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Nasa X-15 Program
5 24,132 6 9 NASA X-15 PROGRAM By: T.D. Barnes - NASA Contractor - 1960s NASA contractors for the X-15 program were Bendix Field Engineering followed by Unitec, Inc. The NASA High Range Tracking stations were located at Ely and Beatty Nevada with main control being at Dryden/Edwards AFB in California. Personnel at the tracking stations consisted of a Station Manager, a Technical Advisor, and field engineers for the Mod-2 Radar, Data Transmission System, Communications, Telemetry, and Plant Maintenance/Generators. NASA had a site monitor at each tracking station to monitor our contractor operations. Though supporting flights of the X-15 was their main objective, they also participated in flights of the XB-70, the three Lifting Bodies, experimental Lunar Landing vehicles, and an occasional A-12/YF-12/SR-71 Blackbird flight. On mission days a NASA van picked up each member of the crew at their residence for the 4:20 a.m. trip to the tracking station 18 miles North of Beatty on the Tonopah Highway. Upon arrival each performed preflight calibrations and setup of their various systems. The liftoff of the B-52, with the X-15 tucked beneath its wing, seldom occurred after 9:00 a.m. due to the heat effect of the Mojave Desert making it difficult for the planes to acquire altitude. At approximately 0800 hours two pilots from Dryden would proceed uprange to evaluate the condition of the dry lake beds in the event of an emergency landing of the X-15 (always buzzing our station on the way up and back). -
GAO-21-378, HYPERSONIC WEAPONS: DOD Should Clarify
United States Government Accountability Office Report to Congressional Addressees March 2021 HYPERSONIC WEAPONS DOD Should Clarify Roles and Responsibilities to Ensure Coordination across Development Efforts GAO-21-378 March 2021 HYPERSONIC WEAPONS DOD Should Clarify Roles and Responsibilities to Ensure Coordination across Development Efforts Highlights of GAO-21-378, a report to congressional addressees Why GAO Did This Study What GAO Found Hypersonic missiles, which are an GAO identified 70 efforts to develop hypersonic weapons and related important part of building hypersonic technologies that are estimated to cost almost $15 billion from fiscal years 2015 weapon systems, move at least five through 2024 (see figure). These efforts are widespread across the Department times the speed of sound, have of Defense (DOD) in collaboration with the Department of Energy (DOE) and, in unpredictable flight paths, and are the case of hypersonic technology development, the National Aeronautics and expected to be capable of evading Space Administration (NASA). DOD accounts for nearly all of this amount. today’s defensive systems. DOD has begun multiple efforts to develop Hypersonic Weapon-related and Technology Development Total Reported Funding by Type of offensive hypersonic weapons as well Effort from Fiscal Years 2015 through 2024, in Billions of Then-Year Dollars as technologies to improve its ability to track and defend against them. NASA and DOE are also conducting research into hypersonic technologies. The investments for these efforts are significant. This report identifies: (1) U.S. government efforts to develop hypersonic systems that are underway and their costs, (2) challenges these efforts face and what is being done to address them, and (3) the extent to which the U.S. -
Aerodynamic Study of a Small Hypersonic Plane
Università degli Studi di Napoli “Federico II” Dottorato di Ricerca in Ingegneria Aerospaziale, Navale e della Qualità XXVII Ciclo Aerodynamic study of a small hypersonic plane Coordinatore: Ch.mo Prof. L. De Luca Candidata: Tutors: Ing. Vera D'Oriano Ch.mo Prof. R. Savino Ing. M. Visone (BLUE Engineering) Acknowledgements First I wish to thank my academic tutor Prof. Raffaele Savino, for offering me this precious opportunity and for his enthusiastic guidance. Next, I am immensely grateful to my company tutor, Michele Visone (Mike, for friends) for his technical support, despite his busy schedule, and for his constant encouragements. I also would like to thank the HyPlane team members: Rino Russo, Prof. Battipede and Prof. Gili, Francesco and Gennaro, for the fruitful collaborations. A special thank goes to all Blue Engineering guys (especially to Myriam) for