Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the SNECMA C.450-01 Vertical Take-Off and Landing (VTOL) Research Aircraft.
1 x SNECMA Atar 101 E5V turbojet engine developing 8,160lb of thrust.
Propulsion
497 mph
800 kph | 432 kts
Max Speed
9,843 ft
3,000 m | 2 miles
Service Ceiling