Virgin Galactic, LLC (“Virgin Galactic”) Hereby Requests Experimental
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Validation of Wind Tunnel Test and Cfd Techniques for Retro-Propulsion (Retpro): Overview on a Project Within the Future Launchers Preparatory Programme (Flpp)
VALIDATION OF WIND TUNNEL TEST AND CFD TECHNIQUES FOR RETRO-PROPULSION (RETPRO): OVERVIEW ON A PROJECT WITHIN THE FUTURE LAUNCHERS PREPARATORY PROGRAMME (FLPP) D. Kirchheck, A. Marwege, J. Klevanski, J. Riehmer, A. Gulhan¨ German Aerospace Center (DLR) Supersonic and Hypersonic Technologies Department Cologne, Germany S. Karl O. Gloth German Aerospace Center (DLR) enGits GmbH Spacecraft Department Todtnau, Germany Gottingen,¨ Germany ABSTRACT and landing (VTVL) spacecraft, assisted by retro-propulsion. Up to now, in Europe, knowledge and expertise in that field, The RETPRO project is a 2-years activity, led by the Ger- though constantly growing, is still limited. Systematic stud- man Aerospace Center (DLR) in the frame of ESA’s Future ies were conducted to compare concepts for possible future Launchers Preparatory Program (FLPP), to close the gap of European launchers [2, 3], and activities on detailed inves- knowledge on aerodynamics and aero-thermodynamics of tigations of system components of VTVL re-usable launch retro-propulsion assisted landings for future concepts in Eu- vehicles (RLV) recently started in the RETALT project [4, 5]. rope. The paper gives an overview on the goals, strategy, and Nevertheless, validated knowledge on the aerodynamic current status of the project, aiming for the validation of inno- and aerothermal characteristics of such vehicles is still lim- vative WTT and CFD tools for retro-propulsion applications. ited to a small amount of experimental and numerical inves- Index Terms— RETPRO, retro-propulsion, launcher tigations mostly on lower altitude VTVL trajectories, e. g. aero-thermodynamics, wind tunnel testing, CFD validation within the CALLISTO project [6, 7, 8]. Other studies were conducted to analyze the aerothermodynamics of a simplified generic Falcon 9 geometry during its re-entry and landing 1. -
Virgin Galactic Announces First Fully Crewed Spaceflight
Virgin Galactic Announces First Fully Crewed Spaceflight Test Flight Window for Unity 22 Mission Opens July 11 Four Mission Specialists to Evaluate Virgin Galactic Astronaut Experience Virgin Galactic Founder Sir Richard Branson Among Mission Specialists First Global Livestream of Virgin Galactic Spaceflight LAS CRUCES, N.M. July 1, 2021 - Virgin Galactic Holdings, Inc. (NYSE: SPCE) (the “Company” or “Virgin Galactic”), a vertically integrated aerospace and space travel company, today announced that the fligHt window for the next rocket-powered test flight of its SpaceShipTwo Unity opens July 11, pending weather and technical checks. The “Unity 22” mission will be the twenty-second flight test for VSS Unity and the Company’s fourth crewed spaceflight. It will also be the first to carry a full crew of two pilots and four mission specialists in tHe cabin, including the Company’s founder, Sir Richard Branson, who will be testing the private astronaut experience. Building on tHe success of the Company’s most recent spaceflight in May, Unity 22 will focus on cabin and customer experience objectives, including: • Evaluating the commercial customer cabin with a full crew, including the cabin environment, seat comfort, the weightless experience, and the views of Earth that the spaceship delivers — all to ensure every moment of the astronaut’s journey maximizes the wonder and awe created by space travel • Demonstrating tHe conditions for conducting human-tended research experiments • Confirming the training program at Spaceport America supports the spaceflight experience For the first time, Virgin Galactic will share a global livestream of the spaceflight. Audiences around the world are invited to participate virtually in tHe Unity 22 test flight and see first-hand the extraordinary experience Virgin Galactic is creating for future astronauts. -
Reusable Launch Vehicle Technology Program{
