Noise and Climate Impacts of an Unconstrained Commercial Supersonic Network
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Concorde Is a Museum Piece, but the Allure of Speed Could Spell Success
CIVIL SUPERSONIC Concorde is a museum piece, but the allure Aerion continues to be the most enduring player, of speed could spell success for one or more and the company’s AS2 design now has three of these projects. engines (originally two), the involvement of Air- bus and an agreement (loose and non-exclusive, by Nigel Moll but signed) with GE Aviation to explore the supply Fourteen years have passed since British Airways of those engines. Spike Aerospace expects to fly a and Air France retired their 13 Concordes, and for subsonic scale model of the design for the S-512 the first time in the history of human flight, air trav- Mach 1.5 business jet this summer, to explore low- elers have had to settle for flying more slowly than speed handling, followed by a manned two-thirds- they used to. But now, more so than at any time scale supersonic demonstrator “one-and-a-half to since Concorde’s thunderous Olympus afterburn- two years from now.” Boom Technology is working ing turbojets fell silent, there are multiple indi- on a 55-seat Mach 2.2 airliner that it plans also to cations of a supersonic revival, and the activity offer as a private SSBJ. NASA and Lockheed Martin appears to be more advanced in the field of busi- are encouraged by their research into reducing the ness jets than in the airliner sector. severity of sonic booms on the surface of the planet. www.ainonline.com © 2017 AIN Publications. All Rights Reserved. For Reprints go to Shaping the boom create what is called an N-wave sonic boom: if The sonic boom produced by a supersonic air- you plot the pressure distribution that you mea- craft has long shaped regulations that prohibit sure on the ground, it looks like the letter N. -
Ovrhyp, Scramjet Test Aircraft STATE UNIVERSITY Student Authors: J
https://ntrs.nasa.gov/search.jsp?R=19910000728 2020-03-19T20:21:21+00:00Z /z7 H OVRhyp, Scramjet Test Aircraft STATE UNIVERSITY Student Authors: J. Asian, T. Bisard, S. Dallinga, K. Draper, G. Hufford, W. Peters, and J. Rogers Supervisor: Dr. G. M. Gregorek Assistant: R. L. Reuss Department of Aeronautical & Astronautical Engineering Universities Space Research Association Houston, Texas 77058 Subcontract Dated November 17, 1989 Final Report May 1990 03/0_ OVRhyp, Scramjet Test Aircraft UNIVERSITY Student Authors: J. Asian, T. Bisard, S. Dallinga, K. Draper, G. Hufford, W. Peters, and J. Rogers Supervisor: Dr. G. M. Gregorek Assistant: R. L. Reuss Department of Aeronautical & Astronautical Engineering Universities Space Research Association Houston, Texas 77058 Subcontract Dated November 17, 1989 Final Report RF Project 767919/722941 May 1990 ABSTRACT (Gary Huff0rd} A preliminary design for an unmanned hypersonic research vehicle to test scramjet engines is presented. The aircraft will be launched from a carrier aircraft at an altitude of 4Q,0QQ feet at Mach 0.8. The vehicle will then accelerate to Mach 6 at an altitude of 100,000 feet. At this stage the prototype scramjet will be employed to accelerate the vehicle to Mach 10 and maintain Mach IQ flight for 2 minutes. The aircraft will then decelerate and safely land, presumably at NASA Dryden F[i_ht Test Center. ii TABLE OF CONTENTS ABSTRACT ............................ ii TABLE OF CONTENTS ....................... iii LIST OF FIGURES ......................... v INTRODUCTION .......................... vi CONFIGURATION .......................... WEIGHTS ANALYSIS ........................ 12 PURPOSE ............................. 12 METHOD ........................... 12 SYSTEMS .......................... 14 AERODYNAMIC SURFACES .................... 14 BODY STRUCTURE ....................... 15 THERMAL PROTECTION SYSTEM ................. 15 LAUNCH AND LANDING SYSTEM ................ -
