|
Specifications and Performance
Bell
UH-1H Iroquois
| Engine |
1
x 1 400shp (1 044kW) Lycoming T53-L-13 turboshaft |
|
Rotor
Span
|
14.63m
|
48ft
0in
|
|
Fuselage
Length
|
12.77m
|
41ft
11in
|
|
Height
|
4.42m
|
14ft
6in
|
|
Rotor
Disc Area
|
168.11sq
m
|
1
809.56sq ft
|
|
Weight
Empty
|
2
521kg
|
9
500lb
|
|
Weight
Loaded
|
4
309kg
|
2
850lb
|
|
Max
Speed
|
204km/h
|
127mph
|
|
Cruising
Speed
|
204km/h
|
127mph
|
|
Initial
Climb
|
487m/min
|
1
600ft/min
|
|
Service
Ceiling
|
3
840m
|
12
600ft
|
|
Range
|
512km
|
318mile
|
|
Compiled
by Don Cameron
|
