E-4 NOAC vs E-8 Joint STARS
Overview
The E-4 NOAC and the E-8 Joint STARS are both Military Special Mission Aircraft, manufactured by Boeing and Boeing/Northrop Grumman respectively.
Top speed is 969 km/h for the E-4 NOAC vs 853 km/h for the E-8 Joint STARS. The E-4 NOAC has an operational range of 12,600 km vs 6,821 km for the E-8 Joint STARS. The E-4 NOAC operates at altitudes up to 13,716 m compared to 12,802 m for the E-8 Joint STARS. At 374,850 kg MTOW, the E-4 NOAC is 2.5x the E-8 Joint STARS's 152,407 kg.
The E-4 NOAC has been produced in 4 units vs 17 for the E-8 Joint STARS. Unit cost is $223M for the E-4 NOAC vs $250M for the E-8 Joint STARS. The E-4 NOAC first flew 14 years before the E-8 Joint STARS (1980 vs 1994).
| American advanced airborne command post, launched during the Cold War, extensively employed for national emergency operations. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Boeing |
| First flight | 1 January 1980 |
| Year introduced | 1974 |
| Number produced | 4 units |
| Average unit price | $223 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 | 510.0 mΒ² β |
| Wingspan | 59.7 m β |
| Height | 19.3 m β |
| Length | 70.5 m β |
| Maximum speed | 969 km/h β |
| Operational range | 12,600 km β |
| Service ceiling | 13,716 m β |
| Max. takeoff weight | 374,850 kg β |
| Empty weight | 190,000 kg β |
| Total thrust | 4 x 5,954 kgf 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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