Acta Astronautica Vol. 41, No. 11, pp. 777±790, 1997 # 1998 Published by Elsevier Science Ltd. All rights reserved Printed in Great Britain PII: S0094-5765(97)00197-5 0094-5765/98 $19.00 + 0.00 REUSABLE LAUNCH VEHICLE TECHNOLOGY PROGRAM{ DELMA C. FREEMAN{ JR. and THEODORE A. TALAY} NASA Langley Research Center, Hampton, Virginia 23681-0001, USA R. EUGENE AUSTIN} NASA Marshall Space Flight Center, Marshall Space Flight Center, Alabama 35812-1000, USA (Received 25 April 1997) AbstractÐIndustry/NASA reusable launch vehicle (RLV) technology program eorts are underway to design, test, and develop technologies and concepts for viable commercial launch systems that also satisfy national needs at acceptable recurring costs. Signi®cant progress has been made in understanding the technical challenges of fully reusable launch systems and the accompanying management and oper- ational approaches for achieving a low-cost program. This paper reviews the current status of the RLV technology program including the DC-XA, X-33 and X-34 ¯ight systems and associated technology programs. It addresses the speci®c technologies being tested that address the technical and operability challenges of reusable launch systems including reusable cryogenic propellant tanks, composite structures, thermal protection systems, improved propul- sion, and subsystem operability enhancements. The recently concluded DC-XA test program demon- strated some of these technologies in ground and ¯ight tests. Contracts were awarded recently for both the X-33 and X-34 ¯ight demonstrator systems. The Orbital Sciences Corporation X-34 ¯ight test ve- hicle will demonstrate an air-launched reusable vehicle capable of ¯ight to speeds of Mach 8. -
A Review of Current Research in Subscale Flight Testing and Analysis of Its Main Practical Challenges
aerospace Article A Review of Current Research in Subscale Flight Testing and Analysis of Its Main Practical Challenges Alejandro Sobron * , David Lundström and Petter Krus Department of Management and Engineering, Division of Fluid and Mechatronic Systems, Linköping University, SE-58183 Linköping, Sweden; [email protected] (D.L.); [email protected] (P.K.) * Correspondence: [email protected]; Tel.: +46-1328-1893 Abstract: Testing of untethered subscale models, often referred to as subscale flight testing, has traditionally had a relatively minor, yet relevant use in aeronautical research and development. As recent advances in electronics, rapid prototyping and unmanned-vehicle technologies expand its capabilities and lower its cost, this experimental method is seeing growing interest across academia and the industry. However, subscale models cannot meet all similarity conditions required for simulating full-scale flight. This leads to a variety of approaches to scaling and to other alternative applications. Through a literature review and analysis of different scaling strategies, this study presents an overall picture of how subscale flight testing has been used in recent years and synthesises its main issues and practical limitations. Results show that, while the estimation of full-scale characteristics is still an interesting application within certain flight conditions, subscale models are progressively taking a broader role as low-cost technology-testing platforms with relaxed similarity constraints. Different approaches to tackle the identified practical challenges, implemented both by the authors and by other organisations, are discussed and evaluated through flight experiments. Citation: Sobron, A.; Lundström, D.; Keywords: subscale flight testing; similarity; scale model; remotely piloted aircraft; demonstration; Krus, P. -
+ Part 10: Test and Evaluation
10. Test and Evaluation 10.1 Approach Architecture Design, Development, Test, and Evaluation (DDT&E) schedule, costs, and risk are highly dependent on the integrated test and evaluation approach for each of the major elements. As a part of the Exploration Systems Architecture Study (ESAS), a top-level test and evaluation plan, including individual flight test objectives, was developed and is summarized in this section. The test and evaluation plan described here is derived from the Apollo Flight Test Program of the 1960s. A more detailed test and evaluation plan will be based on detailed verification requirements and objectives documented in specifications and verification plans. In order to support schedule, cost, and risk assessments for the reference ESAS architecture, an integrated test and evaluation plan was developed to identify the number and type of major test articles (flight and ground) and the timing and objectives of each major flight test, including facilities and equipment required to support those tests. This initial plan is based on the Apollo Program and the ESAS Ground Rules and Assumptions (GR&As)—including the human- rating requirements from NASA Procedural Requirements (NPR) 8705.2A, Human-Rating Requirements for Space Systems. 