Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Gloster E.28/39 Single-Seat, Single-Engine Experimental Prototype Aircraft.
1 x Power Jets W.1 turbojet engine developing 860 lb of thrust.
Propulsion
339 mph
545 kph | 294 kts
Max Speed
32,005 ft
9,755 m | 6 miles
Service Ceiling
407 miles
655 km | 354 nm
Operational Range
1,065 ft/min
325 m/min
Rate-of-Climb