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https://en.wikipedia.org/wiki/Horten_Ho_229
The Horten H.IX, RLM designation Ho 229 (or Gotha Go 229 for extensive re-design work done by Gotha to prepare the aircraft for mass production) was a German prototype fighter/bomber initially designed by Reimar and Walter Horten to be built by Gothaer Waggonfabrik late in World War II. It was the first flying wing to be powered by jet engines. The design was a response to Hermann Göring's call for light bomber designs capable of meeting the "3×1000" requirement; namely to carry 1,000 kilograms (2,200 lb) of bombs a distance of 1,000 kilometres (620 mi) with a speed of 1,000 kilometres per hour (620 mph). Only jets could provide the speed, but these were extremely fuel-hungry, so considerable effort had to be made to meet the range requirement. Based on a flying wing, the Ho 229 lacked all extraneous control surfaces to lower drag. It was the only design to come even close to the 3×1000 requirements and received Göring's approval. Its ceiling was 15,000 metres (49,000 ft). The H.IX was of mixed construction, with the center pod made from welded steel tubing and wing spars built from wood. The wings were made from two thin, carbon-impregnated plywood panels glued together with a charcoal and sawdust mixture. The wing had a single main spar, penetrated by the jet engine inlets, and a secondary spar used for attaching the elevons. It was designed with a 7g load factor and a 1.8× safety rating; therefore, the aircraft had a 12.6g ultimate load rating. The wing's chord/thickness ratio ranged from 15% at the root to 8% at the wingtips. The aircraft utilized retractable tricycle landing gear, with the nosegear on the first two prototypes sourced from a He 177's tailwheel system, with the third prototype using an He 177A main gear wheelrim and tire on its custom-designed nosegear strutwork and wheel fork. A drogue parachute slowed the aircraft upon landing. The pilot sat on a primitive ejection seat. A special pressure suit was developed by Dräger. The aircraft was originally designed for the BMW 003 jet engine, but that engine was not quite ready, and the Junkers Jumo 004 engine was substituted. Control was achieved with elevons and spoilers. The control system included both long-span (inboard) and short-span (outboard) spoilers, with the smaller outboard spoilers activated first. This system gave a smoother and more graceful control of yaw than would a single-spoiler system. Role Fighter/Bomber Manufacturer Gothaer Waggonfabrik Designer Horten brothers First flight 1 March 1944 (glider) Primary user Luftwaffe Number built 3 The first prototype H.IX V1, an unpowered glider with fixed tricycle landing gear, flew on 1 March 1944. Flight results were very favorable, but there was an accident when the pilot attempted to land without first retracting an instrument-carrying pole extending from the aircraft. The design was taken from the Horten brothers and given to Gothaer Waggonfabrik. The Gotha team made some changes: they added a simple ejection seat, dramatically changed the undercarriage to enable a higher gross weight, changed the jet engine inlets, and added ducting to air-cool the jet engine's outer casing to prevent damage to the wooden wing. The H.IX V1 was followed in December 1944 by the Junkers Jumo 004-powered second prototype H.IX V2; the BMW 003 engine was preferred, but unavailable. Göring believed in the design and ordered a production series of 40 aircraft from Gothaer Waggonfabrik with the RLM designation Ho 229, even though it had not yet taken to the air under jet power. The first flight of the H.IX V2 was made in Oranienburg on 2 February 1945. The V3 was larger than previous prototypes, the shape being modified in various areas, and it was meant to be a template for the pre-production series Ho 229 A-0 day fighters, of which 20 machines had been ordered. The V3 was meant to be powered by two Jumo 004C engines, with 10% greater thrust each than the earlier Jumo 004B production engine used for the Me 262A and Ar 234B, and could carry two MK 108 30 mm cannons in the wing roots. Work had also started on the two-seat Ho 229 V4 and Ho 229 V5 night-fighter prototypes, the Ho 229 V6 armament test prototype, and the Ho 229 V7 two-seat trainer. During the final stages of the war, the U.S. military initiated Operation Paperclip, an effort to capture advanced German weapons research, and keep it out of the hands of advancing Soviet troops. A Horten glider and the Ho 229 V3, which was undergoing final assembly, were transported by sea to the United States as part of Operation Seahorse for evaluation. On the way, the Ho 229 spent a brief time at RAE Farnborough in the UK, during which it was considered whether British jet engines could be fitted, but the mountings were found to be incompatible with the early British turbojets, which used larger-diameter centrifugal compressors as opposed to the slimmer axial-flow turbojets the Germans had developed. The Americans were just starting to create their own axial-compressor turbojets before the war's end, such as the Westinghouse J30, with a thrust level only approaching the BMW 003A's full output. After the war, Reimar Horten said he mixed charcoal dust in with the wood glue to absorb electromagnetic waves (radar), which he believed could shield the aircraft from detection