DOCSLIB.ORG

Space Chronicle General Issue

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Space Chronicle General Issue ISSN 0007-084X Space Chronicle General Issue Journal of the British Interplanetary Society Vol. 66, Suppl. 2, 2013 JBIS Publication Date: 19 November 2013 Space Chronicle: JBIS Supplement Space Chronicle issues are published as a part of JBIS, but as Supplements to preserve the continuity of the regular series of JBIS (blue cover) issues. Editor: John Becklake Space Chronicle welcomes the submission Production Assistant: B. Jones for publication of technical articles of general Promotion: S. Parry interest, historical contributions and reviews Space Chronicle Office: 27/29 South Lambeth Road, London, SW8 in space science and technology, astronautics 1SZ, England. and related fields. Tel: 020 7735 3160 Text should be: Fax: 020 7587 5118 Email: [email protected] 1. As concise as the content allows; www.bis-space.com 2. Submitted in both electronic form(*) and hardcopy; * * * * Text can be accepted in Word for Windows up to Version Word Space Chronicle is a publication which promotes the objectives of 2007. the British Interplanetary Society. Opinions expressed in signed Illustrations should be either: articles are those of the contributors and do not necessarily reflect the views of the Editor or the Council of the British Interplanetary 1. Photographic prints, line drawings or 35 mm slides. (Not Society. Security clearance, where necessary, is the responsibility transparencies); or of the author. 2. High resolution (Photos - 300 dpi and Line drawings - 600 * * * dpi) electronic images on disk/email in either jpg or tiff format. Space Chronicle is distributed worldwide by mail and may be received by annual subscription or purchase of single copies. It More detailed information and a License to Publish can be is available through membership of the British Interplanetary obtained from www.bis-space.com/publications or by contacting Society at much reduced rates. the Space Chronicle office. * * * Material for publication including a signed License to Publish should be sent to: Published by the British Interplanetary Society, 27/29 South Lambeth Road, London, SW8 1SZ, England. Registered Company Space Chronicle No: 402498. Registered Charity No: 250556. Printed by Latimer The British Interplanetary Society Trend & Company Ltd, Estover Road, Plymouth, PL6 7PY, England. 27/29 South Lambeth Road London * * * SW8 1SZ Copyright © British Interplanetary Society 2013. No part of this UK magazine may be reproduced or transmitted in any form or by or via email to [email protected] any means, electronic or mechanical, including photocopying or recording by any information storage or retrieval system without Authors will receive a complimentary copy of the issue in which prior permission from the Publishers. their paper appears. Journal of the British JBIS Interplanetary Society The July/August 2013 issue of the Journal of the British Interplanetary Society is now available and contains the following papers: Review, Analyses, and Recommendations Related to Modern International use of Nuclear Space Technologies with Focus on United States and Russia Science Fiction and the Big Questions Interstellar Flight, Imagination and Myth Creation as an Effective Means for Enduring Inspiration Interstellar Colonization and Multi-Generation Spaceships: Getting There is Half the Fun Utilizing Video Games The Interstellar Vision: Principles and Practice Comparison of Historic Exploration with Contemporary Space Policy Suggests a Retheorisation of Settings Warp Field Mechanics 101 Project Icarus: A Review of the Daedalus Main Propulsion System Evolutionary Lightsailing Missions for the 100-Year Starship Copies of JBIS, priced at £15 for members, £40 to non-members, P&P: UK £1.50, Europe £3.50, Rest of the World £3.50 Back issues are also available and can be obtained from The British Interplanetary Society, 27/29 South Lambeth Road, London, SW8 1SZ, England Published By The British Interplanetary Society Space Chronicle Journal of the British Vol. 66, Suppl. 2, 2013 JBIS Interplanetary Society LIST OF CONTENTS 46 Mystery WW2 German Liquid Rocket Engine Martin Postranecky 49 Walterwerke KG Shamus Reddin 65 The Nuclear Possibility: History, Current Status and Future Prospects Anders Hansson 77 The Ariane 5 from a Technical Point of View: The Ariane 5 ECA Versus its Early 5G Version Lieven Roesems * * * Front Cover: (upper left) Artist’s concept of the Jupiter Icy Moons Orbiter (JIMO). (lower left) Walter U-Boat V80 on trial in the Schlei inlet. (right) Cut open view of an Ariane 5G. The payload pictured is that of Ariane 502, launched on 30 October 1997. The payload was stacked using a SPELTRA payload adapter. 