Facing the Heat Barrier: a History of Hypersonics
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Twenty-First Century Space Propulsion Study
AD-A229 279A AL-TR-90-030 AD: FiaRFILE CPY Final Report T for tihe period 21st Century Space Propulsion Study 30 Jul 1987 to 30 Apr 1990 DTIC ELECTE D NOV 141990 October 1990 Author: Forward Unlimited Dr R.L. Forward RO.Box 2783 Malibu CA 90265-7783 F04611-87-C-0029 Approved for Public Release Distribution Is unlimited. The AL Technical Services Office has reviewed this report, and it Is releasable to the National Technical Information Service, where it will be available to the general public, including foreign nationals. Prepared for the: Astronautics Laboratory (AFSC) Air Force Space Technology Center Space Systems Division Air Force Systems Command Sf Edwards AFB CA 93523-5000 NOTICE When U. S. Government drawings, specifications, or other data are used for any purpose other than a definitely related Government procurement operatictt, the fact that the Govern- ment may have formulated, furnished, or in any way supphrd the said drawings, V specifications, or other data, is not to be regarded by implication or otherwise, or in any way licensing the holder or any other person or corporation, or conveying any rights or permission to manufacture, use or sell any patented invention that may be related thereto. FOREWORD This final report was submitted by Forward Unlimited, Malibu CA on completion of contract F04611-87-C-0029 with the Astronautics Laboratbry (AFSC), Edwards AFB CA. AL Project Manager was Dr Franklin B. Mead, Jr.. This report has been reviewed and is approved for release and distribution in accordance with the distribution statement on the cover and on the DD Form 1473. -
The Power for Flight: NASA's Contributions To
The Power Power The forFlight NASA’s Contributions to Aircraft Propulsion for for Flight Jeremy R. Kinney ThePower for NASA’s Contributions to Aircraft Propulsion Flight Jeremy R. Kinney Library of Congress Cataloging-in-Publication Data Names: Kinney, Jeremy R., author. Title: The power for flight : NASA’s contributions to aircraft propulsion / Jeremy R. Kinney. Description: Washington, DC : National Aeronautics and Space Administration, [2017] | Includes bibliographical references and index. Identifiers: LCCN 2017027182 (print) | LCCN 2017028761 (ebook) | ISBN 9781626830387 (Epub) | ISBN 9781626830370 (hardcover) ) | ISBN 9781626830394 (softcover) Subjects: LCSH: United States. National Aeronautics and Space Administration– Research–History. | Airplanes–Jet propulsion–Research–United States– History. | Airplanes–Motors–Research–United States–History. Classification: LCC TL521.312 (ebook) | LCC TL521.312 .K47 2017 (print) | DDC 629.134/35072073–dc23 LC record available at https://lccn.loc.gov/2017027182 Copyright © 2017 by the National Aeronautics and Space Administration. The opinions expressed in this volume are those of the authors and do not necessarily reflect the official positions of the United States Government or of the National Aeronautics and Space Administration. This publication is available as a free download at http://www.nasa.gov/ebooks National Aeronautics and Space Administration Washington, DC Table of Contents Dedication v Acknowledgments vi Foreword vii Chapter 1: The NACA and Aircraft Propulsion, 1915–1958.................................1 Chapter 2: NASA Gets to Work, 1958–1975 ..................................................... 49 Chapter 3: The Shift Toward Commercial Aviation, 1966–1975 ...................... 73 Chapter 4: The Quest for Propulsive Efficiency, 1976–1989 ......................... 103 Chapter 5: Propulsion Control Enters the Computer Era, 1976–1998 ........... 139 Chapter 6: Transiting to a New Century, 1990–2008 .................................... -
The Rise and Fall of Missiles in the Us Air Force, 1957-1967
FLAMEOUT: THE RISE AND FALL OF MISSILES IN THE U.S. AIR FORCE, 1957-1967 A Dissertation by DAVID WILLIAM BATH Submitted to the Office of Graduate and Professional Studies of Texas A&M University in partial fulfillment of the requirements for the degree of DOCTOR OF PHILOSOPHY Chair of Committee, Joseph G. Dawson, III Committee Members, Terry H. Anderson Olga Dror Angela Pulley Hudson James Burk Head of Department, David Vaught December 2015 Major Subject: History Copyright 2015 David William Bath ABSTRACT This dissertation documents how the U.S. national perspective toward ballistic nuclear missiles changed dramatically between 1957 and 1967 and how the actions and attitudes of this time brought about long term difficulties for the nation, the Air Force, and the missile community. In 1957, national leaders believed that ballistic missiles would replace the manned bomber and be used to win an anticipated third world war between communist and capitalist nations. Only ten years later, the United States was deep into a limited war in Vietnam and had all but proscribed the use of nuclear missiles. This dissertation uses oral histories, memoirs, service school theses, and formerly classified government documents and histories to determine how and why the nation changed its outlook on nuclear ballistic missiles so quickly. The dissertation contends that because scientists and engineers created the revolutionary weapon at the beginning of the Cold War, when the U.S. and U.S.S.R. were struggling for influence and power, many national leaders urged the military to design and build nuclear ballistic missiles before the Soviet Union could do so. -
