Attribute | ![]() Convair F-106 Delta Dart × | ![]() North American F-100 Super Sabre × |
---|---|---|
General | ||
Manufacturer | Convair | North American Aviation NAA |
Model | Convair F-106 Delta Dart | North American F-100 Super Sabre |
Country | United States | United States |
Manufactured from (year) | 1956 | 1953 |
Manufactured to (year) | 1968 | 1959 |
Type | Fighter Jets | Fighter Jets |
Icao | F106 | F100 |
Performance | ||
Engine | 1x Pratt & Whitney J75-P-17 | 1x Pratt & Whitney J57-P-21/21A |
Power, lbf (lbf) | 24,500 | 16,000 |
Avionics | Hughes MA-1 Fire Control System & IBM Semi-Automatic Ground Environment | Minneapolis-Honeywell MB-3, AN/AJB-1B, AN/APR-26 |
Max cruise speed (km/h) | 2,454 | 1,487 |
Approach speed (km/h) | 267 | 300 |
Travel range (km) | 4,345 | 3,211 |
Service ceiling (m) | 17,374 | 15,240 |
Rate of climb (m/sec) | 152.4 | 113.79 |
Take off distance (m) | 1,280 | - |
Landing distance (m) | 1,341 | - |
Weights | ||
Max take off weight (kg) | 18,975 | 15,800 |
Max landing weight (kg) | 16,021 | 15,606 |
Max payload (kg) | 4,553 | 3,190 |
Fuel tank capacity (l) | 5,731 | 9,887 |
Dimensions | ||
Seats | 1 | 1 |
Exterior length (m) | 21.57 | 15 |
Tail height (m) | 6.18 | 4.95 |
Fuselage diameter (m) | 1.4 | 1.6 |
Wing span (m) | 11.68 | 11.8 |
Wing tips | No Winglets | No Winglets |