FORCETALLY
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At a glance
Measured figures
Il-76MD-90AE · Length
Single source46.6 m (152 ft 11 in)[source]
Configuration
| Specification | Ilyushin Il-76 | KC-130J |
|---|---|---|
| Type | Strategic and tactical airlifter[source] | — |
| National origin | Soviet Union / Russia[source] | — |
| Designer | Ilyushin[source] | — |
| Built by | Tashkent Aviation Production Association (formerly) Aviastar-SP[source] | — |
| Status | In service[source] | — |
| Primary users | Soviet Air Forces (historical) Russian Aerospace Forces People's Liberation Army Air Force Indian Air Force |
KC-130J
KC-130J · Dimensions · KC-130J
Single sourceKC-130J · Only the source-declared variant KC-130J · KC-130J
Single source97 ft 9 in (29.79 m)[source]Only the source-declared variant KC-130J
29.79 m[source]KC-130J · Dimensions
97 feet 9 inches (29.79 meters)[source]KC-130J
Il-76MD-90AE · Height
Single source14.42 m (47 ft 4 in)[source]
KC-130J · Dimensions · KC-130J
Single sourceKC-130J · Only the source-declared variant KC-130J · KC-130J
Single sourceKC-130J · Tail Height
Single source38 ft 10 in (11.84 m)[source]Only the source-declared variant KC-130J
11.66 m[source]KC-130J · Dimensions
(Tail Height) 38 feet 3 inches (11.66 meters)[source]KC-130J
Empty; Il-76MD-90AE · Il-76TD-90
Single sourceMaximum take-off; Il-76MD-90AE · Il-76MD-90A
Single source92,500 kg (203,928 lb) Il-76TD-90[source]
210,000 kg (462,971 lb) Il-76MD-90A[source]
Empty; KC-130J · Only the source-declared variant KC-130J · KC-130J
Single sourceGross; KC-130J · Only the source-declared variant KC-130J · KC-130J
Single sourceIl-76MD-90AE · Crew
Single sourceKC-130J · Only the source-declared variant KC-130J · KC-130J · two pilots, one crew chief and one loadmaster are minimum crew
Single sourceKC-130J · System · KC-130J · 2 pilots, navigator, flight engineer, radio operator/loadmaster
Single source4 (two pilots, one crew chief and one loadmaster are minimum crew)[source]Only the source-declared variant KC-130J
5 (2 pilots, navigator, flight engineer, radio operator/loadmaster)[source]KC-130J · System
Five (two pilots, one ACS operator and two loadmasters)[source]KC-130J · KC-130J Tanker
Pilot, co-pilot and crewmaster[source]KC-130J
Cruise; Il-76MD-90AE · Cruise speed
Single source750–800 km/h (470–500 mph, 400–430 kn)[source]
Cruise; KC-130J · Only the source-declared variant KC-130J · KC-130J
Single sourceMaximum; KC-130J · Only the source-declared variant KC-130J · KC-130J
Single source362 kn (417 mph, 670 km/h)[source]Only the source-declared variant KC-130J
348 kn (400 mph, 644 km/h)[source]Only the source-declared variant KC-130J
Ferry; Il-76MD-90AE · Il-76MD-90A with no payload
Single sourceIl-76MD-90AE · Il-76MD-90A with 52 t (51 long tons; 57 short tons) payload
Single source5,000 km (3,100 mi, 2,700 nmi) Il-76MD-90A with 52 t (51 long tons; 57 short tons) payload.[source]
9,700 km (6,000 mi, 5,200 nmi) Il-76MD-90A with no payload.[source]
KC-130J
Single sourceKC-130J · /6,570.90 kilometers
Single sourceKC-130J · Only the source-declared variant KC-130J · KC-130J · 4 × Allison T56 and Rolls-Royce AE 2100D3 turboprop engines, 4,637 shp ( ) each
Single source4 × Allison T56 and Rolls-Royce AE 2100D3 turboprop engines, 4,637 shp (3,458 kW) each[source]Only the source-declared variant KC-130J
Il-76MD-90AE · 4 × Aviadvigatel PS-90 A-76 turbofans thrust each
Single source4 × Aviadvigatel PS-90 A-76 turbofans , 156.9 kN (35,300 lbf) thrust each[source]
Il-76MD-90AE · Service ceiling
Single source12,200 m (40,000 ft)[source]
KC-130J · System · KC-130J
Single source19,356 kg[source]KC-130J · System
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Number built | 981[source] | — |
|---|
| Manufactured | 1971–present[source] | — |
|---|
| Introduction date | June 1974 ( June 1974 )[source] | — |
|---|
| First flight | 25 March 1971 ( 25 March 1971 )[source] | — |
|---|
| Variants | Ilyushin Il-78 Beriev A-50 Beriev A-60 Beriev A-100 Shaanxi KJ-2000[source] | — |
|---|
