Bachem-Werke Ba 349 "Natter"
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Messerschmitt Me 262
Messerschmitt Me 262 The Messerschmitt Me 262 Schwalbe / Sturmvogel (English: "Swallow"/ "Storm Bird") of Nazi Germany was the world's first operational jet- powered fighter aircraft. Design work started before World War II began, but engine problems and top-level interference kept the aircraft from operational status with the Luftwaffe until mid-1944. Heavily armed, it was faster than any Allied fighter, including the British jet-powered Gloster Meteor.One of the most advanced aviation designs in operational use during World War II,the Me 262 was used in a variety of roles, including light bomber, reconnaissance, and even experimental night fighter versions. Me 262 pilots claimed a total of 542 Allied kills, although higher claims are sometimes made. The Allies countered its potential effectiveness in the air by attacking the aircraft on the ground and during takeoff and landing. Engine reliability problems, from the pioneering nature of its Junkers Jumo 004 axial- flow turbojetengines—the first ever placed in mass production—and attacks by Allied forces on fuel supplies during the deteriorating late-war situation also reduced the effectiveness of the aircraft as a fighting force. In the end, the Me 262 had a negligible impact on the course of the war as a result of its late introduction and the consequently small numbers put in operational service. While German use of the aircraft ended with the close of the Second World War, a small number were operated by the Czechoslovak Air Force until 1951. Captured Me 262s were studied and flight tested by the major powers, and ultimately influenced the designs of a number of post-war aircraft such as the North American F-86 Sabreand Boeing B-47 Stratojet. -
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. -
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. -
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. -
Part 2 — Aircraft Type Designators (Decode) Partie 2 — Indicatifs De Types D'aéronef (Décodage) Parte 2 — Designadores De Tipos De Aeronave (Descifrado) Часть 2
2-1 PART 2 — AIRCRAFT TYPE DESIGNATORS (DECODE) PARTIE 2 — INDICATIFS DE TYPES D'AÉRONEF (DÉCODAGE) PARTE 2 — DESIGNADORES DE TIPOS DE AERONAVE (DESCIFRADO) ЧАСТЬ 2. УСЛОВНЫЕ ОБОЗНАЧЕНИЯ ТИПОВ ВОЗДУШНЫХ СУДОВ ( ДЕКОДИРОВАНИЕ ) DESIGNATOR MANUFACTURER, MODEL DESCRIPTION WTC DESIGNATOR MANUFACTURER, MODEL DESCRIPTION WTC INDICATIF CONSTRUCTEUR, MODÈLE DESCRIPTION WTC INDICATIF CONSTRUCTEUR, MODÈLE DESCRIPTION WTC DESIGNADOR FABRICANTE, MODELO DESCRIPCIÓN WTC DESIGNADOR FABRICANTE, MODELO DESCRIPCIÓN WTC УСЛ . ИЗГОТОВИТЕЛЬ , МОДЕЛЬ ВОЗДУШНОГО WTC УСЛ . ИЗГОТОВИТЕЛЬ , МОДЕЛЬ ВОЗДУШНОГО WTC ОБОЗНАЧЕНИЕ ОБОЗНАЧЕНИЕ A1 DOUGLAS, Skyraider L1P M NORTH AMERICAN ROCKWELL, Quail CommanderL1P L DOUGLAS, AD Skyraider L1P M NORTH AMERICAN ROCKWELL, A-9 Sparrow L1P L DOUGLAS, EA-1 Skyraider L1P M Commander NORTH AMERICAN ROCKWELL, A-9 Quail CommanderL1P L A2RT KAZAN, Ansat 2RT H2T L NORTH AMERICAN ROCKWELL, Sparrow CommanderL1P L A3 DOUGLAS, TA-3 Skywarrior L2J M DOUGLAS, NRA-3 SkywarriorL2J M A10 FAIRCHILD (1), OA-10 Thunderbolt 2 L2J M DOUGLAS, A-3 Skywarrior L2J M FAIRCHILD (1), A-10 Thunderbolt 2L2J M FAIRCHILD (1), Thunderbolt 2L2J M DOUGLAS, ERA-3 SkywarriorL2J M AVIADESIGN, A-16 Sport Falcon L1P L DOUGLAS, Skywarrior L2J M A16 AEROPRACT, A-19 L1P L A3ST AIRBUS, Super Transporter L2J H A19 AIRBUS, Beluga L2J H A20 DOUGLAS, Havoc L2P M DOUGLAS, A-20 Havoc L2P M AIRBUS, A-300ST Super TransporterL2J H AEROPRACT, Solo L1P L AIRBUS, A-300ST Beluga L2J H A21 SATIC, Beluga L2J H AEROPRACT, A-21 Solo L1P L SATIC, Super Transporter L2J H A22 SADLER, Piranha -
Subject Reference Dbase 09-05-2006
