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List Of Tailless Aircraft
A tailless aircraft is one which has no separate horizontal stabilizer or control surface, either behind or in front of the main wing. List of aircraft , - , Aériane Swift , , US , , Glider , , , , 1989 , , , , n/a , , Foot-launched. , - , Aerospatiale-BAC Concorde , , France & UK , , Jet , , Transport , , 1969 , , Production , , 20 , , SST. , - , AeroVironment Wasp III , , US , , Propeller , , UAV , , 2007 , , , , n/a , , Date of service entry with USAF , - , Akaflieg München Mü5 Wastl , , Germany , , Glider , , Experimental , , 1929 , , Prototype , , 1 , , , - , Akaflieg Braunschweig SB-13 Arcus , , Germany , , Glider , , Experimental , , 1988 , , Prototype , , 1 , , , - , Antonov E-153 , , USSR , , Jet , , Fighter , , 1947 , , Prototype , , 1 , , , - , Arup S-1 , , US , , Propeller , , Experimental , , 1932 , , Prototype , , 1 , , Rounded "heel wing". , - , Arup S-2 , , US , , Propeller , , Experimental , , 1 ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Tailless Aircraft
In aeronautics, a tailless aircraft is an aircraft with no other horizontal aerodynamic surface besides its main wing. It may still have a fuselage, vertical tail fin (vertical stabilizer), and/or vertical rudder. Theoretical advantages of the tailless configuration include low parasitic drag as on the Horten H.IV soaring glider and good stealth characteristics as on the Northrop B-2 Spirit bomber. Disadvantages include a potential sensitivity to trim. Tailless aircraft have been flown since the pioneer days; the first stable aeroplane to fly was the tailless Dunne D.5, in 1910. The most successful tailless configuration has been the tailless delta, especially for combat aircraft, though the most familiar tailless delta is the Concorde airliner. NASA has used the 'tailless' description for the novel X-36 research aircraft which has a canard foreplane but no vertical fin. Aircraft configuration A tailless aircraft has no other horizontal surface besides its main wing. The aer ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Baynes Bat
The Baynes Bat (or sometimes Slingsby-Baynes Bat) was an experimental glider of the Second World War, designed by L. E. Baynes. It was used to test the tailless design that he had suggested as a means to convert tanks into temporary gliders so they could be flown into battle. Design and development In the late 1930s, armies were looking for a way to airlift heavy military units. There were then no cargo aircraft big enough to lift a tank, and even if such a large aircraft had been created it would have needed many special facilities. A solution which was explored during the Second World War was to tow tanks as gliders, and for this wings had to be added. Most designs were based on straight wings with extended empennage and stabilizers. The design of L.E. Baynes AFRAeS in 1941 was for a 100 ft wingspan "Carrier Wing Glider" consisting chiefly of a swept wing with vertical stabilizers on the wingtips. A 1/3 scale prototype was built entirely of wood in 1943 by Slingsby S ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Douglas F4D Skyray
The Douglas F4D Skyray (later redesignated F-6 Skyray) is an American carrier-based fighter/interceptor built by the Douglas Aircraft Company. Although it was in service for a relatively short time (1956–1964) and never entered combat, it was the first carrier-launched aircraft to hold the world's absolute speed record, at 752.943 mph,Angelluci 1987, p. 92. (1211.744 km/h) and was the first United States Navy and United States Marine Corps fighter that could exceed Mach 1 in level flight.Francillon 1979, p. 480. It was the last fighter produced by the Douglas Aircraft Company before it merged with McDonnell Aircraft and became McDonnell Douglas. The F5D Skylancer was an advanced development of the F4D Skyray that did not go into service. Design and development The Skyray was designed to meet a Navy requirement issued in 1947 for a fighter aircraft that could intercept and destroy an enemy aircraft at an altitude of 50,000 ft (15,240 m) within five minu ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Dassault Mirage III
The Dassault Mirage III () is a family of single/dual-seat, single-engine, fighter aircraft developed and manufactured by French aircraft company Dassault Aviation. It was the first Western European combat aircraft to exceed Mach 2 in horizontal flight,"Mirage III." ''Dassault Aviation'', 18 December 2015. a feat which was achieved on 24 October 1958. In 1952, the French government issued its specification, calling for a , all-weather |
Convair B-58 Hustler
The Convair B-58 Hustler, designed and produced by American aircraft manufacturer Convair, was the first operational bomber capable of Mach 2 flight. The B-58 was developed during the 1950s for the United States Air Force (USAF) Strategic Air Command (SAC). To achieve the high speeds desired, Convair chose a delta wing design used by contemporary fighters such as the Convair F-102. The bomber was powered by four General Electric J79 engines in underwing pods. It had no bomb bay: it carried a single nuclear weapon plus fuel in a combination bomb/fuel pod underneath the fuselage. Later, four external hardpoints were added, enabling it to carry up to five weapons. The B-58 entered service in March 1960, and flew for a decade with two SAC bomb wings: the 43rd Bombardment Wing and the 305th Bombardment Wing. It was considered difficult to fly, imposing a high workload upon its three-man crews. Designed to replace the subsonic Boeing B-47 Stratojet strategic bomber, the B-58 be ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Convair F-106 Delta Dart