| Capacity | Il-76M 42,000 kg (93,000 lb); Il-76MD 48,000 kg (106,000 lb); Il-76MD-90A 60,000 kg (130,000 lb)[source] | 42,000 lb (19,051 kg)[source]Only the source-declared variant KC-130J |
|---|
| Guns | 2 × 23 mm (0.906 in) cannon in radar-directed manned turret at base of tail[source] | — |
|---|
| Thrust/weight | 0.32 at 200 t (200 long tons; 220 short tons) take-off weight and max. take-off thrust[source] | — |
|---|
| Minimum landing run | 450 m (1,480 ft) with thrust reversers[source] | — |
|---|
| Bombs | Some military models have four hardpoints under each outer wing capable of supporting 500 kg (1,100 lb) bombs.[source] | — |
|---|
| Hardpoints | Bombs: Some military models have four hardpoints under each outer wing capable of supporting 500 kg (1,100 lb) bombs.[source] | — |
|---|
| Manufacturer | Ilyushin, Tashkent Mechanical Plant, Aviastar-SP[source] | Lockheed Martin, Marietta, Ga.[source]KC-130J · System Lockheed Martin[source]KC-130J · KC-130J Tanker |
|---|
| Variant description | — | KC-130J[source]Only the source-declared variant KC-130J Variant from C-130J[source]Only the source-declared variant KC-130J |
|---|
| Airfoil | — | root: NACA 64A318 ; tip: NACA 64A412[source]Only the source-declared variant KC-130J |
|---|
| Fuel capacity | — | 61,364 lb (27,834 kg) (with external tanks)[source]Only the source-declared variant KC-130J |
|---|
| Propellers | — | 6-bladed Dowty R391 constant-speed fully feathering reversible-pitch composite propellers[source]Only the source-declared variant KC-130J |
|---|
| Take-off run | — | 3,127 ft (953 m) at 155,000 lb (70,307 kg)[source]Only the source-declared variant KC-130J |
|---|
| Country of origin | — | United States[source]Inventory Origin column; table 1, row 23, cell 2; revision 1374114200 United States[source]KC-130J |
|---|
| Source measurement | — | KC-130J[source]KC-130J · System Multirole Tactical Tanker[source]KC-130J · System 4[source]KC-130J · System INA[source]KC-130J · System 13,629 liter[source]KC-130J · System 25.91 m[source]KC-130J · System 2,272 liters per minute[source]KC-130J · System 40.41 m[source]KC-130J · Dimensions 162.12 m sq[source]KC-130J · Dimensions 2.77 m[source]KC-130J · Dimensions 3.05 m[source]KC-130J · Dimensions 12.22 m[source]KC-130J · Dimensions 2.81 m[source]KC-130J · Dimensions 3.30 m[source]KC-130J · Dimensions 129 cu m[source]KC-130J · Dimensions 34,686 kg[source]KC-130J · Dimensions 70,310 kg[source]KC-130J · Dimensions 25.91 m[source]KC-130J · Dimensions 4 x Allison T56-A-15[source]KC-130J · Automotive Turboprop[source]KC-130J · Automotive 4,591 hp each[source]KC-130J · Automotive 36,636 liters internal[source]KC-130J · Automotive 602 km/h[source]KC-130J · Automotive 556 km/h[source]KC-130J · Automotive 185 km/h[source]KC-130J · Automotive 1,091 m[source]KC-130J · Automotive 518 m[source]KC-130J · Automotive 579 m/min[source]KC-130J · Automotive 10,060 m[source]KC-130J · Automotive 3,791 km[source]KC-130J · Automotive 7,876 km[source]KC-130J · Automotive 7,010 m[source]KC-130J · Automotive 142 m[source]KC-130J · Automotive None[source]KC-130J · Protection No[source]KC-130J · Protection INA[source]KC-130J · Protection INA[source]KC-130J · Protection INA[source]KC-130J · Protection INA[source]KC-130J · Protection |
|---|
| Passengers | — | 92 troops or 64 paratroops[source]KC-130J |
|---|
KC-130J · Max. recommended gross take-off
Single sourceMaximum take-off; KC-130J · Dimensions · KC-130J
Single sourceMaximum take-off; KC-130J · KC 130J Tanker · KC-130J
Single sourceMaximum take-off; KC-130J · Only the source-declared variant KC-130J · KC-130J
Single source75,562 lb (34,274 kg)[source]Only the source-declared variant KC-130J
164,000 lb (74,389 kg)[source]Only the source-declared variant KC-130J
175,000 lb (79,379 kg)[source]Only the source-declared variant KC-130J
79,380 kg[source]KC-130J · Dimensions
164,000 lbs[source]KC-130J · KC 130J Tanker
Max. recommended gross take-off: 164,000 pounds (74,389 kilograms)[source]KC-130J
KC-130J · KC-130J Tanker · KC-130J
Single sourceKC-130J · Only the source-declared variant KC-130J · KC-130J
Single source