Getting Shipshape
AER October 2020 OSPACE DOES AEROSPACE HAVE A RACE PROBLEM? SECRETS FROM THE FALKLANDS AIR WAR POWERING UP ELECTRIC FLIGHT www.aerosociety.com October 2020 GETTING SHIPSHAPE Volume 47 Number 10 Volume UK F-35B FORCE GETS READY FOR FIRST OPERATIONAL CARRIER DEPLOYMENT Royal AeronauticaSociety OCTOBER 2020 AEROSPACE COVER FINAL.indd 1 18/09/2020 14:59 RAeS 2020 Virtual Conference Programme Join us from wherever you are in the world to experience high quality, informative content. Book early for our special introductory offer rates. STRUCTURES & MATERIALS UAS / ROTORCRAFT / AIR TRANSPORT GREENER BY DESIGN 7th Aircraft Structural Urban Air Mobility RAeS Climate Change Design Conference Conference 2020 Conference 2020 DATE NEW DATE DATE 8 October 22 - 23 October 3 - 4 November TIME TIME TIME 14:00 - 17:00 13:00 - 18:00 13:00 - 18:00 SCAN USING SCAN USING SCAN USING YOUR PHONE YOUR PHONE YOUR PHONE FOR MORE INFO FOR MORE INFO FOR MORE INFO Embark on your virtual learning journey with the RAeS Connect and interact with our speakers and ask questions live Engage and network with other professionals from across the world Meet our sponsors at our virtual exhibitor booths Access content post-event to continue your professional development For the full virtual conference programme and further details on what to expect visit aerosociety.com/VCP Volume 47 Number 10 October 2020 EDITORIAL Contents When global rules unravel Regulars 4 Radome 12 Transmission What price global standards, rules and regulations? Pre-pandemic there were The latest aviation and Your letters, emails, tweets aeronautical intelligence, and social media feedback. -
W Oltoria Di Un Uo Non Man at Taman Antonio La D
W OLTORIA DI UN USUO NON20180134382A1 MAN AT TAMAN ANTONIOLA D ( 19) United States (12 ) Patent Application Publication ( 10) Pub . No. : US 2018 /0134382 A1 Scholl et al. (43 ) Pub . Date : May 17 , 2018 ( 54 ) COMMERCIAL SUPERSONIC AIRCRAFT Publication Classification AND ASSOCIATED SYSTEMS AND (51 ) Int. Cl. METHODS B64C 30 / 00 (2006 .01 ) B64D 13 /08 ( 2006 . 01) ( 71) Applicant: Boom Technology, Inc. , Englewood , B64D 43 / 00 (2006 . 01 ) CO (US ) B64D 11 /06 ( 2006 .01 ) (72 ) Inventors : Nathaniel Blake Scholl, Englewood , (52 ) U . S . CI. CO (US ) ; Joe Wilding, Englewood , CO CPC . .. .. B64C 30 / 00 ( 2013 .01 ) ; B64D 13 / 08 (US ) ; Josh Krall, Englewood , CO (2013 .01 ) ; B64D 2013 /0618 (2013 .01 ) ; B64D (US ) ; Andy Berryann , Englewood , CO 11 / 064 (2014 . 12 ); B64D 43 / 00 ( 2013 .01 ) (US ) ; Michael Reid , Englewood , CO (US ) (57 ) ABSTRACT Commercial supersonic aircraft and associated systems and ( 21 ) Appl. No. : 15 /811 ,327 methods . A representative commercial supersonic aircraft includes a fuselage configured to carry a crew and between ( 22 ) Filed : Nov . 13 , 2017 20 and 60 passengers, a delta wing mounted to the fuselage , and a propulsion system carried by at least one of the wing Related U . S . Application Data and the fuselage , the propulsion system including a plurality (60 ) Provisional application No . 62 /421 , 870 , filed on Nov . of engines , at least one variable - geometry inlet , and at least 14 , 2016 . one variable - geometry nozzle . 101 103 100 102 51216 Chen 110 - - - - 000000 - - -
Some Supersonic Aerodynamics
