A310 MRTT vs KC-130 Hercules
Overview
The A310 MRTT and the KC-130 Hercules are both Military Special Mission Aircraft, manufactured by Airbus and Lockheed Martin respectively.
Top speed is 978 km/h for the A310 MRTT vs 670 km/h for the KC-130 Hercules. The A310 MRTT has an operational range of 8,889 km vs 5,250 km for the KC-130 Hercules. The A310 MRTT operates at altitudes up to 12,497 m compared to 8,534 m for the KC-130 Hercules. At 163,998 kg MTOW, the A310 MRTT is 2.1x the KC-130 Hercules's 79,379 kg.
The A310 MRTT has been produced in 6 units vs 124 for the KC-130 Hercules. Unit cost is $108M for the A310 MRTT vs $22M for the KC-130 Hercules. The KC-130 Hercules first flew 43 years before the A310 MRTT (1960 vs 2003).
| European multirole tanker transport, with significant deployments in aerial refueling and strategic airlift operations. | |
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| Origin country | πͺπΊ Europe |
| Category | Military Special Mission Aircraft |
| Manufacturer | Airbus |
| First flight | 1 December 2003 |
| Year introduced | 2004 |
| Number produced | 6 units |
| Average unit price | $108 million |
| American military transport aircraft, noted for tactical refueling and cargo application, extensively operational during Cold War era and beyond. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Lockheed Martin |
| First flight | 1 January 1960 |
| Year introduced | 1962 |
| Number produced | 124 units |
| Average unit price | $22 million |
| Wing area | 219.0 mΒ² β |
| Wingspan | 43.9 m β |
| Height | 15.8 m β |
| Length | 47.5 m β |
| Maximum speed | 978 km/h β |
| Operational range | 8,889 km β |
| Service ceiling | 12,497 m β |
| Max. takeoff weight | 163,998 kg β |
| Empty weight | 113,999 kg β |
| Total thrust | 2 x 13,653 kgf β |
| Wing area | 162.0 mΒ² β |
| Wingspan | 40.4 m β |
| Height | 11.6 m β |
| Length | 29.8 m β |
| Maximum speed | 670 km/h β |
| Operational range | 5,250 km β |
| Service ceiling | 8,534 m β |
| Max. takeoff weight | 79,379 kg β |
| Empty weight | 34,274 kg β |
| Total thrust | 4 x 1,119 kW β |
Performance Radar Chart
Detailed Comparison
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