Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Hawker P.1103 Twin-Seat, Single-Engine Interceptor Proposal.
1 x de Havilland "Gyron" afterburning turbojet engine developing 20,000 thrust dry and 25,000lb of thrust with reheat.
Propulsion
870 mph
1,400 kph | 756 kts
Max Speed
68,898 ft
21,000 m | 13 miles
Service Ceiling
61,000 ft/min
18,593 m/min
Rate-of-Climb