making our site a pleasant and funny place to work. Many thanks to queen Giuly and Peppe "il pazzo", my adoptive family during my stay in Turin, and also to my real family, for the unconditional love and care. My greatest gratitude goes to my unique friends - my potatoes (Alle & Esa), my mentor Valerius and Franca - and to my soul mate Naso, to whom I dedicate this work. Abstract Access to Space is still in its early stages of commercialization. Most of the attention is currently focused on sub-orbital flights, which allow Space tourists to experiment microgravity conditions for a few minutes and to see a large area of the Earth, along with its curvature, from the stratosphere. Secondary markets directly linked to the commercial sub-orbital flights may include microgravity research, remote sensing, high altitude Aerospace technological testing and astronauts training, while a longer term perspective can also foresee point-to-point hypersonic transportation. -
Contacts: Isabel Morales, Museum of Science and Industry, (773) 947-6003 Renee Mailhiot, Museum of Science and Industry, (773) 947-3133
Contacts: Isabel Morales, Museum of Science and Industry, (773) 947-6003 Renee Mailhiot, Museum of Science and Industry, (773) 947-3133 A GLOSSARY OF TERMS Aerodynamics: The study of the properties of moving air, particularly of the interaction between the air and solid bodies moving through it. Afterburner: An auxiliary burner fitted to the exhaust system of a turbojet engine to increase thrust. Airfoil: A structure with curved surfaces designed to give the most favorable ratio of lift to drag in flight, used as the basic form of the wings, fins and horizontal stabilizer of most aircraft. Armstrong limit: The altitude that produces an atmospheric pressure so low (0.0618 atmosphere or 6.3 kPa [1.9 in Hg]) that water boils at the normal temperature of the human body: 37°C (98.6°F). The saliva in your mouth would boil if you were not wearing a pressure suit at this altitude. Death would occur within minutes from exposure to the vacuum. Autothrottle: The autopilot function that increases or decreases engine power,typically on larger aircraft. Avatar: An icon or figure representing a particular person in computer games, Internet forums, etc. Aerospace: The branch of technology and industry concerned with both aviation and space flight. Carbon fiber: Thin, strong, crystalline filaments of carbon, used as a strengthening material, especially in resins and ceramics. Ceres: A dwarf planet that orbits within the asteroid belt and the largest asteroid in the solar system. Chinook: The Boeing CH-47 Chinook is an American twin-engine, tandem-rotor heavy-lift helicopter. CST-100: The crew capsule spacecraft designed by Boeing in collaboration with Bigelow Aerospace for NASA's Commercial Crew Development program. -
The National Aerospace Plane Program: a Revolutionary Concept
ROBERT R. BARTHELEMY THE NATIONAL AEROSPACE PLANE PROGRAM: A REVOLUTIONARY CONCEPT The National AeroSpace Plane program is aimed at developing and demonstrating hypersonic tech nologies with the goal of achieving orbit with a single-stage vehicle. This article describes the technologi cal, programmatic, utilitarian, and conceptual aspects of the program. INTRODUCTION The National AeroSpace Plane (NASP) is a look into The NASP demonstration aircraft, the X-30 (Fig. 1), the future. It is a vision of the ultimate airplane, one will reach speeds of Mach 25, eight times faster than has capable of flying at speeds greater than 17,000 miles per ever been achieved with airbreathing aircraft. As it flies hour, twenty-five times the speed of sound. It is the at through the atmosphere from subsonic speeds to orbital tainment of a vehicle that can routinely fly from Earth velocities (Mach 25), its structure will be subjected to to space and back, from conventional airfields, in afford average temperatures well beyond anything ever achieved able ways. It represents the achievement of major tech in aircraft. While rocket-powered space vehicles like the nological breakthroughs that will have an enormous im shuttle minimize their trajectories through the atmo pact on the future growth of this nation. It is more than sphere, the X-30 will linger in the atmosphere in order a national aircraft development program, more than the to use the air as the oxidizer for its ramjet and scramjet synergy of revolutionary technologies, more than a capa engines. The NASP aircraft must use liquid or slush bility that may change the way we move through the hydrogen as its fuel, which will present new challenges world and the aerospace around it. -
