E-8 Joint STARS vs Hawker 800
Overview
The E-8 Joint STARS and the Hawker 800 are both Military Special Mission Aircraft, manufactured by Boeing/Northrop Grumman and Hawker Beechcraft respectively.
Top speed is 853 km/h for the E-8 Joint STARS vs 830 km/h for the Hawker 800. The E-8 Joint STARS has an operational range of 6,821 km vs 5,232 km for the Hawker 800. The E-8 Joint STARS operates at altitudes up to 12,802 m compared to 12,497 m for the Hawker 800. At 152,407 kg MTOW, the E-8 Joint STARS is 12:1 the Hawker 800's 12,701 kg.
The E-8 Joint STARS has been produced in 17 units vs 650 for the Hawker 800. Unit cost is $250M for the E-8 Joint STARS vs $13.78M for the Hawker 800. The Hawker 800 first flew 11 years before the E-8 Joint STARS (1983 vs 1994).
| 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 |
| British mid-size twinjet corporate aircraft, known for its international charters and private operations since the mid-1980s. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Hawker Beechcraft |
| First flight | 26 June 1983 |
| Year introduced | 1983 |
| Number produced | 650 units |
| Average unit price | $13.8 million |
| Wing area | 283.4 mΒ² |
| 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 |
| Wing area | -- mΒ² |
| Wingspan | 16.6 m β |
| Height | 5.5 m β |
| Length | 15.6 m β |
| Maximum speed | 830 km/h β |
| Operational range | 5,232 km β |
| Service ceiling | 12,497 m β |
| Max. takeoff weight | 12,701 kg β |
| Empty weight | 7,108 kg β |
| Total thrust | 2 x 1,057 kgf β |
Performance Radar Chart
Detailed Comparison
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