Airbus A321neo vs. Grumman OV-1 Mohawk
... or view the full comparison list
here.
Airbus A321neo |
versus |
Grumman OV-1 Mohawk |
44.51 m |
146 ft 0 in |
length |
12.52 m |
41 ft 1 in |
11.76 m |
38 ft 7 in |
height |
3.89 m |
12 ft 9 in |
35.8 m |
117 ft 5 in |
wingspan |
14.63 m |
48 ft |
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
2 x Lycoming T53 turboprop engines |
35,000 lb |
thrust per engine |
Approximately 1,100 hp each |
70,000 lb |
total thrust |
Approximately 2,200 hp total |
97,000 kg |
213,800 lb |
MTOW |
14,950 lb |
6,781 kg |
7,400 km |
4,000 nm |
range |
1,690 km |
913 nm |
828 km/h |
514 mph |
cruise speed |
230 mph |
370 km/h |
180 to 220 passengers |
capacity |
Pilot and observer |
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.