Specifications
Data from Airwar Specifications
General characteristics
- Crew: 2
- Length: 13.41 m (46 ft)
- Wingspan: 11.83 m (38 ft 10 in)
- Height: 3.76 m (12 ft 4 in)
- Airfoil: NACA 65-213
- Empty weight: 3,856 kg (10,284 lb)
- Loaded weight: 6,532 kg (14,400 lb)
- Max. takeoff weight: 7,364 kg (20,000 lb)
- Powerplant: 2 × Garrett TFE731-3A turbofan, 3,700 lbf (16.5 kN) each
- Fuel capacity:
- Internal fuel capacity: 3,191 litres
- Total fuel capacity: 4,932 litres
Performance
- Range:
- Internal fuel: 1960 nmi (3,630 km)
- Internal and external fuel: 2,600 nmi (4,815 km)
- Service ceiling: 40,000 ft (12,192 m)
- Rate of climb: 4900 ft/min (1,494 m/min) at sea level. (985 ft/min at altitude)
- Fuel consumption: 23.3 mg/(N·s).
Armament
A total of 2,700 kg of armament on 10 underwing hardpoints.
T-33A Shooting Star | Boeing Skyfox | |
---|---|---|
Empty weight | 15095 lb (6,847 kg) | 16235 lb (7,364 kg) |
Rate of climb at Sea Level | 3,400 ft/min (1,036 m/min) | 4,300 ft/min (1,490 m/min) |
Time to 9,144 m | 15 min | 8 min and 12 sec |
Operating range | 2,315 km | 3,630 km (Internal fuel) 4,815 km (Internal and external fuel) |
Operating endurance | 2 hours | 5.1 hours (Internal fuel) 7 hours (Internal and external fuel) |
Takeoff distance | 4,600 ft (1,402 m) | 2,600 ft (793 m) |
Read more about this topic: Boeing Skyfox