45 MartinSpace Chronicle: Postranecky JBIS, Vol. 66, pp.46-48, 2013 Mystery WW2 German Liquid Rocket Engine MARTIN POSTRANECKY, FBIS Email: [email protected] In the eastern corner of Moravia in the Czech Republic, near the border with Slovakia, there is a little known private military museum based in the former Czechoslovak Army Base Sokolov outside the town Slavicin. This “Army Park Slavicin” [1], founded in 2006, aims to build up a museum of military vehicles, arms and equipment of the former Czechoslovak People’s Army. It also includes collections (unfortunately incomplete) of various products of nearby munitions factories during and after the Second World War The museum contains an unique collection of military rockets and missiles, including vehicles and launchers, mainly of Soviet and Czech manufacture from the 1960’s onwards. Also included are various training aids, sectioned rocket motors, etc [2]. Among this cornucopia of modern military rocketry there stands an obviously old, sad, strange, sectioned rocket motor with an inconspicuous, hand-written note stuck on with sellotape, which just says - in Czech - “Nemecka Pokusna PL Raketa” (“German Test AA Rocket” in English) [3]. When we visited this museum in the spring of 2013 (and you may need to make a prior appointment by telephone or email, as this place is normally open to public only on Sundays during the summer months - apart from special events), the guide had no idea what this engine was, and where it came from. He said that, as far as he knew, it was donated to the collection by somebody who “worked in the military/explosives industry” and didn’t wish Fig. 1 Test AA Rocket Engine. (Martin Postranecky) to see it “thrown on the scrap heap after his retirement...” A quick search through some old reference material, Our question is - what engine is it, and how it came to be and discussions with friends and colleagues, produced few there? possible answers: from the size and shape it could be the VfK Zg.613-A/-A01 engine, as designed for the Rheinmetall-Borsig There doesn’t appear to be much to go on to try and identify Rheintochter R3(F) anti-aircraft rocket - this engine was also this rocket motor (Fig. 1). It is obviously a small (Fig. 2), ~2ft/60cm used for tests of the experimental Messerschmitt Enzian E-3, tall, liquid-bi-fuel rocket engine, with double-walled chamber E-4 and E-5 test articles [5, 6]. construction for cooling, and with multiple (oxidiser?) injectors in four staggered rows (Fig. 3), one central-threaded (fuel?) It was designed by Dr. Helmuth Konrad (Conrad?) of the injector bushing (no injector present), and an almost cylindrical Berlin Technische Hochschule, working for the “Deutsche chamber - very unlike the usual spherical A-4 shape chamber. Versuchsanstalt fur Kraftfahrzeuge und Fahrzeuge Motoren” (DVK), in 1944 and built and flown in 1945 [5, 6, 7]. There were not many German liquid-bi-fuel anti-aircraft rockets made during the WW2, and the size is the limiting factor. It used Salbei (92% HNO3 + 8% H2SO4) as oxidiser and Visol (Vinyl Isobutyl Ether) as fuel, pressurised by compressed air. It looks almost as a small-scale version of the EMW There is a Rheintochter R3 engine at RAF Cosford Museum [8, Wasserfall engine [4], but not as spherical. 9] which, if accessible, will be examined for comparison. 46 Mystery WW2 German Liquid Rocket Engine Fig. 2 Some of the SAM rocket engines displayed at the Army Park Slavicin. From left; engine of S-200 ‘Vega’ Soviet large SAM missile, the unknown mystery German liquid engine, a sectioned engine from S-75 ‘Volchov’ SAM missile and a nozzle from a solid booster of the S-200 ‘Vega’. (Mgr. Jirka Kroulik) 47 Martin Postranecky universities, aimed at designing improved injectors and mixers for large A-4 type liquid-fuel rocket engines, with articles being tested at Kummersdorf and Peenemunde. Could this be one of these test engines? But without detailed research in German archives, this would be impossible to prove. Also, the paper label does seem to point to an AA rocket. So, let us say that it could well be the Konrad VfK Zg.613-A engine - unless somebody can show us a better fit! And, finally, how did this (sectioned) engine came to be in this remote Moravian museum? Fig. 3 Enlargement of (oxidiser?) injectors. Note the difference It is known that a manufacture of the A-4/V-2 engines was between rows 1, 2, 3 and 4. (Martin Postranecky) being prepared in the (pro-German) Slovakian armament Few other options mentioned were the experimental Dr. factory in Dubnice nad Vahem (then part of “Hermann Goring Konrad DVK SG20 engine for the Rheinmetall-Borsig Feuerlilie Waffenwerke A.G.”) in 1945 [14]. Is it just possible that there F55 tests [10] - probably too small, or the Walter HWK 109-739 were plans to manufacture other rocket parts there...? original engine for Enzian [11] - the wrong shape, or the BMW 109-558 engine for the Henschel Hs-117 Schmetterling rocket But the most likely explanation is that this engine found [12] - too small & the wrong shape. its way, after the war - possibly via the Soviet Union - to some military or technical research establishment in the A completely different suggestion was made by my Czech Czechoslovak Republic where it was used for research or friend Mgr.
