Type | Aircraft | |
Company | Blériot Aéronautique | |
Scheme | Midwing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
14.7
88.7
|
|
Height (m) |
0.6
3.4
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
88
925
|
|
Wingspan (Beam) (m) |
0.1
23.2
95
|
|
Weights | ||
Empty weight (kg) |
8
3,750
276,800
|
|
Loaded weight (kg) |
5
4,966
242,500
|
|
Capacity | ||
Crew (per.) |
1
4
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
199
28,165
|
|
Сruise Speed (km/h) |
52
168
3,087
|
|
Power | ||
Total Power (hp) |
0.4
1,100
60,000
|
2 powerplants |
Performance | ||
Service ceiling (m) |
0.6
7,450
161,544
|
|
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
321
36,000
|
|
Combat | ||
Guns (qt) |
1
4
18
|
2 × forward trainable Lewis guns in nose; 2 × rearward trainable Lewis guns in each of two engine nacelles |
Bombs weight (kg) |
2
1,000
39,000
|
of bombs carried in internal bay |
Stat | ||
Number built (qt) |
0
44
43,000
|
|
Introduction | 1926 | |
First flight | 07.05.1926 | |
Stop production | 1934 |