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Specifications (Do 217 M-1)[edit]
General characteristics
Crew: 4
Length: 17.00 m (55 ft 9 in)
Wingspan: 19.00 m (62 ft 4 in)
Height: 4.96 m (16 ft 3 1⁄2 in)
Wing area: 57.00 m2 (613.54 ft2)
Empty weight: 9,100 kg (20,062 lb)
Max. takeoff weight: 16,700 kg (36,817 lb)
Powerplant: 2 × DB 603A 12-cylinder inverted-vee engine, 1,750 PS (1,726 hp, 1,287 kW) each
Performance
Maximum speed: 557 km/h at 5,700 m (347 mph at 18,700 ft)
Cruise speed: 400 km/h (248 mph)
Range: 2,145 km (1,332 mi)
Service ceiling: 7,370 m (24,180 ft (with max bombload))
Rate of climb: 210 m/min (688 ft/min)
Armament
4 × 7.92 mm (.312 in) MG 81 machine guns in nose and lateral positions
2 × 13 mm (.51 in) MG 131 machine guns in dorsal and ventral positions
Max Load 4,000 kilograms (8,800 lb) internally externally.
Max Internal Load 3,000 kilograms (6,600 lb).
Specifications (Ju 188E)[edit]
General characteristics
Crew: 5
Length: 15 m (49 ft 1 in)
Wingspan: 22 m (72 ft 2 in)
Height: 4.4 m (14 ft 7 in)
Wing area: 56 m² (603 ft²)
Empty weight: 9,900 kg (21,825 lb)
Loaded weight: 14,500 kg (31,967 lb)
Powerplant: 2 × 1 BMW 801 G-2, 1,700 PS (1,250 kW) each
Performance
Maximum speed: 499 km/h (310 mph)
Range: 2,190 km (1,360 mi combat)
Service ceiling: 9,500 m (31,170 ft)
Wing loading: 258.9 kg/m² (53.0 lb/ft²)
Power/mass: 0.175 kW/kg (0.106 hp/lb)
Armament
Guns: 1 × 20 mm MG 151/20 cannon
3 × 13 mm (.51 in) MG 131 machine gun
Bombs: 3,000 kg (6,612 lb)
In terms of capabilities the Do-217 seems to have had greater potential than the later Ju-188, despite the latter's adaptability and easier conversion of the existing production lines. What arguments are their for the Ju-188 over the Do-217 as a medium bomber if any (other than ease of converting existing Ju-88 production lines)?
https://en.wikipedia.org/wiki/Dornier_Do_217#Specifications_.28Do_217_M-1.29
https://en.wikipedia.org/wiki/Junkers_Ju_188#Specifications_.28Ju_188E.29
With much heavier engines that didn't work properly. Also the 317 didn't first fly until 1943 and was a development of the Do217. It was a later design than the two types in question and not part of this discussion for that reason.Real bomb bay. Do-317 version also had a lot more engine power which translates into greater range / payload.
Ju-188 entered service during 1943 and it's a variant of the Ju-88. In both cases were are talking about aircraft (Do-217/Do-317 and Ju-88/Ju-188) which entered (or could have entered) service during 1943 and shared components with an earlier aircraft.
Was the Do217 cruise speed that much better? I cannot find it anywhere online.Eric Brown's Do-217 flight description suggests he was expecting fighter aircraft performance. Not surprisingly, Do-217 medium/heavy bomber aerial performance didn't compare well. If comparison had consisted of placing 3,000kg of ordnance on a target 500 miles away with a high cruise speed then Do-217 performance starts to look a lot better.
Eric Brown's Do-217 flight description suggests he was expecting fighter aircraft performance. Not surprisingly, Do-217 medium/heavy bomber aerial performance didn't compare well. If comparison had consisted of placing 3,000kg of ordnance on a target 500 miles away with a high cruise speed then Do-217 performance starts to look a lot better.
October 1945 British Captain Eric Brown undertook full handling trials with a Do 217 M-1 WNr 56158 at RAF Farnborough. He recalled a distinctly "underwhelming" experience.[99] Brown recalled that he took off with full power of some 2,700 rpm and the lightly loaded Do 217M left the runway at 160 km/h (99 mph). Brown held a shallow climb, waiting to reach 200 km/h (120 mph) before retracting the undercarriage. Brown timed the time it took to retract, which was between 30 and 40 seconds.[99] At 150 m (490 ft) he reduced power to 2,500 rpm and raised the flaps at about 230 km/h (140 mph). With the flaps up a climbing speed of 230 km/h (140 mph) was established giving a rate of "very moderate proportions".[