehicles). Mentioned through a web site update, social media, traditional media, conference paper, press release, etc. sometime after 2010. Have a stated goal of completing a fully operational space launch (orbital) vehicle. Funded concept or feasibility studies by government agencies, patents for new launch methods, etc., do not qualify. Expect to be widely available commercially or to the U.S. Government No specific indication that the effort has been cancelled, closed, or otherwise disbanded. Correc&ons, addi&ons, and comments are welcomed and encouraged! Copyright © 2015 by Orbital ATK, Inc. 3 We did not … … Talk to the individual companies … Rely on any proprietary/confidential information … Verify accuracy of data found in public resources Ø Primarily relied on companies’ web sites Funding sources, when listed, are not implied to be the vehicles sole or even majority funding source. We do not make any value judgements on technical or financial credibility -
Enhancing Suborbital Science Through Better Understanding of Wind Effects
Space Traffic Management Conference 2019 Progress through Collaboration Feb 26th, 11:00 AM Enhancing suborbital science through better understanding of wind effects Pedro Llanos Embry-Riddle Aeronautical University - Daytona Beach, [email protected] Diane Howard University of Texas at Austin Follow this and additional works at: https://commons.erau.edu/stm Part of the Aviation and Space Education Commons, Educational Technology Commons, Operational Research Commons, and the Space Vehicles Commons Llanos, Pedro and Howard, Diane, "Enhancing suborbital science through better understanding of wind effects" (2019). Space Traffic Management Conference. 25. https://commons.erau.edu/stm/2019/presentations/25 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in Space Traffic Management Conference by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Enhancing suborbital science through better understanding of wind effects Pedro Llanos,1 and Diane Howard2 Embry-Riddle Aeronautical University, Daytona Beach, Florida, 32114, USA This paper highlights the importance of understanding some key factors, such as winds effects, trajectory and vehicle parameters variations in order to streamline the space vehicle operations and enhance science in the upper mesosphere at about 85 km. Understanding these effects is crucial to refine current space operations and establish more robust procedures. These procedures will involve training new space operators to conduct and coordinate space operations in class E above FL600 airspace within the Air Traffic Organization (ATO). Space vehicles such as Space Ship Two can spend up to 6 minutes in class E airspace above FL600 after launch. -
Dominant Suborbital Space Tourism Architectures
Dominant Suborbital Space Tourism Architectures The MIT Faculty has made this article openly available. Please share how this access benefits you. Your story matters. Citation Guerster, Markus and Edward F. Crawley. "Dominant Suborbital Space Tourism Architectures." Journal of Spacecraft and Rockets 56, 5 (September 2019): dx.doi.org/10.2514/1.a34385 As Published http://dx.doi.org/10.2514/1.a34385 Publisher American Institute of Aeronautics and Astronautics (AIAA) Version Author's final manuscript Citable link https://hdl.handle.net/1721.1/126666 Terms of Use Creative Commons Attribution-Noncommercial-Share Alike Detailed Terms http://creativecommons.org/licenses/by-nc-sa/4.0/ JOURNAL OF SPACECRAFT AND ROCKETS Dominant Suborbital Space Tourism Architectures Markus Guerster∗ and Edward F. Crawley† Massachusetts Institute of Technology, Cambridge, Massachusetts 02139 DOI: 10.2514/1.A34385 In the early stages of maturity of a system built for a specific function, it is common for the solutions to lie in a broad architectural space, in which numerous concepts are being developed, built, and tested. As the product matures, certain concepts become more dominant. This pattern can currently be observed in the suborbital tourism industry, in which the obvious question is what system architecture will provide the best combination of cost and safety and in the long run become the dominant architecture. This paper addresses this question by defining a broad architectural space of thousands of possibilities and exploring it comprehensively. We identified 33 feasible architectures, 26 of which had not been proposed earlier. A genetic algorithm optimizes each architecture with respect to the launch mass (a proxy for cost) and operational safety. -
