Авиация

[karatik99]

Messerschmitt Me 334.
This design was originally intended to be turbojet powered, but due to the early unavailability of jet engines, Dr. Lippisch modified this aircraft to accept a Daimler Benz DB 605 12-cylinder piston engine. The wings were mounted mid-fuselage and were swept back at a 23.4 degree angle. The main landing gear retracted inwards and the front gear retracted to the rear. Intended armament was to be two MG 131 13mm machine guns. Further development was abandoned when Lippisch designed the P.20.

Span: 9.3 m (30' 6.4") Length: 7.0 m (22' 11.8") Max. Speed: Unknown

[karatik99]

Messerschmitt Me 509
Although the Me 509 can trace its roots back to the Me 309, very little information has survived. The aircraft was to be of an all-metal construction. A new fuselage was designed, with the pressurized cockpit being moved well forward near the nose. The Daimler Benz 605B 12-cylinder engine was buried in the fuselage behind the cockpit, and drove a three-bladed, Me P 6 reversible-pitch propeller by an extension shaft which passed beneath the cockpit (similar to the US Bell P-39). The wing was tapered and had rounded wingtips, and was mounted low on the fuselage. Other Me 309 components were to be used, such as the tricycle landing gear, and the vertical tail assembly was similar to the one used for the Me 309 V1. Armament was not decided upon for the 509, but it is thought that two MG 131 13mm machine guns and two MG 151 20mm cannon were to be used. Although there were advantages of better cockpit visibility and relocation of the engine weight from the nose gear (important, since the Me 309's nose gear often collapsed), the Me 509 design and development was stopped when the Me 309 program was ended in mid-1943.
In April 1945, the Japanese completed a very similar project, the Yokosuka R2Y Keiun. Although no firm evidence exists, it is possible that the Me 309/509 information was licensed to the Japanese military, as were a number of other German designs (Bf 109, He 100, Me 163, Me 410, among others).
The Yokosuka R2Y Keiun, which was built for the Japanese Navy use, was an aircraft very similar in design to the Messerschmitt Me 509. Its first flight was in May 8, 1945, and was cut short due to engine overheating, a problem that probably would have also faced the Me 509.


Messerschmitt Me 509 Dimensions *
Span 11.27 m (37' 0")
Length 9.94 m (32' 7")
Height 3.98 m (13' 1")
* All dimensions approximate., no weights or performance data available

[Botya]

Гена есть ли у тебя материалы по Не-219?

[karatik99]

Messerschmitt Me 609
In 1941, the RLM issued a requirement for a new Zerstörer (destroyer, or heavy fighter), which called for a new design that would use components from existing aircraft, thus not disrupting existing production. After the cancellation of the Me 309 project in 1943, work was continued using it as a basis for other designs. One of these reworked designs was for the Me 509; another was for the 609, which was basically two Me 309 fuselages joined with a new center wing section. Messerschmitt was also working on and had completed a twin-fuselage Bf 109, known as the Me 109Z, but it was destroyed before flight testing.
Two Me 309 fuselages were to be joined with a constant chord center wing section, into which the two inboard landing gear retracted. The two outboard landing gear retracted outwards in to the outer wing sections, with the two nose wheels retracting to the rear and rotating 90 degrees to lie flat beneath the engines. Power was to be supplied by two Daimler Benz 603 or 605 12 cylinder inverted V liquid -cooled engines. The pilot sat in a cockpit located in the port fuselage, with the starboard cockpit canopy being faired over.
Two versions were envisioned: a heavy fighter and a high-speed bomber. In the fighter version, two MK 108 30 mm cannon and two MK 103 30mm cannon were projected as the armament, with a provision for two additional MK 108 30mm cannon mounted beneath the center wing section or under the outer wing sections. In addition, either one SC 500 or two SC 250 bombs could be carried, also beneath the center wing section. The bomber version would have reduced armament, with only two MK 108 30mm cannon were to be installed. Extra fuel (1500 kg) could be carried in the faired over starboard cockpit, and the bomb load was to consist of two SC 1000 bombs which were carried beneath each fuselage.
Even though it was calculated that many components of the 309 could be used (fuselage, engines, equipment, 80% of the wings), by the time this design began to jell, the Me 262 jet fighter was proving to be the plane of the future, and could take over all roles for which the Me 609 was designed. Thus, the Me 609 project was no longer pursued after 1944.

Messerschmitt Me 609 Data
Span 15.75 m (52' 6")
Length 9.72 m (31' 11")
Height 3.43 m (11' 3")
Empty Weight 5247 kg (11660 lbs)
Loaded Weight 6534 kg (14520 lbs)
Max. Speed 760 km/h (472 mph)

[karatik99]

Гена есть ли у тебя материалы по Не-219?

Слава, дома есть только картинки рисованые, надо на работе в компе посмотреть...

[Botya]

Слава, дома есть только картинки рисованые, надо на работе в компе посмотреть...

