Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Focke-Wulf Ta 283 Fighter-Interceptor Aircraft Proposal.
1 x HWK 509A bi-fuel liquid rocket engine with 2 x Focke-Wulf Pabst ramjet engines developing 2,645 lb of thrust.
Propulsion
693 mph
1,115 kph | 602 kts
Max Speed
32,808 ft
10,000 m | 6 miles
Service Ceiling
429 miles
690 km | 373 nm
Operational Range
4,000 ft/min
1,219 m/min
Rate-of-Climb