Load more

Recommended publications
  • The Argonauta
    ARGONAUTA The Newsletter of The Canadian Nautical Research Society / Société canadienne pour la recherche nautique Volume XXXVI Number 2 Spring 2019 ARGONAUTA Founded 1984 by Kenneth MacKenzie ISSN No. 2291-5427 Editors Isabel Campbell and Colleen McKee Winston (Kip) Scoville ~ Production/Distribution Manager Argonauta Editorial Office e-mail submissions to: [email protected] or [email protected] ARGONAUTA is published four times a year—Winter, Spring, Summer and Autumn Chair of the Editorial Board: Roger Sarty Editor The Northern Mariner/ William Glover Le marin du nord: Webmaster: Paul Adamthwaite Executive Officers President: Richard Gimblett 1st Vice President: Walter Lewis 2nd Vice President: Faye Kert Treasurer: Errolyn Humphreys Secretary: Michael Moir Membership Secretary: Sam McLean Councillor/Communications: Kip Scoville Councillor: Richard Goette Councillor: Tom Malcomson Councillor: David More Councillor: Jeff Noakes Councillor: Margaret Schotte Councillor: Ian Yeates Membership Business: P.O. Box 34029 Station B, Ottawa, Ontario, K2J 4B1, Canada e-mail: [email protected] Annual Membership including four issues of ARGONAUTA and four issues of THE NORTHERN MARINER/LE MARIN DU NORD: Canadian International Digital Only Individual $70 $80 $30 Benefactor $250 Institutional $95 $105 n/a Corporate $500 Student $35 $35 $35 Patron $1000 or above NASOH n/a n/a $30 Our Website: http://www.cnrs-scrn.org Copyright © CNRS/SCRN and all original copyright holders In this issue of the Argonauta Editorial 1 President’s Corner
    [Show full text]
  • AIR-INDEPENDENT PROPULSION – AIP Technology Creates a New Undersea Threat Page 1 of 6
    AIR-INDEPENDENT PROPULSION – AIP Technology Creates a New Undersea Threat Page 1 of 6 AIR-INDEPENDENT PROPULSION AIP Technology Creates a New Undersea Threat Walter Type XVIIB up on the stocks. Pictured above is the German Walter Type XVIIB U-1406, partially dismantled shortly after the end of World War II. U-1406 was turned over to the U.S. Navy as a war prize and soon disposed of, but the Royal Navy later operated her sister ship, U-1407, as HMS Meteorite to gain experience in hydrogen-peroxide propulsion technologies. As interest mounts in "Air-Independent Propulsion" (AIP) for enhancing the performance of small, defensive submarines, a serious new underwater threat is developing in littoral waters. Increasingly, smaller nations unwilling or unable to accept the high cost of nuclear power to achieve greater underwater endurance and longer range are turning to lower-priced and less ambitious alternatives that still offer significant operational advantages over conventional diesel- electric submarines. The best of the latter boats, such as the German-designed Type 209 or the Russian KILO, can remain submerged on battery at slow speed for periods on the order of three to five days. But now, several AIP schemes in development or already in operation can increase slow-speed endurance to as much as three weeks or a month. While still dwarfed by the potential of nuclear power, AIP offers diesel submarines a remarkable increase in capability. AIP - The Early History Despite their initial successes, submarine pioneers were still eager to find some means to free their boats from the necessity of surfacing frequently for access to the atmospheric oxygen demanded by the gasoline or diesel engines that charged the batteries.