The Convair F-106 Delta Dart was the primary all-weather interceptor aircraft of the United States Air Force from the 1960s through to the 1980s. Designed as the so-called "Ultimate Interceptor", it proved to be the last specialist interceptor in U.S. Air Force service to date. It was gradually retired during the 1980s, with the QF-106 drone conversions of the aircraft being used until 1998 under the ''Pacer Six'' program.Winchester 2006, p. 55. Development Antecedents The F-106 was the ultimate development of the USAF's 1954 interceptor program of the early 1950s. The initial winner of this competition had been the F-102 Delta Dagger, but early versions of this aircraft had demonstrated extremely poor performance, limited to subsonic speeds and relatively low altitudes. During the testing program the F-102 underwent numerous changes to improve its performance, notably the application of the area rule to the fuselage shaping and a change of engine, and the dropping of the advan ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Convair F-102 Delta Dagger
The Convair F-102 Delta Dagger was an American interceptor aircraft designed and manufactured by Convair. Built as part of the backbone of the United States Air Force's air defenses in the late 1950s, it entered service in 1956. Its main purpose was to intercept invading Soviet strategic bomber fleets (primarily the Tupolev Tu-95) during the Cold War. A total of 1,000 F-102s were built. A member of the Century Series, the F-102 was the USAF's first operational supersonic interceptor and delta-wing fighter. It used an internal weapons bay to carry both guided missiles and rockets. As originally designed, it could not achieve Mach 1 supersonic flight until redesigned with area ruling. The F-102 replaced subsonic fighter types such as the Northrop F-89 Scorpion, and by the 1960s, it saw limited service in the Vietnam War in bomber escort and ground-attack roles. It was supplemented by McDonnell F-101 Voodoos and, later, by McDonnell Douglas F-4 Phantom IIs. Many of the F- ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Convair F2Y Sea Dart
The Convair F2Y Sea Dart was an American seaplane fighter aircraft that rode on twin hydro-skis during takeoff and landing. It flew only as a prototype, and never entered mass production. It is the only seaplane to have exceeded the speed of sound. It was created in the 1950s, to overcome the problems with supersonic planes taking off and landing on aircraft carriers. The program was canceled after a series of unsatisfactory results and a tragic accident on 4 November 1954, in which test pilot Charles E. Richbourg was killed when the Sea Dart he was piloting disintegrated in midair. The four surviving planes were retired in 1957, but some were kept in reserve until 1962. Development The Sea Dart began as Convair's entry in a 1948 U.S. Navy contest for a supersonic interceptor aircraft. At the time, there was much skepticism about operating supersonic aircraft from carrier decks. In order to address this issue, the U.S. Navy ordered many subsonic fighters. The worry had some fo ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Convair XF-92A
The Convair XF-92 (re-designated from XP-92 in 1948) was an American, delta wing, first-generation jet prototype. Originally conceived as a point-defence interceptor, the design was later used purely for experimental purposes and only one was built. However, it led Convair to use the delta-wing on a number of designs, including the F-102 Delta Dagger, F-106 Delta Dart, B-58 Hustler, the US Navy's F2Y Sea Dart as well as the VTOL FY Pogo. Design and development Early work Prior to August 1945, the Vultee Division of Consolidated-Vultee looked at the possibility of a swept-wing aircraft powered by a ducted rocket. Years earlier, the company had performed designs which involved liquid-cooled radiator engines. With this design, fuel would be added to the heat produced by small rocket engines in the duct, creating a "pseudo-ramjet".Jenkins and Landis 2008, p. 122. In August 1945, the United States Army Air Forces (USAAF), soon to be renamed the United States Air Force, iss ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Charpentier C1
The Charpentier C1 was a French tailless experimental aircraft that was designed by Jean Charpentier during the 1930s. The single prototype A prototype is an early sample, model, or release of a product built to test a concept or process. It is a term used in a variety of contexts, including semantics, design, electronics, and Software prototyping, software programming. A prototyp ... crashed on its first flight in January 1934 and further development was cancelled. Specifications (variant specified) References Bibliography *{{cite journal , last1=Borget, first1=Michel, title=Il ne vola qu'un court instant... le Charpentier C 1, journal=Le Fana de l'Aviation , date=November 1977 , issue=96 , pages=8–11 , issn=0757-4169 , language=fr , trans-title=It Only Flew for a Short Time... The Charpentier C 1 Tailless aircraft Trimotors 1930s French experimental aircraft Aircraft first flown in 1934 Tractor aircraft ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Brochocki BKB-1
The Brochocki BKB-1 was a Canadian mid-wing, single-seat, experimental tailless glider that was designed and constructed by Stefan Brochocki with assistance from Witold Kasper and A. Bodek. The designation indicated the contributions of all three men. The aircraft was intended to study flight above the stall angle.Rogers, Bennett: ''1974 Sailplane Directory, Soaring Magazine'', page 94. Soaring Society of America, August 1974. USPS 499-920 Design and development The BKB-1 was constructed in 1959 and built entirely from wood. The wing was swept, had a 9.5:1 aspect ratio and employed a NACA 8-H-12 airfoil. The aircraft had a very high wing area of which resulted in a light wing loading of just 3.81 lb/sq ft (18.6 kg/m2). The prototype BKB-1 was originally registered in Canada as CF-ZDK-X. Later it was moved to the United States, owned by Kasper and registered as N2991G. As a testbed the aircraft went through several modification states. The modifications includ ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
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