Subject reference dbase 09-05-2006 ONDERWERP TYPE NUMMER BIJZ GROEP TREFWOORD1 TREFWOORD2 ELECTRON 1958.12 1958.12 ELEC Z 46 TEK CX GEVR L,KWANTONETC KUBEL TS-N KERST CX LW,KW,LO 0,5/1 KW LW SEND 2.39 As 33/A1 34 Z 101 100-1000 KHZ MOB+FEST MOBS 0,7/1,4 KW SEND AS 60 10.40 AS 60 Z 101 FRUEHE AUSF 3-24 MHZ MOB+FEST MOBS 1 KWTT KW SEND 11.37 S 521 Bs Z 101 =+/-G 1,5.... MOBS 1 KWTT SHORT WAVE TR 5.36 S 486F Z 101 3-7 UND 2,5-6 MHZ MOBS 1 kW KW SEND S 521Bs TELEFUNKEN Z 172 +/-G 1,2K MOBS G1,2K+/- 10 WTT TELEF SENDER 10.34 S 318H Z 101 1500-3333 KHZ GUSS GEH SCHS 100 WTT SEND S 317H TELEFUNKEN Z 172 RS 31g 100-800METER alt SCHS S317H 100 WTT SENDER 4.33 S 317 H Z 101 UNIVERS SENDER 377-3000KHZ MOBS 15 W EINK SEND EMPF 10.35 Stat 272 B Z 101 +/- 15 W SE 469 SE 5285 F1/37 TRSE 15 WTT KARREN STN 4.40 SE 469A Z 101 3-5 MHZ TRSE 15 WTT KW STN 10.35 Spez804/445 Z 101 S= 804Bs E= Spez 445dBg 3-7,5M TRSE 150 WTT LANGW SENDE ANL 8.39 Stat 1006aF Z 101 S 427F SA 429F FLFU 1898-1938 40 JAAR RADIO IN NED SWIERSTRA R. Z 143 INLEGVEL VAN SWIERSTA PRIVE'38 LI 40 RADIO!! WILHELMINA 1kW KW SEND S 486F TELEFUNKEN Z 172 +/-2,5-7,5MHZ MOBS S486 1,5 LW SEND S 366Bs 11.37 S 366Bs Z 101 =+/- G1,5...100-600 KHZ MOBS 1,5kW LW SEND S366Bs TELEFUNKEN Z 172 +/-G 1,5L MOBS S366Bs S366BS 20 WTT FL STN 3.35 Spez 378mF Z 101 TELEF D B FLFU 20 WTT FLUGZEUG STN Spez 378nF TELEFUNKEN Z 172 URALT ANL LW FEST FREQU FLFU Spez378nF Spez378NF 20 WTT MITTELWELL GER Stat901 TELEFUNKEN Z 172 500-1500KHZ Stat 901A/F FLFU 200 WTT KW SEND AS 1008 11.39 AS 1008 Z 101 2,5-10 MHZ A1,A2,A3,HELL -
Battletech Technical Readout: 3055 Upgrade
TM In 3055, a new breed of Inner Sphere BattleMech started rolling off assembling lines—’Mechs specifically designed to counter the Clan invasion—at the same time that second- line Clan ’Mechs began to appear. By 3067 those design have become a staple of the modern battlefield, giving rise to notable MechWarriors and new variants, while the demands of the ever-popular Solaris VII Games have resulted in a plethora of new dueling ’Mechs designed using prototype technology. Technical Readout: 3055 Upgrade presents the Solaris VII ’Mechs built using prototype technologies. Upgraded in appearance and technology, the designs first presented in the Solaris VII box set and Solaris: The Reaches are now back in print, along with several new Solaris VII designs. In addition to the upgraded appearance of selected Clan designs, all the art work for Technical Readout: 3055 Upgrade is new, providing fresh illustrations of now- classic Inner Sphere BattleMechs and Clan OmniFighters. The ’Mechs in the Solaris VII BattleMechs section are constructed using select equipment found in Tactical Operations. To use those designs, players will need that book. STAR LEAGUE ERA CLAN INVASION ERA JIHAD ERA ® SUCCESSION WARS ERA CIVIL WAR ERA DARK AGE ERA ©2011 The Topps Company Inc. All Rights Reserved. BattleTech Technical Readout: 3055 Upgrade, Classic BattleTech, BattleTech, BattleMech, and ’Mech are registered trademarks and/or trademarks of WWW.CATALYSTGAMELABS.COM The Topps Company Inc. in the United States and/or other countries. Catalyst Game Labs and the Catalyst Game Labs logo are trademarks of InMediaRes Productions, LLC. Printed in the U.S.A. -
IGNITION! an Informal History of Liquid Rocket Propellants by John D
IGNITION! U.S. Navy photo This is what a test firing should look like. Note the mach diamonds in the ex haust stream. U.S. Navy photo And this is what it may look like if something goes wrong. The same test cell, or its remains, is shown. IGNITION! An Informal History of Liquid Rocket Propellants by John D. Clark Those who cannot remember the past are condemned to repeat it. George Santayana RUTGERS UNIVERSITY PRESS IS New Brunswick, New Jersey Copyright © 1972 by Rutgers University, the State University of New Jersey Library of Congress Catalog Card Number: 72-185390 ISBN: 0-8135-0725-1 Manufactured in the United Suites of America by Quinn & Boden Company, Inc., Rithway, New Jersey This book