VEB (Baade) 152
1958
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VEB (Baade) 152

The political ambition of the East German politburo and the cancellation of the Alekseyev 150 Soviet bomber project led to the return to East Germany in 1953 of a group of German engineers and scientists deported to Russia in 1945. They were sponsored to proceed with one of the many commercial designs that they had formulated while in Russia. One of these was the 152 airliner, which was based on their experience with the Alekseyev 150 and would be powered by a development of the Junkers Jumo turbojet engine named Pirna 014. The prototype had a glazed nose and an unusual undercarriage arrangement featuring a single central gear assisted by wingtip pod-mounted outriggers. Late availability of the Pirna engines meant the prototype first flew with Tumansky Rd-9b engines. On its second flight, while rehearsing for the Leipzig trade fair, the prototype 152 crashed due to pressure equalization problems between the multifarious tanks and the inadequate engines. The second heavily modified (152A) model (with modified tanks, conventional undercarriage and a glazed nose) flew twice more before the project was cancelled in 1961 due to national economic crises which were exacerbated by the defection of key design team members.

VEB (Baade) 152


Specification 
 MODELVEB 152
 CREW4-5
 PASSENGERS58
 ENGINE4 x 3165kg VDL Pirna 014A-1 turbojets
 WEIGHTS
    Take-off weight46500 kg102515 lb
 DIMENSIONS
    Wingspan25.40 m83 ft 4 in
    Length31.30 m102 ft 8 in
    Height9.70 m31 ft 10 in
 PERFORMANCE
    Max. speed920 km/h572 mph
    Range2500 km1553 miles

3-View 
VEB (Baade) 152A three-view drawing (1378 x 708)

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FACTS AND FIGURES

© The lack of space, poor engines and the bomber's wing meant small payloads and short ranges as well as a low speed for a jetliner.

© The Model 150 bomber had two large Lyul'ka engines, but the VEB 152 had four much weaker engines (a version of that used in the MiG-19), which gave poor thrust for their weight and high fuel consumption.

© The potential baggage space was reduced by the main landing gear wells and the cabin ceiling was obstructed by the large wing box.

© With its bicycle main gear and outrigger wheels the 152 needed to be landed very precisely.



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