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A coleopter is a type of VTOL aircraft design that uses a ducted fan as the primary fuselage of the entire aircraft. Generally they appear to be a large barrel-like extension at the rear, with a small cockpit area suspended above it. Coleopters are generally designed as tail-sitters. The term is an anglicisation of the French coléoptère "beetle" after the first actual implementation of this design, the SNECMA Coléoptère of the mid-1950s.
The first design of an aircraft clearly using the coleopter concept was developed during World War II. From 1944 on, the Luftwaffe was suffering from almost continual daytime attacks on its airfields and was finding it almost impossible to conduct large-scale operations. Their preferred solution was to introduce some sort of VTOL interceptor that could be launched from any open location, and there were many proposals for such a system. Heinkel conducted a series of design studies as part of their Heinkel Wespe and Heinkel Lerche programs. The Wespe intended to use a Benz 2,000 hp turboprop engine, but these were not forthcoming and the Lerche used two Daimler-Benz DB 605 piston engines instead. Nothing ever came of either design.
In the immediate post-war era, most VTOL research involved helicopters. As the limitations of the simple rotary wing became clear, teams started looking for other solutions and many turned to using jet engines directly for vertical thrust. SNECMA, now Safran Aircraft Engines, developed a series of such systems as part of the SNECMA Atar Volant series during the 1950s. To further improve the design, SNECMA had Nord Aviation build an annular wing and adapted it to the last of the Volant series to produce the SNECMA Coléoptère. The Coléoptère first flew on 6 May 1959, but crashed on 25 July and no replacement was built. Even in this limited testing period, the design showed several serious problems related to the high angular momentum of the engine, which made control tricky.
In the US, Hiller Aircraft had been working on a number of ducted fan flying platforms originally designed by Charles H. Zimmerman. The Hiller VXT-8 Coleopter was a proposed annular wing VTOL aircraft designed in the late 1950s, inspired by the French SNECMA Coléoptère. After some early successes, the Army demanded a series of changes that continued to increase the size and weight of the platform, which introduced new stability problems. These generally required more size and power to correct, and no satisfactory design came from these efforts. Instead, Hiller approached the Navy with the idea of building a full coleopter design.
This emerged as the Hiller VXT-8 which was significantly similar to the SNECMA design, although it used a propeller instead of a jet engine. However, the introduction of turbine-powered helicopters like the Bell UH-1 Iroquois so significantly improved their performance over piston-powered designs that the Navy lost interest in the VXT-8 in spite of even better estimated performance. Only a mock-up was completed.
Convair selected the coleopter layout for their Model 49 proposal, entered into the Advanced Aerial Fire Support System (AAFSS).
AAFSS asked for a new high-speed helicopter design for the attack and escort roles. Submissions included gyrodynes, dual-rotor designs and similar advances on conventional designs, but nothing was as unconventional as the Model 49.
The Model 49 was based on a tri-turbine design featuring counter-rotating propellers within a shroud. Exposed areas were armored to withstand 12.7mm fire. The two-man crew was located in an articulated capsule which could either point forward of the shroud when horizontal or at right-angles to it when vertical, and pilot controls were limited to engine speed, blade angle and directional control. The design was believed by its manufacturers to be inherently more reliable than that of conventional helicopters. [1]
As a "tail-sitter" design, and like its forebear the Convair XFY-1 POGO, the Model 49 was intended to take off from a vertical orientation before transitioning to horizontal orientation for flight. Once at its destination it could transition back to vertical mode to hover and provide fire support. [2]
The design was intended to be capable of carrying multiple armament configurations, with all weapons being remotely controlled by the gunner from the crew capsule. [2] Its hardpoints consisted of two side turrets, a center turret, and two hardpoints each for two of the nacelles. All of the weapons could be used in either horizontal or vertical configuration, as well as while grounded. The turrets were mechanically prevented from firing "up" at the crew capsule while in vertical configuration. The side turrets could feature either 7.62 mm machine guns with 12,000 rounds of ammunition each, or 40mm grenade launchers with 500 rounds each. [1]
The center turret carried an XM-140 30mm cannon with 1000 rounds, with the option for a second 30mm cannon, or 500 WASP rockets. Any of the four hardpoints could carry three BGM-71 TOW missiles, or three Shillelagh missiles. Alternatively, up to one hardpoint on each of the nacelles could carry an M40A1C 106mm recoilless rifle with 18 rounds. As an alternative, the hardpoints could mount up to 1,200 gallons of additional fuel in tanks. [1]
Deemed overly complicated, the Army instead selected the Lockheed AH-56 Cheyenne and Sikorsky S-66 for further development. In the end only scale models of the model 49 were ever built. [2]
A vertical take-off and landing (VTOL) aircraft is one that can take off and land vertically without relying on a runway. This classification can include a variety of types of aircraft including helicopters as well as thrust-vectoring fixed-wing aircraft and other hybrid aircraft with powered rotors such as cyclogyros/cyclocopters and gyrodynes.
A tiltrotor is an aircraft that generates lift and propulsion by way of one or more powered rotors mounted on rotating shafts or nacelles usually at the ends of a fixed wing. Almost all tiltrotors use a transverse rotor design, with a few exceptions that use other multirotor layouts.
