|
C-130J Super Hercules
| C-130J Super Hercules
| C-17 Globemaster III
| C-27J Spartan
| C-295/CN235 Joint Cargo Aircraft
| C-295/CN235 Joint Cargo Aircraft
| C-5 Galaxy
| KC-10 Extender
| KC-135 Stratotanker
| KC-30 MRTT
| KC-767 GlobalTanker
|
| Version
| C-130J |
C-130J-30 |
C-17 Globemaster III |
C-27J |
C-295 |
CN-235 |
C-5B Galaxy |
KC-10 |
KC-135E |
KC-30 |
KC-767A |
| Country
| USA |
USA |
USA |
USA/ Italy |
USA/ EU |
USA/ EU |
USA |
USA |
USA |
USA |
USA |
| Type
| Medium tactical and multi-role transport |
Medium tactical and multi-role transport |
Cargo and troop transport |
Medium Tactical Airlift |
Airlift |
Airlift |
Massive strategic transport |
Aerial tanker and transport |
Aerial refueling and airlift |
Tanker/ Cargo Aircraft |
Aerial refueling and airlift |
| Powerplant
| Rolls-Royce AE 2100D3 turboprops (4x) |
Rolls-Royce AE 2100D3 turboprops (4x) |
P&W F117-PW-100 turbofan engine (4x) |
Rolls-Royce E 2100D2 (2x) |
Pratt & Whitney PW127G (2x) |
General Electric CT7-9C3 (2x) |
GE TF39-GE-1C turbofan (4x) |
GE CF6-50C2 turbofans (3x) |
Pratt and Whitney TF-33-PW-102 turbofan engine (4x) |
GE CF6-80E1A4 | P&W PW 4168A |
Pratt & Whitney PW4062 engine (2x) or General Electric CF6-90C2B6F engine (2x) |
| Engine thrust
| 4,700 SHP |
4,700 SHP |
40,440 lbs, each engine |
4,637 SHP |
2,645 shp each one |
1.750 shp each one |
41,000 lbs 183kN each engine |
52,500 lbs 23,625kg, each engine |
18,000 lbs each engine |
GE: 72,000 lbs | P&W: 68,000 lbs |
P&W: 63,000 pounds each engine | GE: 62,100 pounds each engine |
| Length
| 97.9 ft || 29.3 m |
112.9 ft || 34.69 m |
174ft 53.04m |
74.84 ft | 22.8 m |
24.50m | 80 ft 4 in |
21.40m | 70 ft 2 in |
247.1ft 75.53m |
181ft 54.4m |
136.3 ft 41.53 m |
193 ft. 7 in. |
159.2 ft | 48.51m |
| Height
| 38.8 ft || 11.84 m |
38.8 ft || 11.84 m |
55 ft 16,8m |
31.82 ft | 9.7 m |
8.5m | 28 ft 5 in |
7.9m | 26 ft 10 in |
65ft 19.81m |
58ft 17.4m |
41.8 ft 12.7 m |
57 ft. 1 in. |
52 ft | 15.85m |
| Wingspan
| 132.6 ft || 40.41 m |
132.6 ft || 40.41 m |
169.8 ft 51.74m |
94.16 ft | 28.7 m |
25.81m | 84 ft 8 in |
25.81m | 84 ft 8 in |
222.9ft 67.88m |
165ft 50m |
130.1 ft 39.88 m |
197 ft. 10 in. |
156.1 ft | 47.57m |
| Weight
| 155,000 lbs || 69,750 kg (Max TOW) |
164,000 lbs || 74,393 kg |
585,000 lbs 265,352kg (max takeoff) |
70,107 lb | 31,800 kg |
23,200 kg | 51,146 lb (Max TOW) |
16,500 kg | 36,376 lb (Max TOW) |
840,000 lbs 381,018kg (wartime max takeoff) |
590,000 lbs 265,500kg (max take-off) |
322,500 lbs 146,285 kg (max. TOW) |
513,700 lbs (Max TOW) |
395,000 lbs |179,169 kg (Max.TOW) |
| Speed
| 417 mph || 362 ktas || Mach 0.59 || at altitude |
410 mph || 356 ktas || Mach 0.58 at altitude |
500mph at altitude 8,534m Mach .74 |
325 KTAS | 600 kmh | 375 mph |
480 km/h | 260 ktas |
455 km/h | 246 ktas |
570mph 917km/h Mach 0.77 |
619mph Mach 0.825 |
530 mph at altitude |
611km/h | 380 mph |
543 mph @ 30,000 ft | 874 Km/h |
| Ceiling
| 28,000 ft || 8,615 m with 42,000 lb || 19,090 kg p |
26,000 ft || 8 km with 44,500 lb || 20,227 kg payl |
45,000ft at cruising speed 13,716m |
30,000 ft | 9,144 m |
7.620m | 25,000 ft (Normal Operating Altitude) |
7.620m | 25,000 ft (Normal Operating Altitude) |
33,000ft 10,058m |
42,000ft 12,727m |
50,000 ft 15,240 m |
n/a |
43,100 ft (FAA certified altitude) | 13,136.9m |
| Crew
| Three (two pilots and loadmast |
Three (two pilots and loadmast |
3 |
Three |
Two |
Three |
6 |
4 |
Three |
Three |
Three |
| Cost
| $48.5 Million (FY 1998 constant dollars) |
$48.5 Million (FY 1998 constant dollars) |
$202.3 million |
$20-27.5 million (estimate) |
$24-35 million (depending on electronics) |
$22-30 million |
$179 million (1998) |
$88.4 million (1998) |
$39.6 million (FY98 constant dollars) |
n/a |
Between $150 million and $225 million |
All Bombers
