Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Lockheed CL-1200 (Lancer) Lightweight Jet-Powered Fighter / Interceptor Proposal.
1 x Pratt & Whitney TF30-P-100 afterburning turbofan engine developing 15,000lb of thrust dry and up to 25,000lb of thrust with afterburner.
Propulsion
1,448 mph
2,330 kph | 1,258 kts
Max Speed
60,696 ft
18,500 m | 11 miles
Service Ceiling
2,113 miles
3,400 km | 1,836 nm
Operational Range
60,000 ft/min
18,288 m/min
Rate-of-Climb