The designers of the Horten H.XVIII also designed the world's first jet-powered flying wing known by what name?
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Horten H.XVIII The Horten H.XVIII was a proposed German World War II intercontinental bomber, designed by the Horten brothers with pioneering features such as a flying wing configuration, turbojet engines and stealth characteristics. The unbuilt H.XVIII represented, in many respects, a scaled-up version of the Horten Ho 229, a prototype jet fighter. The H.XVIII was one of many proposed designs for an "Amerika Bomber", and would have carried sufficient fuel for transatlantic flights.
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Horten brothers Walter Horten (born 13 November 1913; died 9 December 1998 in Baden-Baden, Germany) and Reimar Horten (born 12 March 1915; died 14 March 1994 in Villa General Belgrano, Argentina), sometimes credited as the Horten Brothers, were German aircraft pilots and enthusiasts. Although they had little, if any, formal training in aeronautics or related fields, the Hortens designed some of the most revolutionary aircraft of the 1940s, including the world's first jet-powered flying wing, the Horten Ho 229.
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Boeing 747 The Boeing 747 is an American wide-body commercial jet airliner and cargo aircraft, often referred to by its original nickname, ""Jumbo Jet"". Its distinctive "hump" upper deck along the forward part of the aircraft makes it among the world's most recognizable aircraft, and it was the first wide-body produced. Manufactured by Boeing's Commercial Airplane unit in the United States, the original version of the 747 was envisioned to have 150 percent greater capacity than the Boeing 707, one of the common large commercial aircraft of the 1960s. First flown commercially in 1970, the 747 held the passenger capacity record for 37 years.
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Fixed-wing aircraft A fixed-wing aircraft is an aircraft, such as an airplane or aeroplane (See Spelling Differences), which is capable of flight using wings that generate lift caused by the vehicle's forward airspeed and the shape of the wings. Fixed-wing aircraft are distinct from rotary-wing aircraft, in which the wings form a rotor mounted on a spinning shaft, and ornithopters, in which the wings flap in similar manner to a bird.
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Sikorsky R-4 The Sikorsky R-4 was a two-seat helicopter designed by Igor Sikorsky with a single, three-bladed main rotor and powered by a radial engine. The R-4 was the world's first large-scale mass-produced helicopter and the first helicopter used by the United States Army Air Forces, the United States Navy, the United States Coast Guard and the United Kingdom's Royal Air Force and Royal Navy. In U.S. Navy and U.S. Coast Guard service, the helicopter was known as the Sikorsky HNS-1. In British service, it was known as the Hoverfly.
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Bede Wing The Bede Wing was an inflated hang glider, designed in the 1970s by aeronautical engineer Jim Bede. Intended as a safer alternative to conventional hang gliders, it resembled an early ram-air parachute, but instead was an inflatable structure, that could be filled with air for gliding, or with helium to act as a gas balloon.
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Biplane A biplane is a fixed-wing aircraft with two main wings stacked one above the other. The first powered, controlled aeroplane to fly, the Wright Flyer, used a biplane wing arrangement, as did many aircraft in the early years of aviation. While a biplane wing structure has a structural advantage over a monoplane, it produces more drag than a similar unbraced or cantilever monoplane wing. Improved structural techniques, better materials and the quest for greater speed made the biplane configuration obsolete for most purposes by the late 1930s.
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Tupolev Tu-98 The Tupolev Tu-98 (NATO reporting name Backfin) was a prototype swept wing jet bomber developed by Tupolev for the Soviet Union.
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Roy Chaplin Roland Henry Chaplin, OBE, FRAeS, (16 May 1899 – 13 December 1988), known as "Roy", was an aeronautical engineer who worked with Sydney Camm at Hawker Aircraft Limited from 1927 to 1962. He helped design the Hawker Fury biplane, the Hurricane monoplane, and the Harrier jump-jet. He graduated with a degree in engineering from London University and retired in the 1960s.
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Hawker Tempest The Hawker Tempest is a British fighter aircraft primarily used by the Royal Air Force (RAF) in the Second World War. The Tempest, originally known as the "Typhoon II", was an improved derivative of the Hawker Typhoon, intended to address the Typhoon's unexpected fall-off of performance at high altitude by replacing its wing with a thinner laminar flow design. Having diverged considerably from the Typhoon, it was chosen to rename the aircraft "Tempest". The Tempest emerged as one of the most powerful fighters of World War II and was the fastest single-engine propeller-driven aircraft of the war at low altitude. The propeller-driven Dornier 335 was even faster, but it had two engines.
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AEA White Wing The White Wing (or Aerodrome #2) was an early US aircraft designed by Frederick W. Baldwin and built by the Aerial Experiment Association in 1908. Unusual for aircraft of its day, it featured a wheeled undercarriage. The wings were equipped with ailerons controlled by a harness worn around the pilot's body; leaning in one direction would cause the aircraft to bank to follow.