Просто у меня эта машина уже лет пять не может сделаться.... Больной вопрос - носовая стойка шасси - нутрянки не найду никак...

[karatik99]

Просто у меня эта машина уже лет пять не может сделаться.... Больной вопрос - носовая стойка шасси - нутрянки не найду никак...

только такая... посмотрю на работе...

[karatik99]

Messerschmitt Me P.08.01




In early 1939, Dr. Alexander Lippisch moved to the Messerschmitt Aircraft Company in Augsburg with most of his closest coworkers. Dr. Wurster designed the P.08.01 in September 1941, which was basically a flying wing design. The wing featured two different sweepback angles, and contained the armored fuel tanks. The fuel could also be jettisoned if need be. Four Daimler Benz DB 615 engines (or DB 613 if teh DB 615 engines were not ready in time), mounted on the wing trailing edge, provided the power. The engine radiators were located in the wing's leading edge and a huge bomb bay/cargo area was to be found in the central fuselage area. A tricycle landing gear arrangement was chosen, with the main gear having double wheels. The cockpit was pressurized and a provision was made for remote controlled defensive armament in the nose and tail. Underwing weapons or loads could also be carried. The P.08.01 was designed as per a specification for a super heavy aircraft that could fulfill several different roles. These included:

• Long range bomber with a bomb load of 20000 kg (44092 lbs) and a range of 15000 km (9321 miles)
• Maritime patrol aircraft with a bomb load of 20000 kg (44092 lbs) of radio-controlled glide bombs, mines or torpedoes
• Tactical bomber with 50000 kg (110230 lbs) and a range of 2500 km (1554 miles)
• Long range reconnaissance aircraft with a range of 27000 km (16778 miles)
• Tactical or strategic wide-body transport with a provision to carry at least a 25 ton tank or an equivalent amount of equipment
• Tow aircraft for transport gliders up to 100000 kg (220460 lbs) flying weight
• Flak carrier aircraft for four 88mm flak cannons

Messerschmitt Me P.08.01 Data
Span 50.6 m
Length 15.35 m
Height 8.6 m
Wing Area 300 m²
Takeoff Weight 90000 kg
Max. Speed 645 km/h / 8500 m
Max. Range 27150 km
Fuel 40000 kg

[Botya]

только такая... посмотрю на работе...

Добро -жду!

[karatik99]

Messerschmitt Me P.1092A-E
Beginning in May 1943, a series of aircraft were designed under the Me P.1092 designation. Meant to fill a role as a multi-purpose aircraft, five basic designs were submitted:
· Me P.1092A - fighter with one turbojet
· Me P.1092B - interceptor with one rocket engine
· Me P.1092C - high-speed bomber with two pulse jets
· Me P.1092D - heavy fighter with two turbojets
· Me P.1092E - two-seat nightfighter/ heavy fighter
· other designs included roles for long-range fighters, torpedo bombers and dive bombers
The first design, the Messerschmitt Me P.1092A, was a small plane. A single Jumo 004C turbojet was mounted on the bottom of the fuselage and was fed by an air intake beneath the nose of the fuselage. The wings, which were basically the outer wing sections from the Me 262, exhibited a small amount of sweepback (approximately 22 degrees) and were mounted mid-fuselage. A V-Tail (or butterfly tail), provided lateral control, and a tricycle landing gear arrangement was chosen. The main landing gear were located about halfway outboard on the wings and retracted inwards. One possible problem would have been the front landing gear, which would have blocked the air intake on takeoff and landing. A single pilot sat in a cockpit located in the middle of the fuselage, and afforded excellent all-around vision. Armament consisted of two MK 103 30mm cannon in the aircraft's nose.
The Me P.1092B was to be an interceptor. It was similar in appearance to the Me P.1092A, with the main exception of the propulsion method. Whereas the P.1092A used a Jumo turbojet, the P.1092B had a rocket motor (probably a Walter HWK109-509A rocket engine) located in the rear fuselage. Six fuel tanks filled most of the fuselage; three held 600 liters, two held 350 liters and one held 230 liters. The tail unit and landing gear was also similar to the P.1092A, but the armament was upgraded to two MK 103 30mm cannon and two MK 108 30mm cannon.
Although none of the Me P.1092A-E designs went any further than the drawing board, a whole new series of designs (also under the P.1092 designation) were begun just a few months later.
Messerschmitt Me P.1092A Data
Span8.4 m
Length 9.0 m
Height 2.5 m
Wing Area 12.0 m²
Loaded Weight* 4000 kg
Max. Wing Loading 330 kg/m²
* Approximate, with 1200 liters (263 gallons) of fuel

Messerschmitt Me P.1092B Data
Span 8.4 m
Length 9.0 m
Height 2.5 m
Wing Area 12.0 m²
Fuselage Width1.35 m
Main Track Width3.28 m