Type | Aircraft | |
Company | Société des Avions Marcel Bloch | |
Scheme | Low wing Monoplane | |
Geometry | ||
---|---|---|
Length (m) |
1.9
12.2
88.7
|
|
Height (m) |
0.6
3.6
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
38
925
|
|
Wingspan (Beam) (m) |
0.1
17.9
95
|
|
Weights | ||
Empty weight (kg) |
8
5,612
276,800
|
|
Loaded weight (kg) |
5
7,160
242,500
|
|
Capacity | ||
Crew (per.) |
1
3
112
|
|
Speeds | ||
Max. Speed (km/h) |
25
530
28,165
|
at 5200 m |
Сruise Speed (km/h) |
52
460
3,087
|
at 4000 m |
Power | ||
Total Power (hp) |
0.4
2,070
60,000
|
2 powerplants 1035 hp each |
Performance | ||
Service ceiling (m) |
0.6
11,000
161,544
|
|
Range (Ferry range) (km) |
4
1,650
40,700
|
|
Сombat radius (km) |
277
1,290
7,210
|
|
Dynamic Performance | ||
Time to altitude (min) |
0.6
11
105
|
to 8000 m |
Combat | ||
Guns (qt) |
1
7
18
|
2 × fixed, forward-firing 7.5 mm (.295 in) MAC 1934 machine guns in the wings; 2 × 7.5 mm (.295 in) MAC 1934s in the dorsal position; 3 × 7.5 mm (.295 in) MAC 1934s on aft-firing mounts |
Bombs (qt) |
1
8
250
|
50 kg bombs |
Stat | ||
Introduction | 01.03.1940 | |
First flight | 01.07.1939 | |
Stop production | 1950 |