Comparison of McDonnell Douglas F-4 Phantom II and North American F-100 Super Sabre

Attribute	McDonnell Douglas F-4 Phantom II ×	North American F-100 Super Sabre ×
General
Manufacturer	McDonnell Douglas	North American Aviation NAA
Model	McDonnell Douglas F-4 Phantom II	North American F-100 Super Sabre
Country	United States	United States
Manufactured from (year)	1958	1953
Manufactured to (year)	1981	1959
Type	Fighter Jets	Fighter Jets
Icao	F4	F100
Performance
Engine	2x 2 × General Electric J79-GE-17A Turbojets	1x Pratt & Whitney J57-P-21/21A
Power, lbf (lbf)	17,900	16,000
Avionics	-	Minneapolis-Honeywell MB-3, AN/AJB-1B, AN/APR-26
Max cruise speed (km/h)	2,371	1,487
Approach speed (km/h)	-	300
Travel range (km)	2,815	3,211
Fuel economy (km/l)	0.205	-
Service ceiling (m)	18,898	15,240
Rate of climb (m/sec)	209.8	113.79
Take off distance (m)	1,370	-
Landing distance (m)	1,120	-
Weights
Max take off weight (kg)	28,030	15,800
Max landing weight (kg)	16,706	15,606
Max payload (kg)	8,500	3,190
Fuel tank capacity (l)	12,624	9,887
Dimensions
Seats	2	1
Exterior length (m)	19.2	15
Tail height (m)	5	4.95
Fuselage diameter (m)	-	1.6
Wing span (m)	11.7	11.8
Wing tips	No Winglets	No Winglets