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 . -
Greason, CEO XCOR Aerospace February 18, 2010
Providing Low Cost Access to Space REM Capabilities of The Lynx Suborbital Vehicle Presentation to Next-Generation Suborbital Researchers Conference February 18, 2010 1 © 2010 XCOR Aerospace, Inc. All RightsProprietary Reserved. & Confidential Proprietary to XCORto XCOR Aerospace Aerospace, (See Inc. Last No Slide) Third Party Disclosure Allowable. 1 Lynx Overview … • Suborbital space vehicle • Horizontal takeoff/landing • Two seats – pilot plus one • Small vehicle – Wingspan ~24 feet – Length ~30 feet • Multi-mission capable – In-cockpit experiments – External mount experiments – Test pilot/astronaut training – Upper atmospheric sampling – Microsatellite launch © 2010– XCORSpace Aerospace, tourism Inc. All Rights Reserved. Proprietary to XCOR Aerospace, Inc. No Third Party Disclosure Allowable. 2 Lynx Heritage … • EZ Rocket taught us … – Development of safe EZ-Rocket (2001-2005) reusable propulsion – Integration into airframe – Low cost & safe operational procedures – Regulatory framework • X-Racer taught us … – Pump fed fuel enabled high performance for future ops – Improved low cost ops and safety regime processes – Improved airframe skill sets and avionics integration X-Racer (2006-2008) © 2010 XCOR Aerospace, Inc. All Rights Reserved. Proprietary to XCOR Aerospace, Inc. No Third Party Disclosure Allowable. 3 Lynx: Mark I • Horizontal takeoff/landing • 61 km (200,000 ft) peak altitude • Mach 2.4 top speed • First flight in 2011 © 2010 XCOR Aerospace, Inc. All Rights Reserved. Proprietary to XCOR Aerospace, Inc. No Third Party Disclosure Allowable. 4 LYNX Mark II • Follows Mark I by 9-18 months • ~5000 flight life • Mach 3.5, over 100 km • Can launch two stage to LEO ~10kg © 2010 XCOR Aerospace, Inc. All Rights Reserved. Proprietary to XCOR Aerospace, Inc. No Third Party Disclosure Allowable. -
XCOR Aerospace, Inc
XCOR Aerospace, Inc. …Providing Low Cost, Safe & Responsive Access to Space © 2013© 2013 XCOR XCOR Aerospace, Aerospace, Inc. Inc. All RightsAll Rights Reserved. Reserved. 1 Watch the video: <http://youtu.be/PjzGaSQX0iU> XCOR Aerospace, Inc. …Providing Low Cost, Safe & Responsive Access to Space © 2013© 2013 XCOR XCOR Aerospace, Aerospace, Inc. Inc. All RightsAll Rights Reserved. Reserved. 1 XCOR History Founded in 1999 Located at Mojave Air & Spaceport, CA –Moving to Midland, TX Fourteen different rocket engine designs –Approximately 5,000 firings –Innovative piston pump © 2013 XCOR Aerospace, Inc. All Rights Reserved. 2 History of Rocketry © 2013 XCOR Aerospace, Inc. All Rights Reserved. 5 Wernher von Braun © 2013 XCOR Aerospace, Inc. All Rights Reserved. 6 History of Rocketry © 2013 XCOR Aerospace, Inc. All Rights Reserved. 7 Turbopumps High efficiency compression of liquid fuels and oxidizer But... Expensive to design Expensive to build Very expensive to maintain © 2013 XCOR Aerospace, Inc. All Rights Reserved. 8 Three Phase Pumping 1 Rate of Flow Time 2 Single piston cylinder leads to sinusoidal variation in flow. 1 Rate of Flow Time © 2013 XCOR Aerospace, Inc. All Rights Reserved. 9 Three Phase Pumping 1 Rate of Flow Time 120° offset 2 Adding a second piston cylinder begins to smooth out net fluid flow. Average flow = 1 1 unit/sec Rate of Flow Time © 2013 XCOR Aerospace, Inc. All Rights Reserved. 10 Three Phase Pumping 1 Rate of Flow Time 120° offset 2 Adding a third piston cylinder smooths out net fluid flow completely. Average flow = 1.5 unit/sec 1 Rate of Flow Time © 2013 XCOR Aerospace, Inc. -
Architectural Options and Optimization of Suborbital Space Tourism Vehicles Markus Guerster Edward F
