|
Type |
B
IV 2-seated sportplane developed from the B II |
B
IVa 2-seater developed for record attempts |
|
Enginen |
1
Wright L4 |
1
Wright L4 |
|
Dimensions |
Length 6.25 m, span 9.15 m, wing area 11.20 m2, aspect ratio 7.5 |
Length 6.25 m, span 9.00 m, wing area 11.20 m2, aspect ratio 7.25 |
|
Weights |
Empty 300 kg, fuel 106 kg, oil 4 kg, crew 150 kg, luggage 15 kg, load
275 kg, flying weight 575 kg, wing loading 51.43 kg/m2 |
Empty 295 kg, fuel 106 kg, oil 4 4 kg, crew 150 kg, luggage 45 kg, load
305 kg, flying weight 600 kg, wing loading 54 kg/m2 |
|
Performance |
Max. speed 210 km/h, cruising speed 180 km/h, climb to 1000 m 6 min., climb
2.8 m/sec., service ceiling 5400 m, range 1200 km |
Max. speed 230 km/h, cruising speed 180 km/h, service ceiling
6000 m, range 1200 km, max. range 2000 km |
