Type | Aircraft | |
Company | Junkers Flugzeug- und Motorenwerke AG | |
Scheme | Monoplane Low wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
16.5
88.7
|
|
Height (m) |
0.6
6
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
102
925
|
|
Wingspan (Beam) (m) |
0.1
30.5
95
|
|
Weights | ||
Empty weight (kg) |
8
5,250
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
8,500
575,000
|
|
Loaded weight (kg) |
5
8,500
242,500
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
one radio operator and one steward |
Capacity passengers (per.) |
1
15
400
|
15 day passengers or 10 night passengers |
Speeds | ||
Max. Speed (km/h) |
25
210
28,165
|
|
Сruise Speed (km/h) |
52
170
3,087
|
|
Power | ||
Total Power (hp) |
0.4
1,575
60,000
|
3 powerplants |
Performance | ||
Service ceiling (m) |
0.6
4,400
161,544
|
|
Range (Ferry range) (km) |
4
850
40,700
|
|
Endurance (h) |
0.0
5
150
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
180
36,000
|
|
Stat | ||
Number built (qt) |
0
13
43,000
|
|
Introduction | 1926 | |
First flight | 1926 |