Do-24K-1 (first 12, in the reconnaissance role) | |
Wingspan: | 27,00 meter |
Length: | 21,95 meter |
Height: | 5,75 meter overall
including rotating propellers 2,10 meter, only fuselage, including cockpit |
Fuselage width | 3,00 meter 7,40 meter with Stummeln |
Surface area's | 108 mē overall,
including ailerons and flaps Stabilo 18,44 mē Rudders 9,10 mē Flaps 8,75 mē |
Wing angles |
4½ degrees swept back in the middle 4½ degrees swept back at the ends 3½ degrees V at the back of the wings |
Fuel | 8 Stummel tanks (2670 liter) and 2 wing tanks (1880 liter) totaling 4550 liter |
Oil | 3 tanks totaling 390 liter |
Engine | Three x Wright Cyclone GR 1820-F52 |
Propellers | Hamilton Type 3E 50-31, metal, constant speed, 3,50 meter diameter, 3 per engine |
Speed |
Maximum 280 km/h at sea level with 3 x 745 hp at 2100 rpm. Maximum 305 km/h at 1770 meter with 3 x 760 hp at 2100 rpm. Cruise 205 km/h at sea level with 3 x 372 hp, weighing 11000 kg Cruise 220 km/h at 1770 meter with 3 x 380 hp, weighing 11000 kg Landing 108 km/h |
Fuel consumption |
215 gr/hp at cruise speed at sea level 215 gr/hp at cruise speed at 1770 meter |
Ceiling | 5600 meter |
Climb time |
To 1000 meter in 3 minutes 30 seconds To 2000 meter in 6 minutes 45 seconds To 3000 meter in 10 minutes 45 seconds To 4000 meter in 16 minutes 30 seconds To 5000 meter in 27 minutes 30 seconds |
Range |
1270 km at sea level at cruise speed without wind factor 1340 km at 1770 meter at cruise speed without wind factor |
Weight |
Empty 7695 kg fixed equipment 660 kg variable equipment 345 kg Empty (equipped) 8970 kg crew 480 kg fuel 0-2725 kg oil 0-190 kg ammunition 0-35 kg Take-off 12400 kg Maximum 13500 kg |
Take-off run |
17 seconds 85 seconds without middle engine at 12400 kg weight 64 seconds without middle engine at 11500 kg weight 76 seconds without one of the outboard engines at 10000 kg weight |
Crew | 5 |
Armament | Three Colt-Browning 7,7 mm machineguns with 500 rounds each. |