by British early-warning ground-based radar that operated at 20 to 30 MHz (top end of the HF band), known as Chain Home. A jet-powered flying wing design such as the Horten Ho 229 has a smaller radar cross-section than conventional contemporary twin-engine aircraft because the wings blended into the fuselage and there are no large propeller disks or vertical and horizontal tail surfaces to provide a typical identifiable radar signature. Engineers of the Northrop-Grumman Corporation had long been interested in the Ho 229, and several of them visited the Smithsonian Museum's facility in Silver Hill, Maryland in the early 1980s to study the V3 airframe, in the context of developing the Northrop Grumman B-2 Spirit. A team of engineers from Northrop-Grumman ran electromagnetic tests on the V3's multilayer wooden center-section nose cones. The cones are 19 mm (0.75 in) thick and made from thin sheets of veneer. The team concluded that there was some form of conducting element in the glue, as the radar signal attenuated considerably as it passed through the cone. However, a later inspection by the museum found no trace of such material. Expert Debunking of Stealth Claims Due to the popularity of this documentary project, the Smithsonian has since posted an extensive debunking of these claims citing their own research and the paper published and presented at the 10th American Institute of Aeronautics and Astronautics Aviation Technology, Integration, and Operations (ATIO) Conference held September 13 through 15 in 2010, in Fort Worth, Texas by the Northrop Grumman team followed in the Myth Merchant documentary. In his later life, Reimar Horten promoted the idea that the Horten Ho 229 V3 was intended to be built as a stealth aircraft, which would have placed this jet’s design several decades ahead of its time. Reimar Horten claimed that he wanted to add charcoal to the adhesive layers of the plywood skin of the production model to render it invisible to radar, because the charcoal “should diffuse radar beams, and make the aircraft invisible on radar” (Horten and Selinger 1983). This statement was published in his 1983 co-authored book Nurflugel (which translates as “only the wing”). While this statement refers to the never-made production model, it seems possible that the experimental charcoal addition could have been used on the Horten Ho 229 V3 prototype. The mere mention of early stealth technology sparked the imagination of aircraft enthusiasts across the world and spurred vibrant debate within the aviation community. The stealth myth has been growing since the 1980s and was invigorated when the National Geographic Channel, in collaboration with Northrup Grumman, produced a documentary called "Hitler's Stealth Fighter" in 2009. The program featured the Horten Ho 229 V3 as a potential "Wonder Weapon" that arrived too late in the war to be used (Myth Merchant Films, 2009). The documentary also referred to the jet's storage location as "a secret government warehouse," which added to the mystique of this artifact. Since the airing of the documentary, public pressure has increased to remove the jet from its so-called secret government warehouse and put it on display. In fact, this secret warehouse is the Museum's Paul E. Garber Facility in Suitland, Maryland where a team of conservators, material scientists, a curator, and aircraft mechanic has been evaluating the aircraft. The Smithsonian has performed a technical study of the materials used and determined that there is "no evidence of carbon black or charcoal in the Horten jet" thus invalidating the proposed mechanism for an essentially non-existent radar absorbent property as compared to the control sample of plywood used in the original testing. "The Ho 229 leading edge has the same characteristics as the plywood except that the frequency exactly match and have a shorter bandwidth. This indicates that the dielectric constant of the Ho 229 leading edge is higher than the plywood test sample. The similarity of the two tests indicates that the design using the carbon black type material produced a poor absorber." Dobrenz and Spadoni use the term 'absorber' to refer to the ability of the Ho 229 leading edge to absorb the radar signal rather than reflecting it back to the antenna receiver. More absorption means less reflected signal and greater stealth. The authors assumed in their paper that crafts persons used the "carbon black material" to lower the RCS, however, our technical study findings described above found no evidence of carbon black or charcoal in the Horten jet. Specifications (Horten Ho 229A (V3)) From manufacturer's estimates— General characteristics Crew: 1 Length: 7.47 m (24 ft 6 in) Wingspan: 16.76 m (55 ft 0 in) Height: 2.81 m (9 ft 2 in) Wing area: 50.20 m² (540.35 ft²) Empty weight: 4,600 kg (10,141 lb) Loaded weight: 6,912 kg (15,238 lb) Max. takeoff weight: 8,100 kg (17,857 lb) Powerplant: 2 × Junkers Jumo 004B turbojet, 8.7 kN (1,956 lbf) each Performance Maximum speed: 977 km/h (estimated) (607 mph) at 12,000 metres (39,000 ft) Service ceiling: 16,000 m (estimated) (52,000 ft) Rate of climb: 22 m/s (estimated) (4,330 ft/min) Wing loading: 137.7 kg/m² (28.2 lb/ft²) Thrust/weight: 0.26 Armament Guns: 2 × 30 mm MK 108 cannon Rockets: R4M rockets Bombs: 2 × 500 kilograms (1,100 lb) bombs. * |
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