    [Show full text]
  • Trade Studies Towards an Australian Indigenous Space Launch System
    TRADE STUDIES TOWARDS AN AUSTRALIAN INDIGENOUS SPACE LAUNCH SYSTEM A thesis submitted for the degree of Master of Engineering by Gordon P. Briggs B.Sc. (Hons), M.Sc. (Astron) School of Engineering and Information Technology, University College, University of New South Wales, Australian Defence Force Academy January 2010 Abstract During the project Apollo moon landings of the mid 1970s the United States of America was the pre-eminent space faring nation followed closely by only the USSR. Since that time many other nations have realised the potential of spaceflight not only for immediate financial gain in areas such as communications and earth observation but also in the strategic areas of scientific discovery, industrial development and national prestige. Australia on the other hand has resolutely refused to participate by instituting its own space program. Successive Australian governments have preferred to obtain any required space hardware or services by purchasing off-the-shelf from foreign suppliers. This policy or attitude is a matter of frustration to those sections of the Australian technical community who believe that the nation should be participating in space technology. In particular the provision of an indigenous launch vehicle that would guarantee the nation independent access to the space frontier. It would therefore appear that any launch vehicle development in Australia will be left to non- government organisations to at least define the requirements for such a vehicle and to initiate development of long-lead items for such a project. It is therefore the aim of this thesis to attempt to define some of the requirements for a nascent Australian indigenous launch vehicle system.
    [Show full text]
  • H2O2) Is Commonly Used for Cleaning Cuts and Sores, and That a Bottle of Hydrogen Peroxide Can Turn a Brunette Into a Blonde
    Hydrogen Peroxide and Sugar Most people know that Hydrogen Peroxide (H2O2) is commonly used for cleaning cuts and sores, and that a bottle of hydrogen peroxide can turn a brunette into a blonde. Yet, how many people know that hydrogen peroxide can also be used as a powerful rocket fuel? And how many people know that hydrogen peroxide accelerated the jet car Peroxide Thunder to 450 mph in 3.4 seconds? Hydrogen peroxide is commonly used (in very low concentrations, typically around 5%) to bleach human hair, hence the phrases "peroxide blonde" and "bottle blonde". It burns the skin upon contact in sufficient concentration. In lower concentrations (3%), it is used medically for cleaning wounds and removing dead tissue. Combined with urea as carbamide peroxide, it is used for whitening teeth. Hydrogen peroxide tends to decompose exothermically into water and oxygen gas. The rate of decomposition is dependent on the temperature and concentration of the peroxide, as well as the presence of impurities and stabilizers. The use of a catalyst (such as manganese dioxide, silver, or the enzyme catalase) vastly increases the rate of decomposition of hydrogen peroxide. High strength peroxide (also called high-test peroxide, or HTP) must be stored in a vented container to prevent the buildup of pressure leading to the eventual rupture of the container. In the 1930s and 40s, Hellmuth Walter pioneered methods of harnessing the rapid decomposition of hydrogen peroxide in gas turbines and rocket engines. Hydrogen peroxide works best as a propellant in extremely high concentrations of 90% or higher. Hydrogen peroxide - Wikipedia Online Encyclopedia Hydrogen peroxide (H2O2) can store energy in the form of chemical energy, similar to hydrogen.
    [Show full text]
  • Hydrazine 1 Hydrazine
    Hydrazine 1 Hydrazine Hydrazine Identifiers [1] CAS number 302-01-2 , 7803-57-8 (hydrate) [2] EC number 206-114-9 UN number 2029 (anhydrous) 2030 (aq. soln., 37–64%) 3293 (aq. soln., <37%) RTECS number MU7175000 Properties Molecular formula N H 2 4 Molar mass 32.05 g/mol (anhydrous) 50.06 g/mol (hydrate) Appearance Colourless liquid Density 1.0045 g/cm3 (anhydrous) 1.032 g/cm3 (hydrate) Melting point 1 °C (274 K, anhydrous) -51.7 °C (hydrate) Boiling point 114 °C (387 K), anhydrous 119 °C (hydrate) Solubility in water miscible Acidity (pK ) 8.1 a Refractive index (n ) [3] D 1.46044 (22 °C, anhydrous) 1.4284 (hydrate) Viscosity 0.876 cP (25 °C) Structure Hydrazine 2 Molecular shape pyramidal at N [4] Dipole moment 1.85 D Hazards [5] MSDS ICSC 0281 EU Index 007-008-00-3 EU classification Carc. Cat. 2 Toxic (T) Corrosive (C) Dangerous for the environment (N) R-phrases R45, R10, R23/24/25, R34, R43, R50/53 S-phrases S53, S45, S60, S61 NFPA 704 Flash point 52 °C Autoignition 24–270 °C (see text) temperature Explosive limits 1.8–100% LD [6] 50 59–60 mg/kg (oral in rats, mice) Related compounds Related nitrogen hydrides Ammonia Hydrazoic acid Related compounds monomethylhydrazine dimethylhydrazine phenylhydrazine [7] (what is this?) (verify) Except where noted otherwise, data are given for materials in their standard state (at 25 °C, 100 kPa) Infobox references Hydrazine is an inorganic chemical compound with the formula N H . It is a colourless liquid with an 2 4 ammonia-like odor and is derived from the same industrial chemistry processes that manufacture ammonia.
