E-8 Joint STARS vs PA-32 Cherokee Six
Overview
The E-8 Joint STARS and the PA-32 Cherokee Six are both Military Special Mission Aircraft, manufactured by Boeing/Northrop Grumman and Piper respectively.
The E-8 Joint STARS reaches 853 km/h β 3.7x the PA-32 Cherokee Six's 228 km/h. The E-8 Joint STARS has an operational range of 6,821 km vs 1,361 km for the PA-32 Cherokee Six. The E-8 Joint STARS operates at altitudes up to 12,802 m compared to 4,359 m for the PA-32 Cherokee Six. At 152,407 kg MTOW, the E-8 Joint STARS is 156:1 the PA-32 Cherokee Six's 975 kg.
The E-8 Joint STARS has been produced in 17 units vs 7,842 for the PA-32 Cherokee Six. The PA-32 Cherokee Six first flew 34 years before the E-8 Joint STARS (1960 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 |
| American light, single-engined aircraft, dominant during the late 20th century, widely used for personal, commercial air taxi services. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Piper |
| First flight | 14 January 1960 |
| Year introduced | 1965 |
| Number produced | 7842 units |
| Average unit price | -- |
| 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 |
| Wing area | 15.0 mΒ² β |
| Wingspan | 9.0 m β |
| Height | 2.2 m β |
| Length | 7.1 m β |
| Maximum speed | 228 km/h β |
| Operational range | 1,361 km β |
| Service ceiling | 4,359 m β |
| Max. takeoff weight | 975 kg β |
| Empty weight | 545 kg β |
| Total thrust | 1 x 112 kW β |
Performance Radar Chart
Detailed Comparison
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