Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Focke-Wulf Fw P.VII (P.7) Jet-and-Rocket-Powered Fighter Proposal.
1 x Heinkel HeS 011 turbojet engine developing 3,305 lb of thrust with 1 x Walter HWK 109-509A liquid rocket motor generating 3,750 lb of thrust.
Propulsion
593 mph
955 kph | 516 kts
Max Speed
45,276 ft
13,800 m | 9 miles
Service Ceiling
466 miles
750 km | 405 nm
Operational Range
3,600 ft/min
1,097 m/min
Rate-of-Climb