    [Show full text]
  • Military & Maritime Catalog
    SCHIFFER P U B L I S H I N G Military & Maritime Catalog AUTUMN/WINTER 2014 aviation: 18 naval: 43 ground forces: 45 militaria: 61 modeling & collectible figures: 76 American Civil War: 78 Cornell Maritime Press: 79 pin-ups: 86 transportation: 88 2 NEW BOOKS MARTIN B-26 MARAUDER: The Ultimate Look: From Drawing William Wolf Board to Widow Maker Vindicated • Fifth in the Ultimate Look bomber series • Photo coverage of the NMUSAF and MAPS restored B-26s • 20 color profiles of some of the most notable of the B-26 series In his fifth book in The Ultimate Look series, Dr. Wolf again brings the same degree of meticulous research to describe this unappreciated and misunderstood B-26 medium bomber. This massive, comprehensive volume is the first to give the reader a definitive description of this neglected bomber, its development, testing, and manufacture. The role of the enigmatic aviation icon Glenn L. Martin is described in the development of the American aviation industry and the Marauder. The author made extensive use of the massive document and photo collections of the Marauder Archives at Akron and Tucson, and the Air Force collection at the NMUSAF. Martin Company design and production information and flight and test evaluations, along with original Company Flight, Parts, and Maintenance Manuals, and rare archival microfilm of original material were also used. The author was given unprecedented access to the family records of B-26 designer Peyton Magruder. The text is complemented by archival photos and drawings, and new color photos of the Marauders at the NMUSAF, Fantasy of Flight, and MAPS Museum.
    [Show full text]
  • A Performance Diagnosis of the 1939 Heinkel He S3B Turbojet
    Proceedings of ASME Turbo Expo 2004 Power for Land, Sea, and Air June 14-17, 2004, Vienna, Austria GT2004-53014 A Performance Diagnosis of the 1939 Heinkel He S3B Turbojet. C Rodgers FASME [email protected] ABSTRACT. The historical development of the world’s first pure SFC Specific fuel Consumption jet propelled aircraft, the Heinkel He 178, and its T Temperature turbojet the He S3B has been extensively TIT Turbine Inlet Temperature documented, however only limited descriptions of U Tip Speed the engine and component aero-thermo-dynamic V0 Turbine Spouting Velocity = √√√2g Had performances have, as yet, been published in open Va Turbine exit axial velocity English literature. W Airflow, or relative velocity The basic He S3B engine flowpath configuration of a ∆∆∆ Difference radial compressor mounted back-to-back with a ηηη Efficiency radial inflow turbine, intrigued the author as one ωωω Angular Velocity excellent example of the pre WW11 radial turbomachinery ingenuity and expertise, to the Subscripts extent that it prompted this diagnosis. ad Adiabatic Recognizing that some of the historically quoted c Compressor HeS3B performance data may be dubious, attempts d Diffuser have been made to coalesce data from multiple crit Sonic conditions sources into a more consistent account by i Inlet conducting a detailed engine performance analysis. n Nozzle HeS3B engine performance characteristics are re- s Static created based upon predicted meanline component t Turbine, or total maps derived from engine drawings and supporting Note all angles relative to the axial plane data recently published by AIAA in his biography “Dr Hans von Ohain -Excellence in Flight”.
