Lockheed U-2 vs. Max Holste M.H.1521 Broussard
... or view the full comparison list
here.
Lockheed U-2 |
versus |
Max Holste M.H.1521 Broussard |
19.2 m |
63 ft 0 in |
length |
10.46 m |
34 ft 4 in |
4.8 m |
15 ft 9 in |
height |
2.74 m |
9 ft |
32 m |
105 ft |
wingspan |
12.86 m |
42 ft 2 in |
1 × General Electric F118-101 |
engines |
1 x Lycoming GSO-480-B1A6 flat-six engine |
17,000 lbf (76 kN) |
thrust per engine |
Approximately 295 hp |
17,000 lbf (76 kN) |
total thrust |
Approximately 295 hp |
18,144 kg |
40,000 lb |
MTOW |
1,900 kg |
4,189 lb |
6,090 nm |
11,278 km |
range |
1,030 km |
556 nm |
475 mph |
764 km/h |
cruise speed |
145 mph |
233 km/h |
|
capacity |
5-7 passengers |
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.