E-2 Hawkeye vs E-8 Joint STARS
Overview
The E-2 Hawkeye and the E-8 Joint STARS are both Military Special Mission Aircraft, manufactured by Grumman and Boeing/Northrop Grumman respectively.
Top speed is 648 km/h for the E-2 Hawkeye vs 853 km/h for the E-8 Joint STARS. The E-2 Hawkeye has an operational range of 2,708 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 10,577 m for the E-2 Hawkeye. At 152,407 kg MTOW, the E-8 Joint STARS is 2.7x the E-2 Hawkeye's 57,500 kg.
The E-2 Hawkeye has been produced in 313 units vs 17 for the E-8 Joint STARS. Unit cost is $232M for the E-2 Hawkeye vs $250M for the E-8 Joint STARS. The E-2 Hawkeye first flew 34 years before the E-8 Joint STARS (1960 vs 1994).
| American all-weather, carrier-capable tactical airborne early warning aircraft, significant for its Cold War to contemporary deployments. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Grumman |
| First flight | 21 October 1960 |
| Year introduced | 1964 |
| Number produced | 313 units |
| Average unit price | $232 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 | 65.0 mΒ² β |
| Wingspan | 24.6 m β |
| Height | 5.6 m β |
| Length | 17.6 m β |
| Maximum speed | 648 km/h β |
| Operational range | 2,708 km β |
| Service ceiling | 10,577 m β |
| Max. takeoff weight | 57,500 kg β |
| Empty weight | 19,536 kg β |
| Total thrust | 2 x 1,902 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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