Specifications and Performance
General
Dynamics F-111C
| Engines
|
2
x Pratt & Whitney TF-30 turbofans
|
| Thrust
each (Dry) |
4
445kg
|
9
800lb
|
| Thrust
each (Afterburner) |
8
390kg
|
18
500lb
|
|
Wing
Span Extended 16°
|
21.3m
|
70ft
0in
|
| Wing
Span Swept 72.5° |
10.4m
|
33ft
11in
|
|
Length
|
23.5m
|
75ft
6.5in
|
|
Height
|
5.2m
|
17ft
0.5in
|
|
Weight
Basic *
|
23
300kg
|
51
300lb
|
|
Weight
Max Takeoff
|
51
845kg
|
114
300lb
|
|
Max
Speed (clean)
|
2
550km/h
|
1584mph
|
|
Cruising
Speed (high level)
|
780km/h
|
483mph
|
| Max
Mach (at sea level) |
1.5
|
|
| Max
Mach (at high level) |
2.5+
|
|
| Internal
Fuel Capacity |
12
316kg
|
33
000lb
|
| External
Fuel Tanks (2 x 600USG) each |
1
814kg
|
4
000lb
|
|
Initial
Climb
|
7 010m/min
|
23
000ft/min
|
|
Service
Ceiling
|
15
200m
|
50
000ft
|
|
Ferry
Range
|
5
560km
|
3
455miles
|
*
As displayed at QAM, A8-129 is estimated to weigh 23 000kg
|
