Y-30 - Specifications
| C-130J | Y-30 Notional | A400 | |
|---|---|---|---|
| External Dimensions | |||
| Wing Span | 132.6 ft / 40.41 m |
133 ft/ 41 meters |
135´ 10" / 41.40 m |
| Wing Aspect Ratio | 10.1 | ||
| Length (Overall) | 97.75 ft / 29.79 m |
114 ft/ 35 meters |
137´ 9" / 42.00 m |
| Height (Overall) | 38.8 ft / 11.84 m |
||
| Tailplane Span | 52.7 ft / 16.05 m |
||
| Wheel Track | 14.25 ft / 4.34 m |
||
| Propeller Diameter | 13.5 ft / 4.11 m |
||
| Wing Area (gross) | 1,745 sq. ft / 162.12 sq. m |
||
| Internal Dimensions | |||
| Cabin Length (excluding ramp) | 40 ft / 12.19 m |
74´ 4" / 22.65 m |
|
| Cabin Length (including ramp) | 50.7 ft / 15.44 m |
||
| Max. Width | 10.25 ft / 3.12 m |
11.5 ft / 3.5 m |
13´ 1" / 4.00 m |
| Max. Height | 9 ft / 2.74 m |
10.5 ft / 3.25 m |
12´ 8" / 3.85 m |
| Total useable volume | 4,551 cubic ft / 128.9 cubic m |
||
| Power Plant | |||
| Number and Model | 4 AE2100D3 Allison | 4 WJ-16 or 4 WJ-10 |
4 TP400-D6 EuroProp International |
| Power per unit | 6,000 shp | 5,072 hp or ~7,000 hp |
9500 SHP / 10,000 CV |
| Weights and loadings | |||
| Operating Empty Weight | 75,562 lbs / 34,274 kg |
||
| Max. Fuel Weight (internal) | 45,900 lbs / 20,519 kg |
||
| Max. Payload, 2.5 g | 41,790 lbs / 18,955 kg |
30 tons | 55,115 lb / 25,000 kg |
| Max. Normal Takeoff Weight | 155,000 lbs / 70,305 kg |
80 tons | 244,378 lb / 110.850 kg |
| Max. Overload Takeoff Weight | 175,000 lbs / 79,380 kg |
||
| Max. Normal Landing Weight | 130,000 lbs / 58,965 kg |
||
| Max. Overload Landing Weight | 155,000 lbs / 70,305 kg |
||
| Max Zero-Fuel Weight, 2.5 g | 117,350 lbs / 53,230 kg |
||
| Max. Wing Loading (normal) | 88.83 lb/sq ft / 433.7 kg/sq m |
||
| Max. Power Loading (normal) | 8.44 lbs/shp / 5.14 kg/kW |
||
| Performance (at max normal takeoff weight, unless indicated otherwise) | |||
| Max. Cruising Speed | 348 kts / 645 km/h |
600-700 km/h | 422 ktas |
| Economy Cruising Speed | 339 kts / 628 km/h |
Mach 0.68 | |
| Stalling Speed | 100 kts / 185 km/h |
||
| Max. Rate of Climb at Sea Level | 2,100 ft/min / 640 m/min |
||
| Time to 6,100 m | 12 min | ||
| Cruising Altitude | 28,000 ft / 8,535 m |
||
| Service Ceiling at 66,680 kg AUW | 30,560 ft / 9,315 m |
||
| Service Ceiling, OEI, at 66,680 kg AUW | 22,820 ft / 6,955 m |
||
| Takeoff Run | 3,290 ft / 1,003 m |
3,500´ / 1,067 m |
|
| Takeoff Run to 15 m | 4,700 ft / 1,433 m |
||
| Takeoff Run using max. effort procedures | 1,800 ft / 549 m |
||
| Landing from 15 m at 58,967 kg AUW | 2,550 ft / 777 m |
||
| Landing Run at 58,967 kg AUW | 1,400 ft / 427 m |
3,500´ / 1,067 m |
|
| Runway LCN: asphalt | 37 | ||
| Runway LCN: concrete | 42 | ||
| Range with 18,144 kg payload and MIL-C-5011A reserves | 2,835 nm / 5,250 km |
||
| Maximum Range | 6000-7000 km | 4,100 nm / 7,593 km |
|
| Range with Full Load | 2,100 nm / 4,000 km |
||
|
NEWSLETTER
|
| Join the GlobalSecurity.org mailing list |
|
|
|