    [Show full text]
  • Up from Kitty Hawk Chronology
    airforcemag.com Up From Kitty Hawk Chronology AIR FORCE Magazine's Aerospace Chronology Up From Kitty Hawk PART ONE PART TWO 1903-1979 1980-present 1 airforcemag.com Up From Kitty Hawk Chronology Up From Kitty Hawk 1903-1919 Wright brothers at Kill Devil Hill, N.C., 1903. Articles noted throughout the chronology provide additional historical information. They are hyperlinked to Air Force Magazine's online archive. 1903 March 23, 1903. First Wright brothers’ airplane patent, based on their 1902 glider, is filed in America. Aug. 8, 1903. The Langley gasoline engine model airplane is successfully launched from a catapult on a houseboat. Dec. 8, 1903. Second and last trial of the Langley airplane, piloted by Charles M. Manly, is wrecked in launching from a houseboat on the Potomac River in Washington, D.C. Dec. 17, 1903. At Kill Devil Hill near Kitty Hawk, N.C., Orville Wright flies for about 12 seconds over a distance of 120 feet, achieving the world’s first manned, powered, sustained, and controlled flight in a heavier-than-air machine. The Wright brothers made four flights that day. On the last, Wilbur Wright flew for 59 seconds over a distance of 852 feet. (Three days earlier, Wilbur Wright had attempted the first powered flight, managing to cover 105 feet in 3.5 seconds, but he could not sustain or control the flight and crashed.) Dawn at Kill Devil Jewel of the Air 1905 Jan. 18, 1905. The Wright brothers open negotiations with the US government to build an airplane for the Army, but nothing comes of this first meeting.
    [Show full text]
  • Archie to SAM a Short Operational History of Ground-Based Air Defense
    Archie to SAM A Short Operational History of Ground-Based Air Defense Second Edition KENNETH P. WERRELL Air University Press Maxwell Air Force Base, Alabama August 2005 Air University Library Cataloging Data Werrell, Kenneth P. Archie to SAM : a short operational history of ground-based air defense / Kenneth P. Werrell.—2nd ed. —p. ; cm. Rev. ed. of: Archie, flak, AAA, and SAM : a short operational history of ground- based air defense, 1988. With a new preface. Includes bibliographical references and index. ISBN 1-58566-136-8 1. Air defenses—History. 2. Anti-aircraft guns—History. 3. Anti-aircraft missiles— History. I. Title. 358.4/145—dc22 Disclaimer Opinions, conclusions, and recommendations expressed or implied within are solely those of the author and do not necessarily represent the views of Air University, the United States Air Force, the Department of Defense, or any other US government agency. Cleared for public re- lease: distribution unlimited. Air University Press 131 West Shumacher Avenue Maxwell AFB AL 36112-6615 http://aupress.maxwell.af.mil ii In memory of Michael Lewis Hyde Born 14 May 1938 Graduated USAF Academy 8 June 1960 Killed in action 8 December 1966 A Patriot, A Classmate, A Friend THIS PAGE INTENTIONALLY LEFT BLANK Contents Chapter Page DISCLAIMER . ii DEDICATION . iii FOREWORD . xiii ABOUT THE AUTHOR . xv PREFACE TO THE SECOND EDITION . xvii PREFACE TO THE FIRST EDITION . xix ACKNOWLEDGMENTS . xxi 1 ANTIAIRCRAFT DEFENSE THROUGH WORLD WAR II . 1 British Antiaircraft Artillery . 4 The V-1 Campaign . 13 American Antiaircraft Artillery . 22 German Flak . 24 Allied Countermeasures . 42 Fratricide . 46 The US Navy in the Pacific .