Status and Perspectives of Hypersonic Systems and Technologies with Emphasis on the Role of Sub-Orbital Flight ∗ S
Aerotecnica Missili & Spazio, The Journal of Aerospace Science, Technology and Systems Status and Perspectives of Hypersonic Systems and Technologies with Emphasis on the Role of Sub-Orbital Flight ∗ S. Chiesaa, G. Russob, M. Fioritia, S. Corpinoa a Politecnico di Torino Department of Mechanical and Aerospace Engineering b AIDAA Sez. Napoletana c/o Department of Industrial Engineering \Federico II" - University of Naples Abstract The relevance and the main features of Hypersonic Flight are shortly presented and discussed. A synthetic overview of the few realisations and of many studies, projects and technological demonstrators offers opportunity of point out many interesting aspects. Then the more actual realisations and studies are considered, with particular attention to the new sector of small suborbital planes for Space Tourism. That gives opportunity of proposing a Road Map for an affordable and logic development of Hypersonic Flight, passing through the development of a suborbital Space Tourism plane on the basis of an existing subsonic business jet. Then the suborbital plane will constitute the basis of developing an Hypersonic Cruise Business Jet and, as a next step, a TSTO. 1. Introduction 2. Hypersonic Flight Concept The hypersonic flight is a subject on which the ef- It is considered appropriate to establish a definition forts of basic and applied aerospace research have been of hypersonic aircraft, useful to define the topic of dis- focused over the years. These efforts consisted in cussion; we define hypersonic aircraft a system capable the development of several projects and correspond- of taking off and landing horizontally (HOTOL - Hori- ing technological fields, such as aerodynamics, propul- zontal Take Off and Landing), and capable of flying at sion, structures capable of withstanding high thermal a Mach higher than 4.5. -
Is the World Ready for High-Speed Intercontinental Package Delivery (Yet)?
IAC-08-D2.4.5 IS THE WORLD READY FOR HIGH-SPEED INTERCONTINENTAL PACKAGE DELIVERY (YET)? John R. Olds* SpaceWorks Engineering, Inc. (SEI), United States of America (USA) [email protected] A.C. Charaniat SpaceWorks Engineering, Inc. (SEI), United States of America (USA) [email protected] Derek Webber:t Spaceport Associates, United States of America (USA) [email protected] Jon G. Wallace§ SpaceWorks Engineering, Inc. (SEI), United States of America (USA) [email protected] Michael Kelly** SpaceWorks Engineering, Inc. (SEI), United States of America (USA) [email protected] ABSTRACT This paper examines the prospects for a successful regularly-scheduled high-speed package delivery service for high-priority intercontinental cargo, notionally to be undertaken within the next decade or two. The topic is investigated from both technical/vehicle design and economics/business case points-of-view. Potential cargo include packages and priority items for which there might be a premium paid for speed, particularly if door-to-door service can be achieved fully one business day earlier than the fastest scheduled offerings currently available in the industry. The paper introduces a preliminary traffic model for a future business case, highlighting key routes and estimated daily volumes and price expected. Candidate flight vehicles and requisite technologies are discussed, with a particular point-to-point reference concept being presented to serve as the basis for non-recurring and recurring service cost estimates. The overall business case is then investigated, -
Computer Modelling of Aerothermodynamic Characteristics for Hypersonic Vehicles