is dedicated to my wife Inga, who heckled me into writing it with such wifely re marks as, "You talk a hell of a fine history. Now set yourself down in front of the typewriter — and write the damned thing!" In Re John D. Clark by Isaac Asimov I first met John in 1942 when I came to Philadelphia to live. Oh, I had known of him before. Back in 1937, he had published a pair of science fiction shorts, "Minus Planet" and "Space Blister," which had hit me right between the eyes. The first one, in particular, was the earliest science fiction story I know of which dealt with "anti-matter" in realistic fashion. Apparently, John was satisfied with that pair and didn't write any more s.f., kindly leaving room for lesser lights like myself. -
Weapons Pack
Weapons Pack for Strike Fighters: Project 1 Wings Over Vietnam Wings Over Europe 03 Jul 2006 ________________________________________________________________________ Rob "Bunyap" McCray [email protected] www.bunyap2w1.com Overview This project is designed to provide a hassle free way of obtaining every 3rd party released weapon and gun. It will be updated after every aircraft release to include the newly created ordnance, gun types, and fuel tanks. All data is checked and verified by experts to provide the most realistic weapons effects and performance possible. The Weapons Pack is compatible with Strike Fighters: Project 1, Wings Over Vietnam, and Wings Over Europe. This version of the Weapons Pack has been re-designed with a far superior system for nation and date assignments than previous versions. Modified aircraft data must be used to take advantage of this. Instructions for installing this data and modifying aircraft that are not included are provided. Some other enhancements include functional targeting pods, guidance for laser, EO, IIR, and GPS guided bombs, better missile guidance, functional EO/IR guided missiles, and functional weapon availability dates. Effects created by Deuces or based on his work are included covering the range of weapons currently available. These include: Bomb explosion effects of various sizes. Cluster Bomb explosion effects. Rocket Launcher effects. Missile and Rocket motor effects. Smoke trails. White Phosphorus explosion effects. Colored smoke effects for WP rockets. Leaflet bomb effects. Chaff and flare effects. White Phosphorus smoke for Anti-radiation missiles. Inert bomb and rocket effects. Spotting charge effects for practice bombs. Rocket sub-munition effects. Illumination flare effects. Napalm explosion effects. -
The Luftwaffe in Wwii: Aircraft • Secret Weapons, Experimental Designs, Jet Aircraft, Rockets & Missiles
42 THE LUFTWAFFE IN WWII: AIRCRAFT • SECRET WEAPONS, EXPERIMENTAL DESIGNS, JET AIRCRAFT, ROCKETS & MISSILES Messerschmitt Bf 110 over all Fronts Secret Wonder Weapons of the Third Reich: Dragonfly: The Luftwaffe’s Experimental 1939-45 Held & Nauroth. The WWII Luft- German Missiles 1934-45 Miranda & Mercado. Triebflügeljäger Project David Myhra. The waffe’s two-engined attack and night-fighter This book covers the great variety of secret and world’s first attempt at perfecting a true, tail-sitting aircraft shown in all its variants over a variety largely unknown German missile programs, under vertical take off and landing (VTOL) interceptor of war fronts. categories such as guided missiles, piloted missiles, flying machine – Focke-Wulf’s Triebflügeljäger, Size: 7.75”x10.5” • 200 bw photos • 248pp. and ballistic missiles. of 1944. ISBN: 0-88740-286-0 • hard • $29.95 Size: 8.5”x11” • 150 bw photos • 144pp. Size: 8.5”x11” • 240 color/bw photos • 120pp. ISBN: 0-7643-0086-5 • hard • $35.00 ISBN: 0-7643-1877-2 • soft • $29.95 Messerschmitt Bf 110/Me 210/Me 410: German Jet Aircraft 1939-45 Hans-Peter Gotha P.60 David Myhra. A detailed look at the An Illustrated History Mankau & Petrick. Diedrich. Germany was one of the leading devel- aircraft proposed by Gotha to replace the Horten For the first time, this richly illustrated book opers of jet propulsion during WWII – in August Ho 229, which had already been selected for series offers a comprehensive, detailed examination 1939 the world’s first jet aircraft, the Heinkel He production by the RLM. Includes a comparison of of the legendary Messerschmitt Bf 110, Me 210, 178, took to the air on its maiden flight. -
