Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the LTV XC-142A Vertical / Short Take-Off and Landing (V/STOL) Experimental Aircraft.
4 x General Electric T64-GE-1 turboprop engines developing 2,850 to 3,080 horsepower each and driving four-bladed propeller units.
Propulsion
432 mph
695 kph | 375 kts
Max Speed
25,000 ft
7,620 m | 5 miles
Service Ceiling
3,790 miles
6,100 km | 3,294 nm
Operational Range
6,800 ft/min
2,073 m/min
Rate-of-Climb