E-3 Sentry AWACS vs E-4 NOAC
Overview
The E-3 Sentry AWACS and the E-4 NOAC are both Military Special Mission Aircraft, manufactured by Boeing and Boeing respectively.
Top speed is 853 km/h for the E-3 Sentry AWACS vs 969 km/h for the E-4 NOAC. The E-3 Sentry AWACS has an operational range of 7,400 km vs 12,600 km for the E-4 NOAC. The E-4 NOAC operates at altitudes up to 13,716 m compared to 10,668 m for the E-3 Sentry AWACS. At 374,850 kg MTOW, the E-4 NOAC is 2.5x the E-3 Sentry AWACS's 147,417 kg.
The E-3 Sentry AWACS has been produced in 68 units vs 4 for the E-4 NOAC. Unit cost is $270M for the E-3 Sentry AWACS vs $223M for the E-4 NOAC. The E-3 Sentry AWACS first flew 8 years before the E-4 NOAC (1972 vs 1980).
| American airborne early warning and control (AWACS) aircraft, principally used in NATO, UK, France, and Saudi Arabia since the Cold War. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Boeing |
| First flight | 9 February 1972 |
| Year introduced | 1977 |
| Number produced | 68 units |
| Average unit price | $270 million |
| 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 |
| Wing area | 283.0 mΒ² β |
| Wingspan | 44.4 m β |
| Height | 12.6 m β |
| Length | 46.6 m β |
| Maximum speed | 853 km/h β |
| Operational range | 7,400 km β |
| Service ceiling | 10,668 m β |
| Max. takeoff weight | 147,417 kg β |
| Empty weight | 83,915 kg β |
| Total thrust | 4 x 2,438 kgf β |
| 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 |
Performance Radar Chart
Detailed Comparison
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