The Hiller Aviation Museum is an aircraft history museum located at the San Carlos Airport in San Carlos, California. It has over fifty aircraft on display, as well as flight simulators, plane cockpits and other exhibits tracing aviation history. The museum was founded by Stanley Hiller in June 1998 and is endowed by members of the Hiller family. It specializes in Northern California aircraft history and helicopter history. The museum is also an affiliate within the Smithsonian Affiliations program.
A vertical and/or short take-off and landing (V/STOL) aircraft is an airplane able to take-off or land vertically or on short runways. Vertical takeoff and landing (VTOL) aircraft are a subset of V/STOL craft that do not require runways at all. Generally, a V/STOL aircraft needs to be able to hover. Helicopters are not considered under the V/STOL classification as the classification is only used for aeroplanes, aircraft that achieve lift (force) in forward flight by planing the air, thereby achieving speed and fuel efficiency that is typically greater than the capability of helicopters.
A tiltwing aircraft features a wing that is horizontal for conventional forward flight and rotates up for vertical takeoff and landing. It is similar to the tiltrotor design where only the propeller and engine rotate. Tiltwing aircraft are typically fully capable of VTOL operations.
A tail-sitter, or tailsitter, is a type of VTOL aircraft that takes off and lands on its tail, then tilts horizontally for forward flight.
The Convair XFY-1 Pogo was an experimental V/STOL aircraft developed during the early years of the Cold War. It was intended to be a high-performance fighter aircraft capable of operating from small warships. Lockheed and Convair were awarded contracts to build experimental VTOL fighters, with Convair producing the XFY-1, also known as the "Pogo." It was developed as an attempt to create a practical V/STOL aircraft.
The Focke-Wulf Triebflügel, or Triebflügeljäger, literally meaning "thrust-wing hunter", was a German concept for an aircraft designed in 1944, during the final phase of World War II, as a defence against the ever-increasing Allied bombing raids on central Germany. It was a vertical take-off and landing tailsitter interceptor design for local defense of important factories or areas which had small or no airfields.
The Lockheed AH-56 Cheyenne is an attack helicopter developed by Lockheed for the United States Army. It rose from the Army's Advanced Aerial Fire Support System (AAFSS) program to field the service's first dedicated attack helicopter. Lockheed designed the Cheyenne using a four-blade rigid-rotor system and configured the aircraft as a compound helicopter with low-mounted wings and a tail-mounted thrusting propeller driven by a General Electric T64 turboshaft engine. The Cheyenne was to have a high-speed dash capability to provide armed escort for the Army's transport helicopters, such as the Bell UH-1 Iroquois.
The Lockheed XFV was an American experimental tailsitter prototype aircraft built by Lockheed in the early 1950s to demonstrate the operation of a vertical takeoff and landing (VTOL) fighter for protecting convoys.
The SNECMA C.450 Coléoptère was a tail-sitting vertical take-off and landing (VTOL) aircraft designed by the French company SNECMA and manufactured by Nord Aviation. While work on the aircraft proceeded to the test flying phase, the project never progressed beyond experimental purposes.
The Focke-Wulf Ta 400 was a large six-engined heavy bomber design developed in Nazi Germany in 1943 by Focke-Wulf as a serious contender for the Amerikabomber project. One of the first aircraft to be developed from components from multiple countries, it was also one of the most advanced Focke-Wulf designs of World War II, though it never progressed beyond a wind tunnel model.
The Heinkel Lerche was the name of a set of project studies made by German aircraft designer Heinkel in 1944 and 1945 for a revolutionary VTOL fighter and ground-attack aircraft.
A powered lift aircraft takes off and lands vertically under engine power but uses a fixed wing for horizontal flight. Like helicopters, these aircraft do not need a long runway to take off and land, but they have a speed and performance similar to standard fixed-wing aircraft in combat or other situations.
The SNECMA Atar Volant or C.400 P1 was a French turbojet engine produced by SNECMA as part of their "Atar" series. Encased in a basic fairing which could hold fuel and remote-control equipment, the unit weighed 5,600 pounds (2,500 kg), and generated a thrust of approximately 6,200 pounds-force ; the Atar Volant was able to cause vertical lift, which was precisely its purpose. There were later Atar Volant models, each made improvements and alterations to the previous designs, and eventually resulted in a full-fledged craft.
A closed wing is a wing that effectively has two main planes which merge at their ends so that there are no conventional wing tips. Closed wing designs include the annular wing, the joined wing, the box wing, and spiroid tip devices.
The Heinkel Wespe was a project study by the German company Heinkel for a tail-sitting, vertical take off and landing-interceptor aircraft. The aircraft did not have conventional wings, but instead featured a large rotor. Completed in 1945, it remained untested due to a lack of material at the end of the Second World War. A related project was the Heinkel Lerche.
The Convair Model 200 was a design for a supersonic vertical takeoff and landing (VTOL) fighter requirement for the United States Navy Sea Control Ship. Further versions were planned for conventional catapult launches and landing using the arresting gear.