Some Supersonic Aerodynamics W.H. Mason Configuration Aerodynamics Class Grumman Tribody Concept – from 1978 Company Calendar The Key Topics • Brief history of serious supersonic airplanes – There aren’t many! • The Challenge – L/D, CD0 trends, the sonic boom • Linear theory as a starting point: – Volumetric Drag – Drag Due to Lift • The ac shift and cg control • The Oblique Wing • Aero/Propulsion integration • Some nonlinear aero considerations • The SST development work • Brief review of computational methods • Possible future developments Are “Supersonic Fighters” Really Supersonic? • If your car’s speedometer goes to 120 mph, do you actually go that fast? • The official F-14A supersonic missions (max Mach 2.4) – CAP (Combat Air Patrol) • 150 miles subsonic cruise to station • Loiter • Accel, M = 0.7 to 1.35, then dash 25nm – 4 ½ minutes and 50nm total • Then, head home or to a tanker – DLI (Deck Launch Intercept) • Energy climb to 35K ft., M = 1.5 (4 minutes) • 6 minutes at 1.5 (out 125-130nm) • 2 minutes combat (slows down fast) After 12 minutes, must head home or to a tanker Very few real supersonic airplanes • 1956: the B-58 (L/Dmax = 4.5) – In 1962: Mach 2 for 30 minutes • 1962: the A-12 (SR-71 in ’64) (L/Dmax = 6.6) – 1st supersonic flight, May 4, 1962 – 1st flight to exceed Mach 3, July 20, 1963 • 1964: the XB-70 (L/Dmax = 7.2) – In 1966: flew Mach 3 for 33 minutes • 1968: the TU-144 – 1st flight: Dec. 31, 1968 • 1969: the Concorde (L/Dmax = 7.4) – 1st flight, March 2, 1969 • 1990: the YF-22 and YF-23 (supercruisers) – YF-22: 1st flt. -
Aircraft of Today. Aerospace Education I
DOCUMENT RESUME ED 068 287 SE 014 551 AUTHOR Sayler, D. S. TITLE Aircraft of Today. Aerospace EducationI. INSTITUTION Air Univ.,, Maxwell AFB, Ala. JuniorReserve Office Training Corps. SPONS AGENCY Department of Defense, Washington, D.C. PUB DATE 71 NOTE 179p. EDRS PRICE MF-$0.65 HC-$6.58 DESCRIPTORS *Aerospace Education; *Aerospace Technology; Instruction; National Defense; *PhysicalSciences; *Resource Materials; Supplementary Textbooks; *Textbooks ABSTRACT This textbook gives a brief idea aboutthe modern aircraft used in defense and forcommercial purposes. Aerospace technology in its present form has developedalong certain basic principles of aerodynamic forces. Differentparts in an airplane have different functions to balance theaircraft in air, provide a thrust, and control the general mechanisms.Profusely illustrated descriptions provide a picture of whatkinds of aircraft are used for cargo, passenger travel, bombing, and supersonicflights. Propulsion principles and descriptions of differentkinds of engines are quite helpful. At the end of each chapter,new terminology is listed. The book is not available on the market andis to be used only in the Air Force ROTC program. (PS) SC AEROSPACE EDUCATION I U S DEPARTMENT OF HEALTH. EDUCATION & WELFARE OFFICE OF EDUCATION THIS DOCUMENT HAS BEEN REPRO OUCH) EXACTLY AS RECEIVED FROM THE PERSON OR ORGANIZATION ORIG INATING IT POINTS OF VIEW OR OPIN 'IONS STATED 00 NOT NECESSARILY REPRESENT OFFICIAL OFFICE OF EOU CATION POSITION OR POLICY AIR FORCE JUNIOR ROTC MR,UNIVERS17/14AXWELL MR FORCEBASE, ALABAMA Aerospace Education I Aircraft of Today D. S. Sayler Academic Publications Division 3825th Support Group (Academic) AIR FORCE JUNIOR ROTC AIR UNIVERSITY MAXWELL AIR FORCE BASE, ALABAMA 2 1971 Thispublication has been reviewed and approvedby competent personnel of the preparing command in accordance with current directiveson doctrine, policy, essentiality, propriety, and quality. -
Congress and the Supersonic Transport, 1960-1971 by John
Congress and the supersonic transport, 1960-1971 by John Marion Bell A thesis submitted in partial fulfillment of the requirements for the degree of MASTER OF ARTS in History Montana State University © Copyright by John Marion Bell (1974) Abstract: Aviation state-of-the-art advances in the 1940's and 1950's paved the way for development of a commercial SST in the 1960's. Military aviation advances were translated directly into subsonic transports and it was felt that the next step in progress would be the SST. Through military programs and basic research by NACA, the United States government aided the development of a commercial SST even before undertaking an active SST program in the 1960's. Foreign governments were also at work on SST's and when the British and French merged their development