Интересные фотки XII

http://www.pr.erau.edu/~aiaa-erau/past/Edwards98/Lim6_01.jpg [not image]

http://www.pr.erau.edu/~aiaa-erau/past/Edwards98/B17_01.jpg [not image]


http://www.pr.erau.edu/~aiaa-erau/past/Edwards98/N9MB_01.jpg [not image]

V se delo v minutah

Самолет на последней фотке напоминает B-2. Или если быть точнее, то самолет больше напоминает немецкий прототип времен конца Второй мировой войны - Go-229. Если нужно, то могу картинку последнего заслать.

Фотку присылай для комплекта.
А это первый портотип В-2.

He P.1078

http://www.geocities.com/Heartland/Village/4082/model2/p1078bi.jpg [not image]
http://www.geocities.com/Heartland/Village/4082/model2/p1078bii.jpg [not image]

wbr, muxel

Я нашел всего несколько картинок, пришлю их KRoNу по мылу. Вот смотришь на эти картинки и понимаешь, что немцы в своих разработках сильно опередили то время.

http://visi.net/~djohnson/gotha/3bgp60a.jpg [not image]


Since Gotha had taken over building and development of the two-seat radar equipped Ho IX flying wing from Horten, the development section of Gotha decided to try their hand at designing similar projects. The P.60 was proposed as a three-piece, arrowhead-shaped flying wing with jets mounted above and below the rear fuselage along the centerline. The P.60A fighter was the first design, and since there was practically no fuselage, the two man crew were positioned prone side-by-side behind the glassed in nose. Steering was accomplished by eight small vertical vanes near the wingtips. Two BMW 003A jet engines were proposed, and armament was to be four MK 108 30 mm cannon.

Span: 12.41 m (40' 9") Length: 9.5 m (31' 2.25") Max. speed: 953 km/h (592 mph)

http://visi.net/~djohnson/gotha/p60acut.jpg [not image]


This view shows to advantage the pilot's prone position, which helps to alleviate G force stresses.



http://visi.net/~djohnson/gotha/3bgp60c.jpg [not image]

This was the final design of the Gotha Go P.60 series, the P.60C nightfighter. There seems to be some confusion as to which engines were to be installed, two HeS 011 or two BMW 003 turbojets. The fuselage was lengthened again, to accommodate the installation of a radar set and its "Morgenstern" (Morningstar) antenna. Again, armament was to be four MK 108 30mm cannon. The end of the war prevented further development.

Span: 13.51m (44' 4.3") Length: 10.9 m (35' 9.5") Max. Speed: 960 km/h (596 mph)

http://visi.net/~djohnson/gotha/p60ccut.jpg [not image]
The arrangement of the crew and radar are shown in this cutaway drawing. Although the radar antenna was supposed to be the "Morningstar", the FuG 240 "Berlin" antenna is pictured.

http://visi.net/~djohnson/gotha/3bgp60b.jpg [not image]

The Gotha Go P.60B was a further development of the P.60 series which simplified construction by utilizing a simplier airframe and a conventional rudder. The two-seat cockpit was located behind the radio equipment in a fuselage section which projected forward from the wing leading edge. Two engines were upgraded to the HeS 011 turbojets, and like the Go P.60B, four MK 108 30mm cannon were to be the armament. The RLM approved the construction of the project in 1945, but later construction of the prototype was halted in midwork in favor of the Go P.60C.

Span: 13.5 m (44' 3.9") Length: 9.9 m (32' 6") Max. Speed: 973 km/h (604 mph)

BMW

http://visi.net/~djohnson/bmw/3bbbmw2.jpg [not image]

BMW designed this bomber as a flying wing. Two BMW 018 turbojets rated at 3450 kp (7590 lbs/thrust) were to be mounted beside one another in the rear of the aircrft and fad by an air intake duct running through the fuselage. The bombardier was to be prone in a ventral armored compartment to provide optimal visibility during bombing runs. Two machine cannon were planned for installation in a remote controlled rear turret, to be operated from the navigator's position. The bomb load was 5000 kg (11000 lbs).

http://users.visi.net/~djohnson/heinkel/3bh1079b.jpg [zero size or time out]

The second design of the He P.1079 was closer to a flying wing layout, although there was a single, vertical fin which replaced the V-tail of the P.1079A. The wings were gull-shaped and were swept back at 45 degrees. This version of the P.1079B all-weather heavy fighter project was to be a single seater. Like the P.1079A, the two HeS 011 turbojets were located in the wing roots and the armament was four MK 108 30mm canon.

Span: 13 m (42' 8.2") Length: 9 m (29' 6.6") Max. Speed: 1015 km/h (630 mph)


[img=http://users.visi.net/~djohnson/heinkel/3bh1078b.jpg]

This second design of the He P.1078 was a tailess, single-seat fighter that had a somewhat unusual cockpit arrangement. The cockpit was located in a gondola on the port side, and another gondola containing three MK 108 30mm cannon and radar was located on the starboard side. An air intake feeding the single HeS 011 turbojet was located between the two gondolas. Like the He P.1078A, the gull wings were swept back at 40 degrees.


Span: 9.43 m (30' 11.5") Length: 6.04 m (19' 10") Max. Speed: 1025 km/h (636 mph)


[img=http://users.visi.net/~djohnson/heinkel/3bh1079c.jpg]

This was the second design (Entwurf II) for the He P.1079B all-weather heavy fighter. The wings were swept back sharply and contained six fuel tanks. Two He S 011 jet engines were located in the wing roots and were fed by intakes in the wing leading edges. A crew of two sat back-to-back in the cockpit, and armament was to be four MK 108 30mm cannon. No evidence has been found that the P.1079 projects were ever submitted to the RLM, but it is known that designer Siegfried Gьnter, along with his engineers Eichner and Hohbach, were working on these designs under U.S. supervision during the summer of 1945.

Span: 13.13m (43' 1.5") Length: 9.48 m (31' 1.5") Max. Speed: 1015 km/h (630 mph)


[hr]


This cutaway drawing of the He P.1079B/II shows the location of the wing fuel tanks, engine positions and other components.....

[img=http://users.visi.net/~djohnson/heinkel/1079ccut.jpg]

Image from ReichDreams Dossier #15, Bats, by J. Miranda & P.Mercado

[img=http://visi.net/~djohnson/junkers/3bj130.jpg]

The Junkers EF.130 was designed at the same time as the Ju EF.128. This flying wing design was powered by four BMW 003 turbojets mounted side-by-side above the ventral trailing wing edge. The construction was to be of metal, with wooden outer wing sections. A small glazed pressurized cockpit was located in the extreme nose for a two or three man crew. Landing gear was to be of a retractable tricycle arrangement, and no defensive armament was known to have been fitted. A bomb load of 2950 kg (6490 lbs) was to be carried.


Span: 24 m (78' 9.6") Length: 11 m (36' 1.4") Max. Speed: 990 km/h (615 mph)

Чуть позже еще фотки модели добавлю.