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Curtiss Eagle The Curtiss Eagle (retroactively designated the Model 19 by Curtiss some years later) was an airliner produced in small numbers in the United States shortly after World War I. The aircraft was a conventional biplane with three-bay, unstaggered wings of equal span. The fuselage was a very advanced design for its day, incorporating careful streamlining of its monocoque structure, and offering the crew as well as the passengers a fully enclosed cabin. The Eagle is sometimes named as the first American tri-motor aircraft; however Curtiss' own Model H flying boat flew with three engines for a time in 1914 before being converted back to twin-engine configuration.
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Santos-Dumont 14-bis The 14-bis "(Quatorze-bis )", also known as Oiseau de proie ("bird of prey" in French), was a pioneer era canard biplane designed and built by Brazilian aviation pioneer Alberto Santos-Dumont. In 1906 near Paris the "14-bis" made a manned powered flight that was the first to be publicly witnessed by a crowd and the first by an airplane outside the U.S.
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Nord 260 The Nord 260, built in prototype form as the Max Holste MH.260 Super Broussard, ("Super Bushranger"), was a turboprop-powered, uprated version of the piston-engined Max Holste MH.250 Super Broussard, that was further developed into the Aérospatiale N 262.
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Hannover F.10 The Hannover F.10 was an early German airliner developed shortly after World War I by Hannoversche Waggonfabrik based on their wartime escort fighters; the Hannover CL.II and its derivatives. Unlike those aircraft, which were all biplane designs, the F.10 was a single-bay triplane, with a middle wing mounted flush with the fuselage top, and a top wing mounted on struts above it. I-struts were used in the interplane gap, as on the Hannover CL.V. The fuselage was essentially similar to its military forebears, but the tail gunner's position was now enclosed as a cabin for two passengers and the wing-mounted radiator was substituted for a frontal radiator. The F.10 also featured the characteristic biplane tail unit that had been developed originally to give the tail gunner a good field of fire.
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Fokker D.XVII Fokker D.XVII, was a Dutch biplane created by Fokker.
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Convair B-58 Hustler The Convair B-58 Hustler was the first operational jet bomber capable of Mach 2 flight. The aircraft was designed by Convair engineer Robert H. Widmer and developed for the United States Air Force for service in the Strategic Air Command (SAC) during the 1960s. It used a delta wing, which was also employed by Convair fighters such as the F-102, with four General Electric J79 engines in pods under the wing. It carried five nuclear weapons; four on pylons under the wings, and one nuclear weapon and fuel in a combination bomb/fuel pod under the fuselage, rather than in an internal bomb bay.
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Blériot VIII The Blériot VIII was a French pioneer era aeroplane built by Louis Blériot, significant for its adoption of both a configuration and a control system that were to set a standard for decades to come. The previous year, Blériot had experimented with a tandem wing design, the Blériot VI, then built another aircraft, the Blériot VII, in which the rear wing was somewhat smaller than the front wing. In the Blériot VIII, he reduced the size of the rear wing yet again, to the point where it was no longer contributing much in the way of lift, but had become the horizontal stabiliser. More novel was his adoption of a single control stick that would control both roll and pitch, while the rudder was controlled by a horizontal, centrally pivoted bar swung by the pilot's feet. A similar control arrangement for roll and pitch control had been incorporated into an aircraft the previous year by Robert Esnault-Pelterie, but the Bleriot VIII was the first use in a single airframe of the combination of hand/arm-operated joystick and foot-operated rudder control, that is in use to the present day, for the basic format of aerodynamic aircraft control systems.
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General Electric J97 The General Electric J97 is a single-shaft turbojet engine designed and built by General Electric as a compact high-performance engine for light attack fighters and eventually a number of drone projects.
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Junkers Ju 49 The Junkers Ju 49 was a German aircraft designed to investigate high-altitude flight and the techniques of cabin pressurization. It was the world's second working pressurized aircraft, following the Engineering Division USD-9A which first flew in the United States in 1921. By 1935, it was flying regularly to around 12,500 m (41,000 ft).
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Dayton-Wright Racer The Dayton-Wright RB-1 (Rinehart-Bauman model one), also known simply as the Dayton-Wright Racer was a racing aircraft developed in the United States to participate in the 1920 Gordon Bennett Cup air race. Advanced for its day, the aircraft was a high-wing monoplane with a monocoque fuselage and cantilever wing (built of solid balsa wood covered in plywood and linen that incorporated a Grant designed mechanism to vary its camber in flight by moving the leading edge and trailing edge. The aircraft also featured a retractable undercarriage operated by a hand-crank making it one of the first instances of undercarriage retraction for aerodynamic benefit alone. The propeller shaft was mounted through a large oval radiator, the pilot had no forward view, but was provided with flexible celluloid side windows. Cockpit access was through a hatch in the top of the fuselage. A prototype was built using non-retractable gear and strut-braced wings. A shorter tapered "racing wing" was installed afterward with leading and trailing edge flaps interconnected with landing gear deployment. The mechanisms and hinges for the wing flaps were exposed across the top of the solid wing. The racing wing produced directional instability requiring small tail fins to be added.
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Lippisch Ente The Ente (German: "duck" ) was the world’s first rocket-powered full-size aircraft. It was designed by Alexander Lippisch as a sailplane and first flown under power on June 11, 1928, piloted by Fritz Stamer.