programs in 1962 the United States was spurred by their competition. President Kennedy announced an active program in June, 1963 a day following Pan Am's order of Anglo-French SST's. There was little opposition to the airplane at first; what little there was was based on the aircraft's unavoidable sonic boom. A design competition was conducted by the FAA to select the best possible American design. Boeing was selected the winner in 1966 on the basis of a radical, swing-wing design. The program then entered a two-prototype development stage. Boeing soon ran into development problems and in 1968 abandoned its swing-wing in favor of a conventional fixed-wing. The airplane's problems were also complicated by the great increase in cost of development as well as a growing opposition based on the possible negative environmental impact of the SST. -
On the Ballistic Wave from Projectiles and Vehicles of Simple Geometry Jean Varnier, Marie-Claire Le Pape, Frédéric Sourgen
On the ballistic wave from projectiles and vehicles of simple geometry Jean Varnier, Marie-Claire Le Pape, Frédéric Sourgen To cite this version: Jean Varnier, Marie-Claire Le Pape, Frédéric Sourgen. On the ballistic wave from projectiles and vehicles of simple geometry. AIAA Journal, American Institute of Aeronautics and Astronautics, 2018, 56 (7), pp.2725-2742. 10.2514/1.J056239. hal-01852518 HAL Id: hal-01852518 https://hal.archives-ouvertes.fr/hal-01852518 Submitted on 1 Aug 2018 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. On the ballistic wave from projectiles and vehicles of simple geometry Jean Varnier*, Marie-Claire Le Pape° ONERA, 92320 Châtillon, France Frédéric Sourgen°° ONERA, 31400 Toulouse, France The ballistic wave is a shock wave generated by a solid body moving at supersonic speed in the atmosphere. It sounds like the crack of a whip for small projectiles, like a detonation (sonic boom) for large-sized objects. Their common signature is a N-shaped pressure profile, the formalism of which is well-known but presents a practical difficulty, namely the calculation of the “shape factor” which characterizes the aerodynamic behavior of the object flying at supersonic speed. -
Examining Explanations for the Strange Phenomena Encountered by U.S
AIRCRAFT DESIGN 14 LUNAR SPACESUITS 18 SUPERSONICS 36 Perlan 2 glider — explained More fl exibility for astronauts Listening for X-59’s sonic thump Mystery sightings Examining explanations for the strange phenomena encountered by U.S. Navy pilots. PAGE 26 NOVEMBER 2019 | A publication of the American Institute of Aeronautics and Astronautics | aerospaceamerica.aiaa.org The Premier Global, Commercial, Civil, Military and Emergent Space Conference Where Ideas Launch • Connections Are Made • Business Gets Done! SpaceSymposium.org SAVE $600 – Register Today for Best Savings! Special Military Rates! +1.800.691.4000 Share: FEATURES | November 2019 MORE AT aerospaceamerica.aiaa.org The Premier Global, Commercial, Civil, Military and Emergent Space Conference 14 18 36 26 Aiming for Exploring the Planning for 90,000 feet moon in new the sound of Mystery phenomena spacesuits Designers of Perlan 2 supersonic fl ight We look at possible explanations for those overcame formidable Former astronaut How NASA’s Low Boom fast and agile objects zipping across F/A-18 engineering Tom Jones examines Flight Demonstrator screens. challenges to NASA’s plans to give will test the public’s create a glider that explorers suits that tolerance for sonic By Jan Tegler and Cat Hofacker has reached the will let them walk, thumps. stratosphere and will lope, crouch and even try to beat its own kneel. By Jan Tegler record next year. Where Ideas Launch • Connections Are Made • Business Gets Done! By Tom Jones By Keith Button SpaceSymposium.org SAVE $600 – Register Today for -
After Concorde, Who Will Manage to Revive Civilian Supersonic Aviation?
