In mid-1944, Junkers inherited the Dornier 335Z long-range reconnaissance
(Z for Zwilling, or twin) program from Heinkel, who were brought in to
assist Dornier because they lacked the experience in building such aircraft.
After meeting with engineers from Dornier and Heinkel, Professor Heinrich
Hertel decided that it would be late 1945 before the first prototype of
the Do 335Z would be ready. He then referred back to Project 1075.01-21/W
00304, which would involve a lot less redesign and modification, and gave
the date of Febuary 1945 for the first prototype to be ready. After a few
more modifications (new main wheels, lengthened fuselages and an increased
center wing both in chord and length), the RLM authorized the use of the
635 number, thus becoming the Ju 635. A purchase order for four prototypes
and six preproduction aircraft was received.
The Ju 635 used two modified Do 335
fuselages, joined by a center wing section of constant chord. The outer
wing panels were tapered back, and two 1200 liter drop tanks could be carried
beneath the wings to increase range. Four Daimler Benz 603E-1 engines supplied
the power, one in each forward fuselage pulling and two in each rear fuselage
driving a pusher propeller via a long drive shaft. Fuel was to be carried
in ten internal wing tanks (see diagram below), four in the fuselages and
possibly one in each fuselage bay. The port fuselage bay carried the two
Rb 50/30 cameras (or one camera and one 250 liter (66 gallon) tank for
GM 1 power boost) and the starboard bay contained five 60 kg (132 lbs)
marker bombs. A crew of three was envisioned, although this could be stretched
to four eventually. The pilot and radio operator sat in the port fuselage
and a second pilot sat in the starboard fuselage. The fourth crew member
(navigator) was to also sit in the starboard fuselage. The landing gear
was to consist of two nose wheels (one under each fuselage nose), two main
wheels which were fitted with mud guards to protect the rear radiator intakes,
and a jettisonable fifth wheel located beneath the center wing, which was
fitted with a parachute for recovery. The main wheels were modified from
the Ju 352 B-1 transport's wheels. Two Walter RATO (Rocket Assisted
Take Off) units could be fitted to assist take off. A variety
of radars were to be fitted also, and no armament was included due to the
fact that this was a long-range reconnaissance aircraft and thus all weight
was reserved for fuel and speed.
Near the end of 1944, the German government
approached the Japanese about certain aircraft designs, the Ju 635 among
them. Although they were impressed with the Ju 635's capabilities, and
were interested in the project, nothing came of the meeting. By early 1945,
windtunnel models had been tested and cockpit mockups had been constructed
(see photos below), but by Febuary 5, due to the worsening war situation,
all further work on the Ju 635 was stopped.
Span: 27.45 m (90' 0")
Length: 18.5 m (60' 8.3")
Max. Speed: 720 km/h (447 mph)
This diagram shows the location of
the internal fuel tanks located within the Ju 635's wing and fuselage....
Photos of the Ju 635 cockpits mockups, January 1945 |
Two different artist impressions of the Ju 635
in flight....
All pictures on this page from the Monogram Monarch #2,
Dornier 335 Arrow