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