V 1 flying bomb Wikipedia. V 1 flying bomb. Fieseler Fi 1. Flakzielgert 7. 6 FZG 7. Type. Guided missile. Place of origin. Nazi Germany. Service history. In service. Used by. Luftwaffe. Wars. World War IIProduction history. As Cassinis tour of Saturn comes to a close, NASAs getting a bit nostalgic. Yesterday, the space agency released a photo of Saturns North pole the doomed. A consideration for this If warfare is about causing the maximum destruction, these space siege scenarios make sense. If warfare is about achieving political. A flurry of reports claim that bomb shelter sales have skyrocketed recently. Ron Hubbard, president of Atlas Survival Shelters, told a California Fox affiliate that. The V1 flying bomb German Vergeltungswaffe 1 Vengeance Weapon 1also known to the Allies as the buzz bomb, or doodlebug, and in Germany as Kirschkern. Designer. Robert Lusser. Manufacturer. Fieseler. Unit cost. 5,0. 90 RMSpecifications. Weight. 2,1. 50 kg 4,7. Length. 8. 3. 2 m 2. Width. 5. 3. 7 m 1. Height. 1. 4. 2 m 4 ft 8 inWarhead. File Download Prompt Windows 7 Iso Image From Microsoft. Get the latest science news and technology news, read tech reviews and more at ABC News. Tabtight professional, free when you need it, VPN service. ISSN 2278 1323 International Journal of Advanced Research in Computer Engineering Technology IJARCET Volume 2, Issue 1, January 2013 47. Bomb disposal is the process by which hazardous explosive devices are rendered safe. Bomb disposal is an allencompassing term to describe the separate, but. Amatol 3. 9Warhead weight. Engine. Argus As 1. Pulsejet. Operationalrange. Speed. 64. 0 kmh 4. Guidancesystem. Gyrocompass based autopilot. The V 1 flying bomb German Vergeltungswaffe 1 Vengeance Weapon 1aalso known to the Allies as the buzz bomb, or doodlebug,b and in Germany as Kirschkern cherrystone or Maikfer maybug5was an early cruise missile and the only production aircraft to use a pulsejet for power. The V 1 was developed at Peenemnde Army Research Center in 1. Nazi German. Luftwaffe during the Second World War. During initial development it was known by the codename Cherry Stone. The first of the so called Vengeance weapons V weapons or Vergeltungswaffen series designed for terror bombing of London because of its limited range, the thousands of V 1 missiles launched into England were fired from launch facilities along the French Pas de Calais and Dutch coasts. The first V 1 was launched at London on 1. June 1. 94. 4,6 one week after and prompted by the successful Allied landings in Europe. At its peak, more than one hundred V 1s a day were fired at south east England, 9,5. October 1. 94. 4, when the last V 1 site in range of Britain was overrun by Allied forces. After this, the V 1s were directed at the port of Antwerp and other targets in Belgium, with 2,4. V 1s being launched. The attacks stopped only a month before the war in Europe ended, when the last launch site in the Low Countries was overrun on 2. March 1. 94. 5. The British operated an arrangement of air defences, including anti aircraft guns and fighter aircraft, to intercept the bombs before they reached their targets as part of Operation Crossbow, while the launch sites and underground V 1 storage depots were targets of strategic bombing. Design and developmenteditIn late 1. Argus Motoren company, Fritz Gosslau began work on the further development of remote controlled aircraft Argus had already developed a remote controlled surveillance aircraft, the AS 2. FZG 4. 3. On 9 November 1. RLM German Air Ministry. Argus worked in cooperation with Lorentz AG and Arado Flugzeugwerke to develop the project as a private venture, and in April 1. Gosslau presented an improved study of Project Fernfeuer to the RLM, as Project P 3. Erfurt. On 3. 1 May, Rudolf Bree of the RLM commented that he saw no chance that the projectile could be deployed in combat conditions, as the proposed remote control system was seen as a design weakness. Heinrich Koppenberg, the director of Argus, met with Ernst Udet on 6 January 1. Udet decided to cancel it. Bomb Detection Robot Project Pdf' title='Bomb Detection Robot Project Pdf' />Despite this, Gosslau was convinced that the basic idea was sound and proceeded to simplify the design. As an aircraft engine manufacturer, Argus lacked the capability to produce a fuselage for the project and Koppenberg sought the assistance of Robert Lusser, chief designer and technical director at Heinkel. On 2. 