    [Show full text]
  • Inhaltsverzeichnis
    Inhaltsverzeichnis Zur Gecchichte das Flugzeugs 7 7 Transavia PI-12 „Airtruk'7PL-12 U „Flying CHINA Mango" 36/570 1. Die Nachahmung des Vogelflugs 77 Harbin C-11 57/572 „Jie-Fang" 57/572 2. Die Vorbilder Nanchang F-6bis 58/572 für den Flug des Menschen 12 BELGIEN „Peking-1" 58/572 3. Die ersten Motorflugzeugprojekte 12 Avions Fairey „Tipsy Nipper" 37/570 4. Die Verwirklichung des Gleitflugs- SABCAS-2 37/570 Voraussetzung für den Motorflug 14 Stampe et Renard SV-4 C 38/570 CSSR 6. Der erste Motorflug der Brüder Wright 75 Aero Ae-02 59/572 6. Die ersten Motorflüge in Europa AeroA-42 59/572 und die Entwicklung der Luftfahrttechnik BRASILIEN Aero 145 60/572 bis zum Jahre 1914 76 AviaBH-3 60/572 7. Der erste Weltkrieg EMBRAER EMB-110 „Bandeirante" 39/570 Avia B-534 67/572 und die Luftfahrttechnik 17 EMBRAER EMB-200/201 „Ipanema" 39/570 AviaB-135 67/572 ITA „Urupema" 40/570 HC-2 „Heli Baby'7HC-102 62/572 8. Der Aufschwung der Luftfahrttechnik Neiva 360 C „Regente"/„Regenta Elo'7 L-13„Blanik" 63/572 in den Jahren 1919 bis 1939 19 „Lanceiro" 40/570 L-60 „Brigadyr" 63/572 8.1. Bauweisen 19 Neiva Paulistinha 56-C/56-D 47/570 L-40 „Meta Sokol" 64/572 8.2. Triebwerke 20 Neiva N-621 „Universal"/T-25 47/570 L-200 „Morava" 64/572 8.3. Aerodynamik 21 L-29 „Delfin" 65/572 8.4. Geschwindigkeiten 22 L-39 „Albatros" 65/572 8.5. Das Verkehrsflugzeug 24 L-410 „Turbolet" 66/572 8.6.
    [Show full text]
  • The World's First True Rocket Aircraft
    VDI DGLR Verein Deutscher Ingenieure Deutsche Gesellschaft Hamburger Bezirksverein e.V. ROYAL AERONAUTICAL SOCIETY für Luft- und Raumfahrt Arbeitskreis Luft- und Raumfahrt Lilienthal-Oberth e.V. HAMBURG BRANCH E.V. Invitation to an RAeS lecture in cooperation with the DGLR and VDI The world’s first true rocket aircraft - the Heinkel He 176 Douglas Downer-Smith Lecture followed by discussion Date: Thursday, 1st October, 18:00 Location: HAW Hamburg Entry free ! Berliner Tor 5 No registration ! (Neubau), Hörsaal 01.12 Praxis Seminar Luftfahrt Germany 1939 - the Heinkel He 176 flew and was the first aircraft specifically designed for liquid fuel rocket propulsion. This was a true milestone of flight and just a few weeks before another milestone, the first flight of a turbojet aircraft – the Heinkel He 178. Both of these flights were made by the same pilot. Despite sparse archival evidence, how this aircraft came into existence against the backdrop of the rise of rocketry in pre-war Germany is covered, especially as regards relationships between those involved – Ernst Heinkel, the Luftwaffe and the pilot, Eric Warsitz. The probable performance of the aircraft is explored using animation and aircraft design software. Pre- war film of aircraft rocket propulsion experiments will be shown for comparison. Douglas Downer-Smith is an electronics engineer with a life-long interest in aviation. This has resulted in a special study of the jet and rocket aircraft of World War II. Researching some of the lesser known aircraft of this period is challenging yet rewarding and he is in contact with leading researchers in Germany and the USA.
    [Show full text]
  • 0106Engines.Pdf
    They approached the jet engine problem in different ways, but they both solved it. The Converging Paths of Whittle and von Ohain Pictured in 1987 is Frank Whittle and the Whittle W1X, the engine he designed. The engine is on display in the jet gallery at the National Air and Space Museum in Washington, D.C. 70 AIR FORCE Magazine / January 2006 They approached the jet engine problem in different ways, but they both solved it. o one who witnessed the first apprentice at the age of 16. His goal flight by a jet aircraft had any was to become a pilot. N idea of the revolution that the Hugh Trenchard, Marshal of the jet engine would bring. The secret flight Royal Air Force, made many important in Germany of the Heinkel He-178 contributions to the RAF, but none more on Aug. 27, 1939, led to revolutions so than his concept of apprentice train- in aviation, warfare, transportation, ing. Trenchard insisted that his enlisted politics, and the world economy. and noncommissioned personnel have The Converging Paths of A functioning jet engine was real- a sound education. Then he wanted ized at about the same time by two his average RAF airman to have three independent inventors, British Frank years’ training as an apprentice before Whittle and German Hans Pabst von entering service as a mechanic or other Ohain. They could not have differed skilled worker. more in personality. Trenchard believed that only educat- Whittle and von Ohain Whittle, an extremely proficient Royal ed and well-trained men could become Air Force pilot, was quick tempered professional airmen.
    [Show full text]