10. Test and Evaluation 645 10.2 Ground Rules and Assumptions ESAS GR&As establish the initial set of key constraints to testing. Although all ESAS GR&As are considered, the specific ones listed below are particularly significant, as they deal with schedule and testing/qualification assumptions. • The crew launch system shall facilitate crew survival using abort and escape. There will be three all-up tests of the Launch Abort System (LAS). -
Virgin Galactic License Orders
License Order No. LRLO 16-092B (Rev 3) OFFICE OF COMMERCIAL SPACE TRANSPORTATION LICENSE ORDER REGARDING FLIGHT AUTHORIZED BY LICENSE NO. LRLO 16-092 ISSUED TO VIRGIN GALACTIC, LLC 1. Authority: This Order is issued to Virgin Galactic (referred to as VG), under 51 U.S.C. subtitle V, chapter 509, and 14 C.F.R. Ch. III. 2. Purpose: This Order modifies License No. LRLO 16-092 issued concurrently by the Federal Aviation Administration’s Office of Commercial Space Transportation, authorizing VG to conduct suborbital RLV missions to launch the SpaceShipTwo (SS2) reusable launch vehicle utilizing the WhiteKnightTwo (WK2) carrier aircraft; and prescribes as conditions to License No. LRLO 16-092 certain requirements applicable to the authorization to conduct flights. 3. Authorization: VG is authorized to conduct flights: (a) Using SS2, in combination with the WK2 carrier aircraft that must hold a valid FAA experimental airworthiness certificate and must operate in accordance with the operating limitations of that certificate and the applicable sections of 14 C.F.R. part 91; (b) From Mojave Air and Space Port, California, and Spaceport America, New Mexico; (c) Transporting non-deployed scientific, experimental, or inert payloads; (d) According to the launch vehicle, launch vehicle systems, flight profiles, and safety management program represented in the VG application as of the date of this order, and any amendments to the license application approved by the FAA, in writing. Order No. LRLO 16-092B (Rev 3) 4. Responsibility and Authority of SS2 Pilot In Command: (a) Prior to flight, VG must designate the pilot in command of the SS2 vehicle who is directly responsible for, and is the final authority as to, the operation of that vehicle. -
Flight Engineer Knowledge Test Guide
AC 63-1 FLIGHT ENGINEER KNOWLEDGE TEST GUIDE U.S. Department of Transportation Federal Aviation Administration 1 FLIGHT ENGINEER KNOWLEDGE TEST GUIDE 1995 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION Flight Standards Service 2 PREFACE The Flight Standards Service of the Federal Aviation Administration (FAA) has developed this guide to help applicants meet the knowledge requirements for the computer administered tests for flight engineer turbojet, turboprop, and reciprocating class certification. This guide contains information about the knowledge test eligibility requirements, test descriptions, testing and retesting procedures, and sample test questions with answers. As a convenience to the applicant, the eligibility requirements for the oral and flight tests are included. Appendix 1 provides a list of reference materials and subject matter knowledge codes, and computer testing designees. Changes to the subject matter knowledge code list will be published as a separate advisory circular. The sample questions and answers in this guide are predicated on Federal Aviation Regulations (FAR's) and references that were current at the time of publication. Questions and answers in the computer administered knowledge tests are updated when changes are made to these reference materials. The flight engineer test question bank and subject matter knowledge code list for all airmen certificates and ratings, with changes, may be obtained by computer access from FedWorld at (703) 321-3339. This bulletin board service is provided by the U.S. Department of Commerce, 24 hours a day, 7 days per week. For technical assistance regarding computer requirements for this service, contact the FedWorld help desk at (703) 487-4608 from 7:30 a.m. -
Virgin Galactic Holdings, Inc. (SPCE) Putting the Zero in Zero-G
