Lockheed L-1011 TriStar 500 vs. McDonnell Douglas F-4 Phantom II

versus
... or view the full comparison list here.
Lockheed L-1011 TriStar 500 versus McDonnell Douglas F-4 Phantom II
50.05 m 164 ft 3 in length 19.2 m 63 ft 0 in
16.87 m 55 ft 4 in height 5.03 m 16 ft 6 in
50.09 m 164 ft 4 in wingspan 11.72 m 38 ft 5 in
3 Rolls-Royce RB211 engines engines Two General Electric J79s
42,000 lbf thrust per engine 17,900 lbs
126,000 lbf (3 engines x 42,000 lbf per engine) total thrust 35,800 lbs
231,330 kg 510,000 lb MTOW 27,965 kg 61,700 lb
11,260 km 6,100 nm range 3,031 km 1,636 nm
525 knots 972 km/h cruise speed Mach 2.2 2,717 km/h
Max. 315 passengers (typical 253) capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.