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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). -
Trends in Missile Technologies 39 the International Institute for Strategic Studies (IISS) Douglas Barrie
King’s Research Portal Document Version Publisher's PDF, also known as Version of record Link to publication record in King's Research Portal Citation for published version (APA): Brockman, K., Bauer, S., Boulanin, V., & Lentzos, F. (2019). New developments in biology. In Conference Reader: Capturing Technology. Rethinking Arms Control. German Federal Foreign Office. https://rethinkingarmscontrol.de/wp-content/uploads/2019/03/2019.-Capturing-Technology.Rethinking-Arms- Control_-Conference-Reader.pdf Citing this paper Please note that where the full-text provided on King's Research Portal is the Author Accepted Manuscript or Post-Print version this may differ from the final Published version. If citing, it is advised that you check and use the publisher's definitive version for pagination, volume/issue, and date of publication details. And where the final published version is provided on the Research Portal, if citing you are again advised to check the publisher's website for any subsequent corrections. General rights Copyright and moral rights for the publications made accessible in the Research Portal are retained by the authors and/or other copyright owners and it is a condition of accessing publications that users recognize and abide by the legal requirements associated with these rights. •Users may download and print one copy of any publication from the Research Portal for the purpose of private study or research. •You may not further distribute the material or use it for any profit-making activity or commercial gain •You may freely distribute the URL identifying the publication in the Research Portal Take down policy If you believe that this document breaches copyright please contact [email protected] providing details, and we will remove access to the work immediately and investigate your claim. -
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. -
CUWS Outreach Journal Issue 1313
Issue No. 1313 4 May 2018 // USAFCUWS Outreach Journal Issue 1313 // Feature Report “Energy and Water Development Appropriations: Nuclear Weapons Activities”. Written by Amy F. Woolf, published by the Congressional Research Service; April 18, 2018 https://fas.org/sgp/crs/nuke/R44442.pdf Summary The annual Energy and Water Development appropriations bill funds civil works projects of the Army Corps of Engineers, the Department of the Interior’s Bureau of Reclamation, the Department of Energy (DOE), and several independent agencies. The DOE budget includes funding for the National Nuclear Security Administration (NNSA), a separately organized agency within DOE. NNSA operates three programs: Defense Nuclear Nonproliferation, which secures nuclear materials worldwide, conducts research and development (R&D) into nonproliferation and verification, and operates the Nuclear Counterterrorism and Incident Response Program; Naval Reactors, which “is responsible for all U.S. Navy nuclear propulsion work”; and Weapons Activities. The last is the subject of this report. The Weapons Activities account supports programs that maintain U.S. nuclear missile warheads and gravity bombs and the infrastructure programs that support that mission. Specifically, according to DOE’s budget documentation, these programs “support the maintenance and refurbishment of nuclear weapons to continue sustained confidence in their safety, reliability, and performance; continued investment in scientific, engineering, and manufacturing capabilities to enable certification of the enduring nuclear weapons stockpile; and manufacture of nuclear weapons components.” NNSA’s budget request for FY2019 seeks $11.02 billion for Weapons Activities within a total of budget of $15.09 billion for NNSA. This represents a 3.6% increase over the $10.642 billion for Weapons Activities in the Consolidated Appropriations Act, 2018 (P.L. -
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. -
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. -
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 -
Technology Needs Test Requirements Hypersonic Airframe Structl Xes
NASA Contractor Report 3130 LOXff AFWL KIRT Hypersonic Airframe Structl xes Technology Needs and Flight Test Requirements J. E. Stone and L. C. Koch CONTRACT NASl-14924 JULY 1979 TECH LIBRARY KAFB, NM IIlliilll Illill 00bm4liiliII/l llilllillllSlllll NASA Contractor Report 3130 Hypersonic Airframe Structures Technology Needs and Flight Test Requirements J. E. Stone and L. C. Koch McDomel~ Don&s Corporation St. Louis, Missom-i Prepared for Langley Research Center under Contracr NASl-14724 IUASA Nalional Aeronautics and Space Administration Scientific and Technical Information Branch FOREWORD The overall objectives of this study were to identify the technological advances required in airframe structures for hypersonic vehicle applications and to define the role that flight testing can play in accomplishing these advances. The study was conducted, in 1977, in accordance with the requirements and instructions of NASA RFP l-16-2700.0042 and McDonnell Technical Proposal Report MDC A4748. Customary units were used for the principal measurements and calculations and converted to the International System of Units (S.I.) for the final report. James E. Stone was the MCAIR Program Manager and Principal Investigator for this study. Leland C. Koch served as the MCAIR Technical Advisor and contributed greatly co the study. Numerous MUIR personnel contributed, within their fields of expertise, to the report. TWO eminent professors, E. E. Sechler uf the California Institute of Technology and R. H. Miller of the Massachusetts Institute of Technology, also served as Technical Advisors for this study. TABLE OF CONTENTS Section Title a 1. SulmARY ............................... 1 2. INTRODUCTION. ............................ 5 3. HYPERSONIC VEHICLE APPLICATIONS ................... i 3.1 Potential Applications .................... -
High Speed/Hypersonic Aircraft Propulsion Technology Development
High Speed/Hypersonic Aircraft Propulsion Technology Development Charles R. McClinton Retired NASA LaRC 3724 Dewberry Lane Saint James City, FL 33956 USA [email protected] ABSTRACT H. Julian Allen made an important observation in the 1958 21st Wright Brothers Lecture [1]: “Progress in aeronautics has been brought about more by revolutionary than evolutionary changes in methods of propulsion.” Numerous studies performed over the past 50 years show potential benefits of higher speed flight systems – for aircraft, missiles and spacecraft. These vehicles will venture past classical supersonic speed, into hypersonic speed, where perfect gas laws no longer apply. The revolutionary method of propulsion which makes this possible is the Supersonic Combustion RAMJET, or SCRAMJET engine. Will revolutionary applications of air-breathing propulsion in the 21st century make space travel routine and intercontinental travel as easy as intercity travel is today? This presentation will reveal how this high speed propulsion system works, what type of aerospace systems will benefit, highlight challenges to development, discuss historic development (in the US as an example), highlight accomplishments of the X-43 scramjet-powered aircraft, and present what needs to be done next to complete this technology development. 1.0 HIGH SPEED AIRBREATHING ENGINES 1.1 Scramjet Engines The scramjet uses a slightly modified Brayton Cycle [2] to produce power, similar to that used for both the classical ramjet and turbine engines. Air is compressed; fuel injected, mixed and burned to increase the air – or more accurately, the combustion products - temperature and pressure; then these combustion products are expanded. For the turbojet engine, air is mechanically compressed by work extracted from the combustor exhaust using a turbine.