  
         The third prototype, Ju 352V3
         The tremendous success 
         of the pre-war Ju 52/3m airliner naturally led Junkers to look for a 
         successor, and after several designs settled on the Ju 252. However, 
         the Ju 252 was a metal aircraft and the raw materials were in short 
         supply for transport aircraft, as were the Jumo 211F engines. In order 
         to redress this, Junkers began design of a wooden version powered by 
         three 1,000 hp (746 kW) BMW-Bramo 323R-2 radials in the spring of 1942. 
         The resultant Ju 352 superficially resembled the Ju 252, but the wooden 
         wing was mounted further back on the fuselage, which itself was a 
         composite structure. It was marginally larger than the Ju 252 but 
         easily distinguished by its squared tail fin rather than the rounded 
         one of the Ju 252. Incorporated in the rear was the Trapoklappe, 
         a hydraulically-powered loading ramp which allowed the rapid loading of 
         bulky items, although vehicles were usually winched up the ramp rather 
         than driven. A detachable tailcone could be replaced by a towing hook 
         for gliders. Defensive armament consisted of a single 20 mm MG 151/20 
         cannon in a HD 151/2 power operated turret behind the cockpit. 
         Provisions were made for two 13 mm (0.51 in) MG 131 machine-guns in the 
         beam positions. 
         
           
         Dubbed the 'Herkules' 
         by the manufacturer, the Ju 352 V1 made its first flight on 1 October 
         1943, from the satellite plant at Fritzlar. The V2 second prototype 
         flew soon after, and an order for 10 pre-production Ju 352A-Os came 
         quickly. Production Ju 352A-ls were delivered to the Luftwaffe from 
         February 1944, but by the summer the worsening war situation led to the 
         cancellation of transport aircraft production. A total of two 
         prototypes, 10 Ju 352A-0s and 33 Ju 352A-ls were completed. 
         In service, the type 
         showed itself a worthy successor to the Ju 52/3m, proving rugged and 
         reliable. The wooden propellers featured reverse pitch, which was 
         appreciated greatly by crews, considerably reducing the landing run by 
         up to 60 percent. The aircraft were assigned to various transport units 
         for special missions, with most going to the infamous I./KG 200 
         (commanded by Major Gunther Mauss). Most ended up with the 
         Grossraum-Transportgruppe at Tutow, although only a few supply missions 
         were flown towards the end of the war. On 25 April 1945, 23 were still 
         on strength but most were destroyed as the Allies neared the airfield. 
         At least two escaped 
         the destruction, one being captured by the British and ferried to RAF 
         Farnborough for evaluation. The other surfaced after the war in 
         Czechoslovakia, where it was restored and presented as a personal gift 
         from the Czech government to Josef Stalin. Developments were planned, 
         including the Ju 352B with 1,800 hp (1343 kW) BMW 801 radial engines, 
         although none left the drawing board.  
         
           
         The company Logo for Junkers Flugzeug un Motorenwerke AG founded by 
         Hugo Junkers 
         Specifications (Junkers 
         Ju 252A-1 Herkules "Hercules") 
         Type: General 
         Purpose Transport  
         Crew: Three or 
         Four depending on loadout  
         Design: Junkers 
         Flugzeug un Motorenwerke AG Design Team  
         Manufacturer: 
         Junkers Flugzeug un Motorenwerke AG from a satellite plant at Fritzlar
          
         Powerplant: 
         Three BMW-Bramo 323R-2 Fafnir 9-cylinder air-cooled radial engines 
         rated at 1,000 hp (746 kW) for take-off and 1,200 hp (895 kW) with 
         water-methanol injection. 
         Performance: 
         Maximum speed 230 mph (370 km/h); service ceiling 19,685 ft (6000 m). 
         Range: 1,860 
         miles (2995 km) with maximum payload. 
         Weight: Empty 
         28,150 lbs (12769 kg) with a maximum take-off weight of 43,200 lbs 
         (19595 kg). 
         Dimensions: Span 
         112 ft 2 3/4 in (34.21 m); length 80 ft 8 1/2 in (24.60 m); height 18 
         ft 10 1/3 in (5.75 m); wing area 1,379.93 sq ft (128.19 sq m). 
         Armament: One 20 
         mm MG 151/20 cannon in a HD 151/2 power operated turret behind the 
         cockpit with provisions for two 13 mm (0.51 in) MG 131 machine-guns in 
         the beam positions. 
         Variants: Ju 352 
         V1, Ju 352 V2, Ju 352A-0 (10 pre-production aircraft), Ju 352A-1 (33 
         production aircraft). 
         Avionics: None. 
         History: First 
         flight (Ju 352 V1) 1 October 1943. 
         Operators: 
         Germany (Luftwaffe).  |