Facing the Heat Barrier: a History of Hypersonics First Thoughts of Hypersonic Propulsion
Facing the Heat Barrier: A History of Hypersonics First Thoughts of Hypersonic Propulsion Republic’s Aerospaceplane concept showed extensive engine-airframe integration. (Republic Aviation) For takeoff, Lockheed expected to use Turbo-LACE. This was a LACE variant that sought again to reduce the inherently hydrogen-rich operation of the basic system. Rather than cool the air until it was liquid, Turbo-Lace chilled it deeply but allowed it to remain gaseous. Being very dense, it could pass through a turbocom- pressor and reach pressures in the hundreds of psi. This saved hydrogen because less was needed to accomplish this cooling. The Turbo-LACE engines were to operate at chamber pressures of 200 to 250 psi, well below the internal pressure of standard rockets but high enough to produce 300,000 pounds of thrust by using turbocom- pressed oxygen.67 Republic Aviation continued to emphasize the scramjet. A new configuration broke with the practice of mounting these engines within pods, as if they were turbojets. Instead, this design introduced the important topic of engine-airframe integration by setting forth a concept that amounted to a single enormous scramjet fitted with wings and a tail. A conical forward fuselage served as an inlet spike. The inlets themselves formed a ring encircling much of the vehicle. Fuel tankage filled most of its capacious internal volume. This design study took two views regarding the potential performance of its engines. One concept avoided the use of LACE or ACES, assuming again that this craft could scram all the way to orbit. Still, it needed engines for takeoff so turbo- ramjets were installed, with both Pratt & Whitney and General Electric providing Lockheed’s Aerospaceplane concept. -
Part 2 of This Article Will Describe the Thunderchief's
On the cover: Two F-16C Fighting Falcons from the 177th Fighter Wing fly over MetLife Stadium in East Rutherford, New Jersey on Nov. 8, 2015 prior to the “Salute The Service” game between the NY Jets and the Jacksonville Jaguars. The ceremonies were opened by an enlistment of new troops in the end zone, followed by jumpers from the United States Military Academy- West Point Parachute Team and concluded with a giant 40 yard U.S. flag being unfurled by representatives from each branch of service for the singing of the National Anthem and the flyover. (Photo courtesy of John Iocono - Pro Football Hall of Fame) NOVEMBER 2015, VOL. 49 NO. 11 THE CONTRAIL STAFF 177TH FW COMMANDER COL . JOHN R. DiDONNA CHIEF, PUBLIC AFFAIRS CAPT. AMANDA BATIZ EDITOR/PUBLIC AFFAIRS SUPERINTENDENT MASTER SGT. ANDREW J. MOSELEY PHOTOJOURNALIST TECH. SGT. ANDREW J. MERLOCK PHOTOJOURNALIST SENIOR AIRMAN SHANE S. KARP PHOTOJOURNALIST SENIOR AIRMAN AMBER POWELL AVIATION HISTORIAN DR. RICHARD PORCELLI WWW.177FW.ANG.AF.MIL This funded newspaper is an authorized monthly publication for members of the U.S. Military Services. Contents of The Contrail are not necessarily the official view of, or endorsed by, the 177th Fighter Wing, the U.S. Government, the Department of Defense or the Depart- On desktop computers, click For back issues of The Contrail, ment of the Air Force. The editorial content is edited, prepared, and provided by the Public Affairs Office of the 177th Fighter Wing. All Ctrl+L for full screen. On mobile, and other multimedia products photographs are Air Force photographs unless otherwise indicated. -
Mars Exploration Entry, Descent and Landing Challenges1,2
Mars Exploration Entry, Descent and Landing Challenges1,2 Robert D. Braun Robert M. Manning Georgia Institute of Technology Jet Propulsion Laboratory Atlanta, GA 30332-0150 California Institute of Technology (404) 385-6171 Pasadena, CA 91109 [email protected] (818) 393-7815 [email protected] Abstract—The United States has successfully landed five interesting locations within close proximity (10’s of m) of robotic systems on the surface of Mars. These systems all pre-positioned robotic assets. These plans require a had landed mass below 0.6 metric tons (t), had landed simultaneous two order of magnitude increase in landed footprints on the order of hundreds of km and landed at sites mass capability, four order of magnitude increase in landed below -1 km MOLA elevation due the need to perform accuracy, and an entry, descent and landing operations entry, descent and landing operations in an environment sequence that may need to be completed in a lower density with sufficient atmospheric density. Current plans for (higher surface elevation) environment. This is a tall order human exploration of Mars call for the landing of 40-80 t that will require the space qualification of new EDL surface elements at scientifically interesting locations within approaches and technologies. close proximity (10’s of m) of pre-positioned robotic assets. This paper summarizes past successful entry, descent and Today, robotic exploration systems engineers are struggling landing systems and approaches being developed by the with the challenges of increasing landed mass capability to 1 robotic Mars exploration program to increased landed t while improving landed accuracy to 10’s of km and performance (mass, accuracy and surface elevation). -
