Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Dassault Mirage IIIV-01 Vertical Take-Off and Landing (VTOL) Fighter Prototype Aircraft.
1 x SNECMA (Pratt & Whitney) TF104B turbofan engine developing 19,842lb of thrust; 8 x Rolls Royce RB162 lift engines developing 4,410 lb of thrust each.
Propulsion
1,566 mph
2,520 kph | 1,361 kts
Max Speed
55,774 ft
17,000 m | 11 miles
Service Ceiling