Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Folland Fo.148 Swing-Wing Trainer / Light Strike Aircraft Proposal.
1 x Rolls-Royce RB.153-61 afterburning turbojet engine developing 6,720lb of thrust dry and 11,750lb of thrust with reheat; thrust-reverser capability.
Propulsion
1,572 mph
2,530 kph | 1,366 kts
Max Speed
49,213 ft
15,000 m | 9 miles
Service Ceiling
1,118 miles
1,800 km | 972 nm
Operational Range
20,000 ft/min
6,096 m/min
Rate-of-Climb