Architectural Options and Optimization of Suborbital Space Tourism Vehicles Markus Guerster Edward F. Crawley System Architecture Lab, MIT System Architecture Lab, MIT 77 Massachusetts Avenue. 77 Massachusetts Avenue. Cambridge, MA 02139 Cambridge, MA 02139 857-999-6103 617-230-6604 [email protected] [email protected] Abstract— Since the creation of the Ansari X-Prize, a significant The birth of the suborbital space tourism dates to May 1996, technical and commercial interest has developed in suborbital where the Ansari XPrize was launched by the Ansari family. space tourism. An obvious question arises: what system This competition challenged teams all around the world to architecture will provide the best combination of cost and safety build a reusable, private-funded and manned spaceship. The for the performance defined by the prize? The objective of this first team carrying three people to 100 km above the Earth’s paper is to address this question, by defining the design space and searching comprehensively through it with respect to surface twice within two weeks received the $10 million launch mass (a proxy for cost) and safety. We have identified 33 price. 26 teams from 7 nations proposed their concept. architectures and visualized them in a single table. Of these, 26 Finally, the Mojave Aerospace Ventures team, which was led have not earlier been proposed. A genetic algorithm optimized by Burt Rutan and his company Scaled Composites and each of these 33 architectures for launch mass and safety. The financed from Paul Allen, won the competition on October 4, launch mass was calculated by a design framework consisting of 2004. -
Lot 1 (Contract No. 30-CE-036363/00-01)
Ref. Ares(2013)617034 - 09/04/2013 Ref. Request for Services under Framework Service Contract No. ENTR/2009/050— Lot 1 (Contract No. 30-CE-036363/00-01) EVALUATION OF THE EUROPEAN MARKET POTENTIAL FOR COMMERCIAL SPACEFLIGHT Prepared fon THE EUROPEAN COMMISSION ENTERPRISE AND INDUSTRY DIRECTORATE-GENERAL IS01 February, 2013* FINAL REPORT By Booz & Company « space-tec With contributions of ^ PARTNERS This report is protected by copyright. Reproduction is authorised provided the source is acknowledged, save where otherwise stated. Where prior permission must be obtained for the reproduction or use of textual and multimedia information (sound, images, software, etc.), such permission shall cancel the above mentioned general permission and shall clearly indicate any restrictions on use. * resubmitted on 2 8 (Ш 2013 Ref. Request for Services - Framework Contract No. ENTR/2009/050 Lot 1 - Conunercial Space Table of Contents 1 EXECUTIVE SUMMARY 3 L.L INDUSTRY AND MARKET ASSESSMENT 3 \2 GAP ANALYSIS AND INSTMMONAL ACTIONS 5 2 INTRGDUCTIGN 7 2.1 OBJECTIVE OF THE STUDY 7 22 STUDY SUBJECT DEFiNmoN AND яюкт BACKGROUND 7 23 STUDY APPROACH 9 2.3.1 Stakeholder consultation 10 3 HIGH-LEVEL INDUSTRY AND MARKET CHARACTERIZATION 12 3.1 INDUSTRY STRUCTURE AND EXTERNAL ENVIRONMENT 12 3.1.1 Vehicle manufacturers 13 3.1.2 Spaceports 15 3.1.3 Service Operators 18 3.1.4 Insurance companies 19 3.1.5 Competitive Dynamics 20 3.1.6 External Factors 21 32 EUROPEAN SCENARIO 23 3.2.1 Vehicle developers 23 3.2.2 Air/Space Ports 24 3.2.3 Operators 25 3.2.4 External factors in Europe 25 3.2.5 U.S. -
Cecil Spaceport Master Plan 2012
March 2012 Jacksonville Aviation Authority Cecil Spaceport Master Plan Table of Contents CHAPTER 1 Executive Summary ................................................................................................. 1-1 1.1 Project Background ........................................................................................................ 1-1 1.2 History of Spaceport Activities ........................................................................................ 1-3 1.3 Purpose of the Master Plan ............................................................................................ 1-3 1.4 Strategic Vision .............................................................................................................. 1-4 1.5 Market Analysis .............................................................................................................. 1-4 1.6 Competitor Analysis ....................................................................................................... 1-6 1.7 Operating and Development Plan................................................................................... 1-8 1.8 Implementation Plan .................................................................................................... 1-10 1.8.1 Phasing Plan ......................................................................................................... 1-10 1.8.2 Funding Alternatives ............................................................................................. 1-11 CHAPTER 2 Introduction ............................................................................................................. -
