T-55
From ERPC Wiki Archive
| T-55 | |
|---|---|
| Lua error: Internal error: The interpreter has terminated with signal "1". </div> | |
| Role | |
| Manufacturer | somebody |
| Introduction | 1558 |
| Retired | n/a |
| Status | operational |
| Produced | ### |
Design[edit]
Variants[edit]
Specifications[edit]
- Crew: 2
- Length: 13.14 m (43.1 ft)
- Wingspan: 9.45 m (31 ft) (with wingtip missiles)
- Height: 4.94 m (16.2 ft)
- Empty weight: 6,470 kg (14,285 lb)
- Max takeoff weight: 12,300 kg (27,300 lb)
- Powerplant: 1× afterburning turbofan
- Dry thrust: 53.07 kN (11,925 lbf)
- Thrust with afterburner: 78.7 kN (17,700 lbf)
- Maximum speed: Mach 1.5
- Range: 1,851 km
- Service ceiling: 14,630 m
- Rate of climb: 11,887 m/min
- Thrust/weight: 0.96
- Max g limit: -3 g / +8 g
- Guns: 1× 20 mm 3-barrel rotary cannon
- Hardpoints: 7 with x4 underwing x2 wingtip and one under fuselage; holding up to 3,740 kg of payload
Operators[edit]