June 2021 Virgin Galactic Holdings, Inc. (SPCE) Putting the Zero in Zero-G We are short shares of Virgin Galactic Holdings, Inc., often described as the only publicly traded space-tourism company. After going public in October 2019 by way of a merger with a “blank check” company, Virgin Galactic has seen its share price and trading volume soar. It’s become a retail darling, with day traders captivated by images of billionaires donning space suits, blasting off from launchpads, and looking down on the blue marble of Earth. But Virgin Galactic’s $250,000+ commercial “spaceflights” – if they ever actually happen, after some 17 years of delays and disasters – will offer only the palest imitations of these experiences. In lieu of pressurized space suits with helmets – unnecessary since so little time will be spent in the upper atmosphere – the company commissioned Under Armour to provide “high-tech pajamas.” In lieu of vertical takeoff, Virgin’s “spaceship” must cling to the underside of a specialized airplane for the first 45,000 feet up, because its rocket motor is too weak to push through the lower atmosphere on its own. In lieu of the blue-marble vista and life in zero-g, Virgin’s so-called astronauts will at best be able to catch a glimpse of the curvature of Earth and a few minutes of weightlessness before plunging back to ground. This isn’t “tourism,” let alone Virgin’s more grandiose term, “exploration”; it’s closer to a souped- up roller coaster, like the “Drop of Doom” ride at Six Flags. -
Rewarding Energy Innovation to Achieve Climate Stabilization
Case Western Reserve University School of Law Scholarly Commons Faculty Publications 2011 Eyes on a Climate Prize: Rewarding Energy Innovation to Achieve Climate Stabilization Jonathan H. Adler Case Western University School of Law, [email protected] Follow this and additional works at: https://scholarlycommons.law.case.edu/faculty_publications Part of the Environmental Law Commons, and the Science and Technology Law Commons Repository Citation Adler, Jonathan H., "Eyes on a Climate Prize: Rewarding Energy Innovation to Achieve Climate Stabilization" (2011). Faculty Publications. 656. https://scholarlycommons.law.case.edu/faculty_publications/656 This Article is brought to you for free and open access by Case Western Reserve University School of Law Scholarly Commons. It has been accepted for inclusion in Faculty Publications by an authorized administrator of Case Western Reserve University School of Law Scholarly Commons. \\jciprod01\productn\H\HLE\35-1\HLE101.txt unknown Seq: 1 14-MAR-11 12:33 EYES ON A CLIMATE PRIZE:REWARDING ENERGY INNOVATION TO ACHIEVE CLIMATE STABILIZATION Jonathan H. Adler* Stabilizing atmospheric concentrations of greenhouse gases at double their pre-in- dustrial levels (or lower) will require emission reductions far in excess of what can be achieved at a politically acceptable cost with current or projected levels of tech- nology. Substantial technological innovation is required if the nations of the world are to come anywhere close to proposed emission reduction targets. Neither tradi- tional federal support for research and development of new technologies nor tradi- tional command-and-control regulations are likely to spur sufficient innovation. Technology inducement prizes, on the other hand, have the potential to significantly accelerate the rate of technological innovation in the energy sector. -
Window Opens for Virgin Galactic Test Flight from Spaceport 11 December 2020, by Susan Montoya Bryan
Window opens for Virgin Galactic test flight from spaceport 11 December 2020, by Susan Montoya Bryan CEO Michael Colglazier said the company has minimized the number of people onsite at its headquarters at Spaceport America in accordance with state mandates and that only spaceport staff critical to the mission will be present. Officials with Virgin Galactic and the state-financed spaceport said the test flight will mark another key milestone in the march toward commercial flights. The impending flight will be the third space flight for Virgin Galactic and the first from New Mexico. "We are thrilled about hosting the first human This photo provided by Virgin Galactic shows spaceflight from New Mexico. This is an incredible SpaceShipTwo Unity being released from the carrier moment for the entire state," Scott McLaughlin, the mothership, VMS Eve for second successful glide flight spaceport's interim executive director, said in a in New Mexico on Thursday, June 25, 2020. Virgin