Attribute | ![]() Convair F-106 Delta Dart × | ![]() Mitsubishi F-2 × |
---|---|---|
General | ||
Manufacturer | Convair | Mitsubishi Heavy Industries |
Model | Convair F-106 Delta Dart | Mitsubishi F-2 |
Country | United States | Japan |
Manufactured from (year) | 1956 | 1995 |
Manufactured to (year) | 1968 | 2011 |
Type | Fighter Jets | Fighter Jets |
Icao | F106 | F2 |
Performance | ||
Engine | 1x Pratt & Whitney J75-P-17 | 1x General Electric F110-IHI-129 |
Power, lbf (lbf) | 24,500 | 29,500 |
Avionics | Hughes MA-1 Fire Control System & IBM Semi-Automatic Ground Environment | J/APG-2, AN/ARC-164, NEC V/UHF transceiver, Japan Aviation Electronics/Honeywell digital AFCS etc. |
Max cruise speed (km/h) | 2,454 | 2,124 |
Approach speed (km/h) | 267 | - |
Travel range (km) | 4,345 | 835 |
Service ceiling (m) | 17,374 | 17,983 |
Rate of climb (m/sec) | 152.4 | 243.84 |
Take off distance (m) | 1,280 | 450 |
Landing distance (m) | 1,341 | 650 |
Weights | ||
Max take off weight (kg) | 18,975 | 22,100 |
Max landing weight (kg) | 16,021 | 18,300 |
Max payload (kg) | 4,553 | 9,000 |
Fuel tank capacity (l) | 5,731 | 4,637 |
Dimensions | ||
Seats | 1 | 1 |
Exterior length (m) | 21.57 | 15.5 |
Tail height (m) | 6.18 | 5 |
Fuselage diameter (m) | 1.4 | 1.3 |
Wing span (m) | 11.68 | 11.1 |
Wing tips | No Winglets | No Winglets |