2 January 1. Lusser took up a position with the Fieseler aircraft company. He met with Koppenberg on 2. February and was informed of Gosslaus project. Gosslaus design used two pulsejet engines Lusser improved the design to use a single engine. A final proposal for the project was submitted to the Technical Office of the RLM on 5 June and the project was renamed Fi 1. Fieseler was to be the chief contractor. On 1. 9 June, Generalfeldmarschall. Erhard Milch gave Fi 1. Bomb Detection Robot Project Pdf' title='Bomb Detection Robot Project Pdf' />Luftwaffes Erprobungsstelle coastal test centre at Karlshagen, part of the Peenemnde West facility. By 3. 0 August, Fieseler had completed the first fuselage, and the first flight of the Fi 1. V7 took place on 1. December, when it was airdropped by a Fw 2. The V 1 was named by The Reich journalist Hans Schwarz Van Berkl in June 1. Hitlers approval. DescriptioneditThe V 1 was designed under the codename Kirschkern cherry stone by Lusser and Gosslau, with a fuselage constructed mainly of welded sheet steel and wings built of plywood. The simple, Argus built pulsejet engine pulsed 5. It was known briefly in Germany on Hitlers orders as Maikfer May bug and Krhe crow. Power planteditIgnition of the Argus pulsejet was accomplished using an automotive type spark plug located about 7. Three air nozzles in the front of the pulsejet were at the same time connected to an external high pressure air source that was used to start the engine. Acetylene gas was typically used for starting the engine, and very often a panel of wood or similar material was held across the end of the tailpipe to prevent the fuel from diffusing and escaping before ignition. The V 1 was fuelled by 6. US gallons of 7. Once the engine had been started and the temperature had risen to the minimum operating level, the external air hose and connectors were removed and the engines resonant design kept it firing without any further need for the electrical ignition system, which was used only to ignite the engine when starting. Rear view of V 1 in IWM Duxford showing launch ramp section. The Argus As 0. 14 also known as a resonant jet could operate at zero airspeed because of the nature of its intake shutters and its acoustically tuned resonant combustion chamber. However, because of the low static thrust of the pulse jet engine and the very high stall speed of the small wings, the V 1 could not take off under its own power in a practically short distance, and thus needed to be ground launched by aircraft catapult or air launched from a modified bomber aircraft such as a Heinkel He 1. Beginning in January 1. V 1s pulsejet engine was also tested on a variety of craft, including automobiles and an experimental attack boat known as the Tornado. The unsuccessful prototype was a version of a Sprengboot, in which a boat loaded with explosives was steered towards a target ship and the pilot would leap out of the back at the last moment. The Tornado was assembled from surplus seaplane hulls connected in catamaran fashion with a small pilot cabin on the crossbeams. The Tornado prototype was a noisy underperformer and was abandoned in favour of more conventional piston engined craft. The engine made its first flight aboard a Gotha Go 1. April 1. 94. 1. Guidance systemeditThe V 1 guidance system used a simple autopilot developed by Askania in Berlin to regulate altitude and airspeed the RLM at first planned to use a radio control system with the V 1 for precision attacks, but the government decided instead to use the missile against London. A weighted pendulum system provided fore and aft attitude measurement to control pitch damped by a gyrocompass, which it also stabilized. Operating power for the gyroscope platform and the flight control actuators was provided by two large spherical compressed air tanks that also pressurized the fuel tank. These air tanks were charged to 1. With the counter determining how far the missile would fly, it was only necessary to launch the V 1 with the ramp pointing in the approximate direction, and the autopilot controlled the flight.