statement. Galactic is celebrating the second successful glide flight of its spaceship over Spaceport America in southern New Mexico. (Virgin Galactic via AP) The window opened Friday for Virgin Galactic's first rocket-powered test flight from Spaceport America in southern New Mexico as the company prepares for commercial flights next year, but the exact timing of the launch will depend on the weather. Virgin Galactic posted on social media that the flight crew is ready but do not plan to fly before This photo provided by Virgin Galactic shows Saturday. SpaceShipTwo Unity on it's second successful glide flight over Spaceport America in New Mexico on Thursday, "We have range clearance through the weekend June 25, 2020. -
Virgin Galactic Announces Third Quarter 2020 Financial Results First
Virgin Galactic Announces Third Quarter 2020 Financial Results First Spaceflight from Spaceport America Expected to Occur Between November 19-23 Rollout of Second Spaceship Scheduled to Take Place in the First Quarter of 2021 Reopening Ticket Sales in 2021 Following Sir Richard Branson’s Spaceflight LAS CRUCES, N.M. – November 5, 2020 – Virgin Galactic Holdings, Inc. (NYSE: SPCE) (“Virgin Galactic” or the “Company”), a vertically integrated aerospace and space travel company, today announced its financial results for the third quarter ended September 30, 2020. “During the quarter we made good progress completing the final steps to prepare for VSS Unity’s first rocket powered test flight from Spaceport America this November. This will be the first-ever human spaceflight conducted from New Mexico,” said Michael Colglazier, Chief Executive Officer of Virgin Galactic. “We also made meaningful progress on our second SpaceShipTwo vehicle, which we plan to unveil in the first quarter of 2021. During my first three months at the Company, I have been continually impressed with the team and the tremendous work that has gone into making the dream of commercial spaceflight a reality. As we continue to prepare for commercial launch, we will reopen ticket sales following Richard Branson’s flight in 2021. I am excited and confident in our ability to execute our vision and provide transformative experiences to people around the world.” Third Quarter 2020 Business Highlights: • Completed the application of the thermal protection system on the Wing and Fuselage, progressed on systems installation, and successfully completed the initial Pilot Simulator evaluations of the second SpaceShipTwo vehicle, in preparation for its expected rollout in the first quarter of 2021. -
UAS FLIGHT TEST for SAFETY and for EFFICIENCY Seamus M
UAS FLIGHT TEST FOR SAFETY AND FOR EFFICIENCY Seamus M. McGovern, U.S. DOT National Transportation Systems Center, Cambridge, Massachusetts Abstract (e.g., SAE International technical standards and recommended practices) but also takes advantage of Manned aircraft that operate in the National competitive racing in order to evaluate new Airspace System (NAS) typically undergo technologies and materials (as it turns out, this may certification flight test to ensure they meet a have applicability to UASs as well with the advent of prescribed level of safety—dependent on their several organizations and sanctioning bodies category—before they are able to enter service [for including the European Rotor Sports Association and example, Federal Aviation Administration (FAA) the Drone Racing League). Other aviation-related advisory circular (AC) 25-7C is the flight-test guide tests and test formats not discussed here include the for certification of transport-category airplanes]. typically Department of Defense-focused With the integration of unmanned aircraft systems developmental test and evaluation; operational test (UAS) into the NAS, in the future some type of and evaluation; and research, development, test, and certification flight test may ultimately be required, evaluation structures. however, even lacking such a requirement UAS manufacturers can find value in flight testing UASs In terms of flight test, the military services have using familiar experimental and certification flight- their own criteria for evaluating their various aircraft. test procedures, the results of which can enhance the These requirements are often bound by contractual safety of the design, the safety of the operation, agreements between the service and the vendor, and/or the efficiency of the operation.