P-8 Poseidon vs Cirrus SR-20
Overview
The P-8 Poseidon and the Cirrus SR-20 are both Military Special Mission Aircraft, manufactured by Boeing and Cirrus respectively.
The P-8 Poseidon reaches 907 km/h β 3.2x the Cirrus SR-20's 287 km/h. The P-8 Poseidon has an operational range of 2,225 km vs 1,450 km for the Cirrus SR-20. The P-8 Poseidon operates at altitudes up to 12,500 m compared to 5,334 m for the Cirrus SR-20. At 85,820 kg MTOW, the P-8 Poseidon is 62:1 the Cirrus SR-20's 1,383 kg.
The P-8 Poseidon has been produced in 187 units vs 1,459 for the Cirrus SR-20. Unit cost is $150M for the P-8 Poseidon vs $0.63M for the Cirrus SR-20. The Cirrus SR-20 first flew 14 years before the P-8 Poseidon (1995 vs 2009).
| American maritime patrol and reconnaissance aircraft, developed in the early 21st century, used for anti-submarine warfare, anti-surface warfare, and intelligence, surveillance, and reconnaissance. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Boeing |
| First flight | 25 April 2009 |
| Year introduced | 2013 |
| Number produced | 187 units |
| Average unit price | $150 million |
| American civil utility aircraft, renowned from the late 20th century, extensively deployed in private aviation and flight training. | |
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| Origin country | πΊπΈ United States |
| Category | Military Special Mission Aircraft |
| Manufacturer | Cirrus |
| First flight | 21 March 1995 |
| Year introduced | 1999 |
| Number produced | 1459 units |
| Average unit price | $630K |
| Wing area | -- mΒ² |
| Wingspan | 37.6 m β |
| Height | 12.8 m β |
| Length | 39.5 m β |
| Maximum speed | 907 km/h β |
| Operational range | 2,225 km β |
| Service ceiling | 12,500 m β |
| Max. takeoff weight | 85,820 kg β |
| Empty weight | 62,730 kg β |
| Total thrust | 2 x 61 kN β |
| Wing area | 13.5 mΒ² |
| Wingspan | 11.7 m β |
| Height | 2.5 m β |
| Length | 8.0 m β |
| Maximum speed | 287 km/h β |
| Operational range | 1,450 km β |
| Service ceiling | 5,334 m β |
| Max. takeoff weight | 1,383 kg β |
| Empty weight | 943 kg β |
| Total thrust | 1 x 149 kW β |
Performance Radar Chart
Detailed Comparison
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