Journal of Applied Mathematics and Physics, 2014, 2, 115-123 Published Online April 2014 in SciRes. http://www.scirp.org/journal/jamp http://dx.doi.org/10.4236/jamp.2014.25015 Computer Modelling of Aerothermodynamic Characteristics for Hypersonic Vehicles Yuri Ivanovich Khlopkov, Anton Yurievich Khlopkov, Zay Yar Myo Myint Department of Aeromechanics and Flight Engineering, Moscow Institute of Physics and Technology, Zhukovsky, Russia Email: [email protected], [email protected] Received December 2013 Abstract The purpose of this work is to describe the suitable methods for aerodynamic characteristics cal- culation of hypersonic vehicles in free molecular flow and the transitional regimes. Moving of the hypersonic vehicles at high altitude, it is necessary to know the behavior of its aerodynamic cha- racteristics for all flow regimes. Nowadays, various engineering approaches have been developed for modelling of aerodynamics of aircraft vehicle designs at initial state. The engineering method that described in this paper provides good results for the aerodynamic characteristics of various geometry designs of hypersonic vehicles in the transitional regime. In this paper present the cal- culation results of aerodynamic characteristics of various hypersonic vehicles in all range of re- gimes by using engineering method. Keywords Aerodynamic Characteristics, Computational Aerodynamics, Hypersonic Technology, Rarefied Gas Dynamics; Engineering Method, Aerodynamics in Transitional Regime 1. Introduction Theoretical studies of hypersonic flows associated with the creation of “Space Shuttle” to transport people and cargo into Earth orbit began in the last century. Research had been focused mainly on the department of TsAGI named after N.Y. Zhukovsky (Central Aerohydrodynamic Institute). Practical work on the creation of aerospace systems had been instructed engineering centre of the experimental design bureau named after A.I. -
Climate Change Two Satellites That Could Cool the Debate
February 2014 Target: Climate change Two satellites that could cool the debate Managing air traffic, page 32 Moonwalking with Buzz, page 24 WHAT HAPPENS WHEN MICHIGAN means business It’s a new day for business in Michigan. Through a series of recent initiatives, Michigan is once again becoming a preferred place for business. Starting with a new flat 6% business tax. The elimination of personal property taxes. New right-to-work legislation. All added to redesigned incentive programs and streamlined regulatory processes. All to create an ideal combination of opportunity, resources and passion for business right here in Michigan. 1.888.565.0052 michiganbusiness.org/AA Michigan Economic Development Corporation February 2014 DEPARTMENTS EDITOR’S NOTEBOOK 2 Unsettled business. LETTERS TO THE EDITOR 3 Show some optimism. INTERNATIONAL BEAT 4 Space tourism sets sights on 2014. SCITECH 2014 8 Page 32 News and quotes from the annual forum. CONVERSATION 10 NASA’s chief scientest Ellen Stofan. ENGINEERING NOTEBOOK 12 Laser eye on aircraft ice. GREEN ENGINEERING 16 Runway taxiing goes green. CAREER PROFILE 18 Outreach 101: Listen. THE VIEW FROM HERE 20 Grading “Gravity”. Page 24 OUT OF THE PAST 44 CAREER OPPORTUNITIES 46 FEATURES “MOONWALKING” WITH BUZZ 24 Buzz Aldrin and the author travel together on a book tour. by Leonard David TARGET: CLIMATE CHANGE 26 Page 20 In the next two years, NASA will launch satellites to study the concentration of carbon dioxide in the atmosphere. by Natalia Mironova AIR TRAFFIC CONTROLLERS FACE AUTOMATION 32 Page 16 The promised revolution in air traffic management will bring automation on a grand scale. -
Vysoké Učení Technické V Brně Brno University of Technology
VYSOKÉ UČENÍ TECHNICKÉ V BRNĚ BRNO UNIVERSITY OF TECHNOLOGY FAKULTA STROJNÍHO INŽENÝRSTVÍ LETECKÝ ÚSTAV FACULTY OF MECHANICAL ENGINEERING INSTITUTE OF AEROSPACE ENGINEERING PŘEHLED VÝVOJE KOSMICKÝCH RAKETOPLÁNŮ SURVEY OF THE SPACE ROCKETPLANES DEVELOPMENT BAKALÁŘSKÁ PRÁCE BACHELOR'S THESIS AUTOR PRÁCE TOMÁŠ KAPOUN AUTHOR VEDOUCÍ PRÁCE doc. Ing. VLADIMÍR DANĚK, CSc. SUPERVISOR BRNO 2013 Vysoké učení technické v Brně, Fakulta strojního inženýrství Letecký ústav Akademický rok: 2012/2013 ZADÁNÍ BAKALÁŘSKÉ PRÁCE student(ka): Tomáš Kapoun který/která studuje v bakalářském studijním programu obor: Strojní inženýrství (2301R016) Ředitel ústavu Vám v souladu se zákonem č.111/1998 o vysokých školách a se Studijním a zkušebním řádem VUT v Brně určuje následující téma bakalářské práce: Přehled vývoje kosmických raketoplánů v anglickém jazyce: Survey of the Space Rocketplanes Development Stručná charakteristika problematiky úkolu: Mnohonásobně použitelné kosmické dopravní prostředky se staly předmětem vývoje na