AC-130 vs E-8 Joint STARS
Overview
The AC-130 and the E-8 Joint STARS are both Military Special Mission Aircraft, manufactured by Lockheed Martin and Boeing/Northrop Grumman respectively.
Top speed is 669 km/h for the AC-130 vs 853 km/h for the E-8 Joint STARS. The AC-130 has an operational range of 4,800 km vs 6,821 km for the E-8 Joint STARS. The E-8 Joint STARS operates at altitudes up to 12,802 m compared to 9,144 m for the AC-130. At 152,407 kg MTOW, the E-8 Joint STARS is 2.2x the AC-130's 70,307 kg.
The AC-130 has been produced in 21 units vs 17 for the E-8 Joint STARS. Unit cost is $150M for the AC-130 vs $250M for the E-8 Joint STARS. The AC-130 first flew 27 years before the E-8 Joint STARS (1967 vs 1994).
| American gunship, deployed in Vietnam and Iraq wars, known for long duration, low-level ground attack and close air support missions. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Lockheed Martin |
| First flight | 1 January 1967 |
| Year introduced | 1968 |
| Number produced | 21 units |
| Average unit price | $150 million |
| American command and control aircraft, instrumental during Persian Gulf War, primarily deployed for surveillance and ground-target tracking missions. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Boeing/Northrop Grumman |
| First flight | 1 January 1994 |
| Year introduced | 1996 |
| Number produced | 17 units |
| Average unit price | $250 million |
| Wing area | 162.2 mΒ² β |
| Wingspan | 40.4 m β |
| Height | 11.7 m β |
| Length | 29.8 m β |
| Maximum speed | 669 km/h β |
| Operational range | 4,800 km β |
| Service ceiling | 9,144 m β |
| Max. takeoff weight | 70,307 kg β |
| Empty weight | 33,063 kg β |
| Total thrust | 4 x 915 kW β |
| Wing area | 283.4 mΒ² β |
| Wingspan | 44.4 m β |
| Height | 13.0 m β |
| Length | 46.6 m β |
| Maximum speed | 853 km/h β |
| Operational range | 6,821 km β |
| Service ceiling | 12,802 m β |
| Max. takeoff weight | 152,407 kg β |
| Empty weight | 77,564 kg β |
| Total thrust | 4 x 2,177 kgf β |
Performance Radar Chart
Detailed Comparison
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