KC-135 Stratotanker vs PA-32 Cherokee Six
Overview
The KC-135 Stratotanker and the PA-32 Cherokee Six are both Military Special Mission Aircraft, manufactured by Boeing and Piper respectively.
The KC-135 Stratotanker reaches 933 km/h — 4.1x the PA-32 Cherokee Six's 228 km/h. The KC-135 Stratotanker has an operational range of 2,400 km vs 1,361 km for the PA-32 Cherokee Six. The KC-135 Stratotanker operates at altitudes up to 15,240 m compared to 4,359 m for the PA-32 Cherokee Six. At 146,283 kg MTOW, the KC-135 Stratotanker is 150:1 the PA-32 Cherokee Six's 975 kg.
The KC-135 Stratotanker has been produced in 803 units vs 7,842 for the PA-32 Cherokee Six. The KC-135 Stratotanker first flew 4 years before the PA-32 Cherokee Six (1956 vs 1960).
| American refueling aircraft, deployed during Cold War, Desert Storm and ongoing operations worldwide for mid-air refueling missions. | |
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| Origin country | 🇺🇸 United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Boeing |
| First flight | 31 August 1956 |
| Year introduced | 1957 |
| Number produced | 803 units |
| Average unit price | $39 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 | 🇺🇸 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 | 226.0 m² ◉ |
| Wingspan | 39.9 m ◉ |
| Height | 12.7 m ◉ |
| Length | 41.5 m ◉ |
| Maximum speed | 933 km/h ◉ |
| Operational range | 2,400 km ◉ |
| Service ceiling | 15,240 m ◉ |
| Max. takeoff weight | 146,283 kg ◉ |
| Empty weight | 44,663 kg ◉ |
| Total thrust | 4 x 2,453 kgf ◉ |
| Wing area | 15.0 m² ◉ |
| Wingspan | 9.0 m ◉ |
| Height | 2.2 m ◉ |
| Length | 7.1 m ◉ |
| Maximum speed | 228 km/h ◉ |
| Operational range | 1,361 km ◉ |
| Service ceiling | 4,359 m ◉ |
| Max. takeoff weight | 975 kg ◉ |
| Empty weight | 545 kg ◉ |
| Total thrust | 1 x 112 kW ◉ |
Performance Radar Chart
Detailed Comparison
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