The Ultimate High Ground—U.S. Intersector Cooperation in Outer Space C
Journal of Air Law and Commerce Volume 81 | Issue 4 Article 2 2016 The Ultimate High Ground—U.S. Intersector Cooperation in Outer Space C. Brandon Halstead Follow this and additional works at: https://scholar.smu.edu/jalc Recommended Citation C. Brandon Halstead, The Ultimate High Ground—U.S. Intersector Cooperation in Outer Space, 81 J. Air L. & Com. 595 (2016) https://scholar.smu.edu/jalc/vol81/iss4/2 This Article is brought to you for free and open access by the Law Journals at SMU Scholar. It has been accepted for inclusion in Journal of Air Law and Commerce by an authorized administrator of SMU Scholar. For more information, please visit http://digitalrepository.smu.edu. THE ULTIMATE HIGH GROUND—U.S. INTERSECTOR COOPERATION IN OUTER SPACE C. BRANDON HALSTEAD* I. INTRODUCTION PACE, THE FINAL FRONTIER.” Those words opened “Seach episode of the original 1960s’ television series Star Trek.1 In a seemingly relentless effort to dominate this final fron- tier, the second half of the 20th century was marked by a space race of United States and Soviet Union competition to attain superior space capabilities. Those few States2 able to achieve or- bit comprised an exclusive club, with the technology and fi- nances necessary to successfully launch, orbit, and recover space vehicles embodying State prestige and power. Yet as the campy science fiction films and television series of the 1950s and 1960s gave way to blockbuster space movies and television dramas from the 1970s onward, so too has science fiction and space ca- pabilities transformed from the silver screen to reality. -
GAO-15-706, Federal Aviation Administration: Commercial Space
United States Government Accountability Office Report to the Chairman, Committee on Science, Space and Technology, House of Representatives August 2015 FEDERAL AVIATION ADMINISTRATION Commercial Space Launch Industry Developments Present Multiple Challenges GAO-15-706 August 2015 FEDERAL AVIATION ADMINISTRATION Commercial Space Launch Industry Developments Present Multiple Challenges Highlights of GAO-15-706, a report to the Chairman, Committee on Science, Space and Technology, House of Representatives Why GAO Did This Study What GAO Found The U.S. commercial space launch During the last decade, U.S. companies conducted fewer orbital launches in total industry has changed considerably than companies in Russia or Europe, which are among their main foreign since the enactment of the Commercial competitors. However, the U.S. commercial space launch industry has expanded Space Launch Amendments Act of recently. In 2014, U.S. companies conducted 11 orbital launches, compared with 2004. FAA is required to license or none in 2011. In addition, in 2014, U.S. companies conducted more orbital permit commercial space launches, but launches than companies in Russia, which conducted four, or Europe, which to allow the space tourism industry to conducted six. develop, the act prohibited FAA from regulating crew and spaceflight The Federal Aviation Administration (FAA)—which is responsible for protecting participant safety before 2012—a the public with respect to commercial space launches, including licensing and moratorium that was later extended but permitting launches—faces multiple challenges in addressing industry will now expire on September 30, developments. If Congress does not extend the regulatory moratorium beyond 2015. Since October 2014, there have September 2015, FAA will need to determine whether and when to regulate the been three mishaps involving FAA safety of crew and spaceflight participants.