počátku 70. let. Z mnoha koncepčních návrhů se ukázalo, že z ekonomických důvodů není doposud přijatelná varianta dvoustupňového kosmického dopravního systému. Řešení vedlo jen k částečně vícenásobně použitelnému kosmickému dopravnímu systému. Předmětem bakalářské práce by měl být historicko-technický přehled vývoje raketoplánů. Cíle bakalářské práce: Vypracujte historicko-technický přehled vývoje vícenásobně použitelných kosmických dopravních systémů založených na využívání aerodynamického principu návratu orbitálního stupně do hustých vrstev atmosféry a při přistání. Zpracujte přehled počátků vývoje suborbitálních raketoplánů a vztlakových těles. Technické a ekonomické problémy vývoje orbitálních raketoplánů a poznatky z jejich dosavadního provozu. Budoucnost využití vícenásobně použitelných kosmických dopravních systémů. Seznam odborné literatury: [1] MARTINEK,F. Z historie a současnosti kosmických raketoplánů. Vlašské Meziříčí: Hvězdárna Valašské Meziříčí, 1997. 144 s. ISBN 80-902445-2-1 [2] ISAKOWITZ, Steven J. -
Theotherguysnasa Needs a Space Taxi. the Likely Pick Is Spacex
NASA needs a space taxi. The likely pick is SpaceX — but don’t count out this Colorado company. The Other Guys BY MICHAEL BEHAR STANDING BESIDE Dream Chaser, for our nation. It’s the opportunity to get the United States back into launching it’s hard to ignore its resemblance humans into space.” to the space shuttle. It’s smaller— Voss showed me around the bay where Sierra Nevada is constructing Dream only 30 feet long from nose to Chaser, a seven-passenger reusable space- tail—and the wings are upswept plane that, if it is selected by NASA, would be carried to space atop an Atlas V rocket. and canted. But in overall shape, After decoupling from its launch vehicle, Dream Chaser would ignite its engines the kinship is clear. Still, the com- to reach its final destination. It’s capable pany building this vehicle says of docking with the ISS, or performing a variety of multi-day missions in low Earth it is not trying to make Shuttle orbit, then returning home in a glide to a 2.0. “We’re not fixing all the shut- runway landing. While Dream Chaser is based on a long-established aerodynamic tle’s problems,” avows Jim Voss, concept called a lifting body, it incorporates the avuncular vice president of numerous innovations never before used Opposite: Vying for the job of frst commercial astronaut hauler, Dream Chaser got on a manned orbital vehicle, including put through its aerodynamic paces last year when its maker, Sierra Nevada, dangled Sierra Nevada Corporation’s Space hybrid-fueled engines and a carbon-fiber it from an Erickson Air-Crane helicopter over Jeferson County, Colorado. -
Performance Analysis of Skip-Glide Trajectories for Hypersonic Waveriders in Planetary Exploration
University of Tennessee, Knoxville TRACE: Tennessee Research and Creative Exchange Masters Theses Graduate School 5-2008 Performance Analysis of Skip-Glide Trajectories for Hypersonic Waveriders in Planetary Exploration Ngoc-Thuy Dang Nguyen University of Tennessee - Knoxville Follow this and additional works at: https://trace.tennessee.edu/utk_gradthes Part of the Aerospace Engineering Commons Recommended Citation Nguyen, Ngoc-Thuy Dang, "Performance Analysis of Skip-Glide Trajectories for Hypersonic Waveriders in Planetary Exploration. " Master's Thesis, University of Tennessee, 2008. https://trace.tennessee.edu/utk_gradthes/416 This Thesis is brought to you for free and open access by the Graduate School at TRACE: Tennessee Research and Creative Exchange. It has been accepted for inclusion in Masters Theses by an authorized administrator of TRACE: Tennessee Research and Creative Exchange. For more information, please contact [email protected]. To the Graduate Council: I am submitting herewith a thesis written by Ngoc-Thuy Dang Nguyen entitled "Performance Analysis of Skip-Glide Trajectories for Hypersonic Waveriders in Planetary Exploration." I have examined the final electronic copy of this thesis for form and content and recommend that it be accepted in partial fulfillment of the equirr ements for the degree of Master of Science, with a major in Aerospace Engineering. Gary A. Flandro, Major Professor We have read this thesis and recommend its acceptance: Kenneth R. Kimble, John S. Steinhoff Accepted for the Council: Carolyn R. Hodges