Diamond DA62 vs P-8 Poseidon
Overview
The Diamond DA62 and the P-8 Poseidon are both Military Special Mission Aircraft, manufactured by Diamond and Boeing respectively.
The P-8 Poseidon reaches 907 km/h β 2.4x the Diamond DA62's 372 km/h. The Diamond DA62 has an operational range of 2,380 km vs 2,225 km for the P-8 Poseidon. The P-8 Poseidon operates at altitudes up to 12,500 m compared to 6,069 m for the Diamond DA62. At 85,820 kg MTOW, the P-8 Poseidon is 37:1 the Diamond DA62's 2,300 kg.
The Diamond DA62 has been produced in 120 units vs 187 for the P-8 Poseidon. Unit cost is $1.9M for the Diamond DA62 vs $150M for the P-8 Poseidon. The P-8 Poseidon first flew 3 years before the Diamond DA62 (2009 vs 2012).
| Austrian twin-engine, civil utility aircraft, used worldwide for light transport and aerial surveys in the 21st century. | |
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| Origin country | π¦πΉ Austria |
| Category | Military Special Mission Aircraft |
| Manufacturer | Diamond |
| First flight | 1 April 2012 |
| Year introduced | 2015 |
| Number produced | 120 units |
| Average unit price | $1.9 million |
| 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 |
| Wing area | 17.1 mΒ² |
| Wingspan | 14.6 m β |
| Height | 2.8 m β |
| Length | 9.2 m β |
| Maximum speed | 372 km/h β |
| Operational range | 2,380 km β |
| Service ceiling | 6,069 m β |
| Max. takeoff weight | 2,300 kg β |
| Empty weight | 1,590 kg β |
| Total thrust | 2 x 66 kW β |
| 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 |
Performance Radar Chart
Detailed Comparison
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