Messerschmitt Me 262B-1A/U1
consTRUCTion Me 262 ieaves the production (ine at a heavjly assembly piant situated in the woods, possibly eim, adjacent to the Munich—Stuttgart Autobahn. The Swallow's Anatomy The me 262, unofficially named the Sclìwalbe, or swallow, mas optimised for simple and cheap construction. The type's structure is described by Dr RLFRED PRICE LTHOUGH THE BASIC structure with single l-section main- Structure of the Me 262 spars, with flush-riveted stressed airframe was essentially skin fitted into recesses in the A nothing new, the aircraft did underside of the fuselage. The centre introduce a number of innovations in portions, between the fuselage and aircraft design, most notably the engine nacelles, had a sweptback wing's thickness-to-chord ratio, leading edge and swept-forward which was kept low to provide high- trailing edge. The outer portions of speed aerodynamic efficiency. These the wings were tapered and swept• notes describe a typical Me 262A. back, with square-cut tips. The ABOVE The Rheìnmetall-Borsig MK108 30mm cannon. A sweepback at the wing leading edge technician hoids one of the 330g (11oz) high-explosive rounds. BELOW An Me 262A-1a of JG7 with 12 R4M 55mm folding-fìn Fuselage was 18° 32'. The wings had rocitets mounted on a wooden racle under the starboard wing. The fuselage was an ali-metal detachable tips and full-span semi-monocoque structure of near- automatic leading-edge slats. triangular section with rounded Frise-type ailerons were fitted in two corners, the wing passing through sections on each wing, Slotted flaps the base. It was assembied in tour were mounted inboard of the ailerons sections: the nose cone, which and had maximum extension of 60° housed the guns and ammunition, and a backward movement of Sin. -
The Royal Hungarian Army 1920 - 1945 Volume I Organization and History
The Royal Hungarian Army 1920 - 1945 Volume I Organization and History Leo W.G. Niehorster 2 The Royal Hungarian Army 1920 - 1945 The Royal Hungarian Army 1920 – 1945 by Leo W.G. Niehorster Copyright © 1998 and 2010 by Leo W.G. Niehorster All rights reserved. Except for use in a review, no portion of this book may be reproduced in any form without the express written permission of the pub- lisher. Neither the author nor the publisher assumes any responsibility for the use or misuse of information contained in this book. The Royal Hungarian Army 1920 - 1945 3 CONTENTS Page Foreword .................................................................................................................................. 4 Hungarian Military Organizational Symbols................................................................................ 5 A Short Review of Hungarian History up to 1920 ....................................................................... 6 Part I The Royal Hungarian Army 1920 – 1941 Chapter 1 Hungary Between the Wars ................................................................................... 16 Chapter 2 Military Organization and the Armed Forces ........................................................ 21 Chapter 3 The Ground Forces to 1941 ................................................................................... 38 Chapter 4 The Air Force to 1941............................................................................................ 54 Chapter 5 The River Forces to 1941 .....................................................................................