Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the BAe P.103 Vertical Take-Off and Landing (VTOL) Fighter Study.
2 x Turbo-Union (Rolls-Royce, MBB, Aeritalia) RB.199-62R afterburning turbofan engines developing 20,750lb of thrust dry and up to 37,850lb of thrust with reheat; engines fitted to wing mainplane member tiling mechanism for VTOL operations.
Propulsion
1,553 mph
2,500 kph | 1,350 kts
Max Speed