While the Junkers Ju 252 had proven itself the expected improvement over the original Ju 52 tri-motor transport, it arrived at a time when the German war effort was in full swing. Restrictions on use of war material meant that only fifteen of the Ju 252 would see the light of day as attention shifted to development of the Ju 352 "Herkules" of similar form and function - though using far less needed war material in its construction.
Design of the Ju 352 came directly from German Air Ministry authorities who understood the value of the preceding Ju 252 but not its total material commitment. Junkers was approached in early 1942 just as the Ju 252 program was picking up steam. Much of the metalworks of the Ju 252 was replaced by wood and the important Junkers Jumo 211F engines were given up for the readily available BMW Bramo 323R radial instead. The wing mainplanes were shifted further aft as the aircraft began to take on something of an all-new appearance when compared to the original Ju 252. The powered rear loading ramp featured in the Ju 252 - which leveled the aircraft fuselage by raising the rear off its tailwheel support - was retained in the Ju 352. Defensive armament would become 1 x MG 151 cannon fitted to a dorsal turret as well as 2 x MG 131 machine guns at beam positions (one unit per window).
First flight of a prototype occurred on August 18th, 1943 and ten pre-production aircraft were ordered and built. This was followed by thirty-three production-quality Ju 352A models until the German attention was off of transport types and onto fighters and more advanced jet-powered aircraft. Just fifty Ju 352s were competed in all. One was built by Letov in the post-war years for the Soviet Union and another operated with the Czech Air Force.
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Czechoslovakia (post-war); Nazi Germany; Soviet Union
(OPERATORS list includes past, present, and future operators when applicable)
✓Transport
General transport functionality to move supplies/cargo or personnel (including wounded and VIP) over range.
Length
80.7 ft (24.60 m)
Width/Span
112.2 ft (34.20 m)
Height
18.8 ft (5.74 m)
Empty Wgt
27,558 lb (12,500 kg)
MTOW
43,211 lb (19,600 kg)
Wgt Diff
+15,653 lb (+7,100 kg)
(Showcased structural values pertain to the Junkers Ju 352A (Herkules) production variant)
Installed:
3 x BMW Bramo 323 R-2 Fafnir 9-cylinder radial piston engines (one in nose and one at each wing) developing 986 horsepower and 1,184 horsepower.
(Showcased performance specifications pertain to the Junkers Ju 352A (Herkules) production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
OPTIONAL:
1 x 15mm MG 151 cannon in dorsal turret
2 x 13mm MG 131 heavy machine guns in waist positions.
Supported Types
(Not all ordnance types may be represented in the showcase above)
Hardpoint Mountings: 0
Ju 352 - Base Series Designation
Ju 352A - Main production model
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.
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Czechoslovakia (post-war); Nazi Germany; Soviet Union