Mimi WI NR Form
NPS Form 10-900 OMB No. 10024-0018 (January 1992) United States Department of Interior National Park Service National Register of Historic Places Registration Form This form is for use in nominating or requesting determinations for individual properties and districts. See instructions in How to Complete the National Register of Historic Places Registration Form (National Register Bulletin 16A). Complete each item by marking "x" in the appropriate box or by entering the information requested. If an item does not apply to the property being documented, enter "N/A" for "not applicable." For functions, architectural classification, materials, and areas of significance, enter only categories and subcategories from the instructions. Place additional entries and narrative items on continuation sheets (NPS Form 10-900A). Use a typewriter, word processor, or computer, to complete all items. 1. Name of Property historic name Minuteman ICBM Launch Control Facility Delta-01 and Launch Facility Delta-09, Ellsworth Air Force Base other names/site number Minuteman Missile National Historic Site (MIMI) 2. Location street & number Minuteman Missile National Historic Site (MIMI), Delta-01: W side Jackson CR CS23A, approx. .5 mi. N of I-90, Exit 127 city or town Cottonwood Vicinity X state South Dakota code SD county Jackson code 071 zip code 57775 (see continuation sheet) 3. State/Federal Agency Certification As the designated authority under the National Historic Preservation Act, as amended, I hereby certify that this X nomination request for determination of eligibility meets the documentation standards for registering properties in the National Register of Historic Places and meets the procedural and professional requirements set forth in 36 CFR Part 60. -
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, -
Chang'e Flying to the Moon
Issue 7 January 2013 All about the Chinese Space Programme GO TAIKONAUTS! Editor’s Note COVER STORY If you are a fan of the Chinese space pro- gramme, you must have heard about Brian Harvey, who is the first Western writer to publish a book on the Chinese space pro- gramme. We are very happy that Mr. Harvey contributed an article to Go Taikonauts! The article about Chinese ... page 2 Quarterly Report October - December 2012 Launch Events China made six space launches in the last three months of 2012, setting a new annual launch record of 19 and overtaking U.S. in number of suc- cessful annual space launches for the first time. In 2011, China also ... page 3 Deep Space Adventure of Chang’e 2 From A Backup Lunar Orbiter to An Asteroid Probe Observation Just before Chang’e 1 (CE-1)’s successful mission to the Moon was completed, Echo of the Curiosity in China China announced that they would send the second lunar probe Chang’e 2 (CE-2) The 6 August 2012 was a special day to an to the Moon in 2010. No one at that time could anticipate the surprises that CE-2 American-Chinese girl. She is Clara Ma, would bring a few years later since it was just a backup ... page 8 a 15-year-old middle school student from Lenexa, Kansas. She waited for this day for more than three years. In May 2009, History Ma won a NASA essay contest for naming the Mars Science Laboratory, the most Chang’e Flying to the Moon complicated machine .. -
Suborbital Reusable Launch Vehicles and Applicable Markets
SUBORBITAL REUSABLE LAUNCH VEHICLES AND APPLICABLE MARKETS Prepared by J. C. MARTIN and G. W. LAW Space Launch Support Division Space Launch Operations October 2002 Space Systems Group THE AEROSPACE CORPORATION El Segundo, CA 90245-4691 Prepared for U. S. DEPARTMENT OF COMMERCE OFFICE OF SPACE COMMERCIALIZATION Herbert C. Hoover Building 14th and Constitution Ave., NW Washington, DC 20230 (202) 482-6125, 482-5913 Contract No. SB1359-01-Z-0020 PUBLIC RELEASE IS AUTHORIZED Preface This report has been prepared by The Aerospace Corporation for the Department of Commerce, Office of Space Commercialization, under contract #SB1359-01-Z-0020. The objective of this report is to characterize suborbital reusable launch vehicle (RLV) concepts currently in development, and define the military, civil, and commercial missions and markets that could capitalize on their capabilities. The structure of the report includes a brief background on orbital vs. suborbital trajectories, as well as an overview of expendable and reusable launch vehicles. Current and emerging market opportunities for suborbital RLVs are identified and discussed. Finally, the report presents the technical aspects and program characteristics of selected U.S. and international suborbital RLVs in development. The appendix at the end of this report provides further detail on each of the suborbital vehicles, as well as the management biographies for each of the companies. The integration of suborbital RLVs with existing airports and/or spaceports, though an important factor that needs to be evaluated, was not the focus of this effort. However, it should be noted that the RLV concepts discussed in this report are being designed to minimize unique facility requirements. -
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.