Comparison of Grumman F11F Tiger and North American F-100 Super Sabre

Attribute	Grumman F11F Tiger ×	North American F-100 Super Sabre ×
General
Manufacturer	Grumman	North American Aviation NAA
Model	Grumman F11F Tiger	North American F-100 Super Sabre
Country	United States	United States
Manufactured from (year)	1954	1953
Manufactured to (year)	1959	1959
Type	Fighter Jets	Fighter Jets
Icao	F11F	F100
Performance
Engine	1x Wright J65-W-18 afterburning turbojet	1x Pratt & Whitney J57-P-21/21A
Power, lbf (lbf)	10,500	16,000
Avionics	AN/ARC-27A UHF COMMS, AN/ARA-25 UHF, AN/ARR-40 UHF, AN/ARN-14E VHF Nav etc.	Minneapolis-Honeywell MB-3, AN/AJB-1B, AN/APR-26
Max cruise speed (km/h)	1,213	1,487
Approach speed (km/h)	-	300
Travel range (km)	2,056	3,211
Service ceiling (m)	12,771	15,240
Rate of climb (m/sec)	82.8	113.79
Weights
Max take off weight (kg)	10,641	15,800
^1↑Max landing weight (kg)	9,541	15,606
Max payload (kg)	1,360	3,190
Fuel tank capacity (l)	3,872	9,887
Dimensions
Seats	1	1
Exterior length (m)	13.98	15
Tail height (m)	4.03	4.95
Fuselage diameter (m)	0.7	1.6
Wing span (m)	9.64	11.8
Wing tips	No Winglets	No Winglets