After Concorde, who will manage to revive civilian supersonic aviation? By François Sfarti and Sebastien Plessis December 2019 Commercial aircraft are flying at the same speed as 60 years ago. Since Concorde, which made possible to fly from Paris to New York in only 3h30, no civilian airplane has broken the sound barrier. The loudness of the sonic boom was a major technological lock to Concorde success, but 50 years after its first flight, an on-going project led by NASA is about to make supersonic flights over land possible. If successful, it will significantly increase the number of supersonic routes and increase the supersonic aircraft market size substantially. This technological improvement combined with R&D efforts on operational costs and a much larger addressable market than when Concorde flew may revive civilian supersonic aviation in the coming years. Who are the new players at the forefront and the early movers? What are the current investments in this field? What are the key success drivers and remaining technological and regulatory locks to revive supersonic aviation? EXECUTIVE SUMMARY Commercial aircraft are typically flying between 800 km/h and 900 km/h, which is between 75% and 85% of the speed of sound. It is the same speed as 60 years ago and since Concorde, which flew at twice the speed of sound, was retired in 2003, there has been no civilian supersonic aircraft in service. Due to a prohibition to fly supersonic over land and large operational costs, Concorde did not reach commercial success. Even if operational costs would remain larger than subsonic flights, current market environment seems much more favourable: since Concorde was retired in 2003, the air traffic has more than doubled and the willingness to pay can be supported by an increase in the number of high net worth individuals and the fact that business travellers value higher speed levels. -
S U Personics + Clim a Te
MOON LANDING 36 HYPERSONICS 14 SPACE ECONOMY 30 What Apollo can teach Artemis Predicting overheating A new role for space-faring governments ICS + ON CL RS IM E A P T U E S Mach 1 passenger jets could exacerbate aviation’s carbon footprint. The search for solutions is underway. PAGE 22 REPORTER’S PICKS PAGE 18 Your IAC preview OCTOBER 2019 | A publication of the American Institute of Aeronautics and Astronautics | aerospaceamerica.aiaa.org SECURE YOUR AIAA CORPORATE MEMBERSHIP TODAY! Take advantage of being a Corporate Member: › Industry recognition › Transformative conversations › Automatically elevate your staff to AIAA Senior Members › Annual forum registration allotment and discounted registrations › Recruit students and young professionals at Meet the Employer events › Plus so much more! LEARN MORE: aiaa.org/corporatemembership CONTACT US TO TODAY TO LEARN WHAT AIAA CAN DO FOR YOU! Chris Semon • Vickie Singer • Paul doCarmo 703.264.7510 | [email protected] FEATURES | October 2019 MORE AT aerospaceamerica.aiaa.org 18 30 36 22 IAC preview Seismic shift in Apollo’s lessons satellite market for Artemis Supersonic transports Our staff reporter describes the Space-faring Experience gleaned International and climate change governments are during the 20th- Astronautical taking a new role century moon program The industry has creative ideas for Congress events she in the satellite can help sustain addressing the warming infl uence of doesn’t want to miss. market as startups today’s momentum proposed Mach 1 passenger jets. and established toward a 2024 lunar By Cat Hofacker companies vie for landing. By Adam Hadhazy investors. By John M. Logsdon By Debra Werner On the cover: Photo illustration aerospaceamerica.aiaa.org | OCTOBER 2019 | 1 RENO, NEVADA 15–19 June 2020 | Reno-Sparks Convention Center CALL FOR PAPERS The AIAA AVIATION Forum is the only global event that covers the entire integrated spectrum of aviation business, research, development, and technology. -
Aviation Week & Space Technology
STARTS AFTER PAGE 34 MRO’s Bumpy Path Rolls Speeds Back to Recovery to Supersonics ™ $14.95 AUGUST 17-30, 2020 ADVANCING AIR MOBILITY Digital Edition Copyright Notice The content contained in this digital edition (“Digital Material”), as well as its selection and arrangement, is owned by Informa. and its affiliated companies, licensors, and suppliers, and is protected by their respective copyright, trademark and other proprietary rights. Upon payment of the subscription price, if applicable, you are hereby authorized to view, download, copy, and print Digital Material solely for your own personal, non-commercial use, provided that by doing any of the foregoing, you acknowledge that (i) you do not and will not acquire any ownership rights of any kind in the Digital Material or any portion thereof, (ii) you must preserve all copyright and other proprietary notices included in any downloaded Digital Material, and (iii) you must comply in all respects with the use restrictions set forth below and in the Informa Privacy Policy and the Informa Terms of Use (the “Use Restrictions”), each of which is hereby incorporated by reference. Any use not in accordance with, and any failure to comply fully with, the Use Restrictions is expressly prohibited by law, and may result in severe civil and criminal penalties. Violators will be prosecuted to the maximum possible extent. You may not modify, publish, license, transmit (including by way of email, facsimile or other electronic means), transfer, sell, reproduce (including by copying or posting on any network computer), create derivative works from, display, store, or in any way exploit, broadcast, disseminate or distribute, in any format or media of any kind, any of the Digital Material, in whole or in part, without the express prior written consent of Informa.