| TECHNICAL
SPECIFICATIONS ( F-89D) |
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General characteristics
- Crew: 2
- Length: 53 ft 10 in (16.4 m)
- Wingspan: 60 ft 5 in (18.4 m)
- Height: 17 ft 6 in (5.3 m)
- Wing area: 606 ft (56.3 m)
- Empty weight: 24,200 lb (11,000 kg)
- Loaded weight: 42,250 lb (19,200 kg)
- Max takeoff weight: 46,800 lb (21,200 kg)
- Powerplant: 2 x Allison J35-A-35A afterburning turbojets
- Dry thrust: 5,600 lbf (24.9 kN) each
- Thrust with afterburner: 7,400 lbf (32.9 kN) each
Performance
- Maximum speed: 636 mph (553 knots, 1,020 km/h)
- Range: 1,367 mi (1,188 nm, 2,200 km)
- Service ceiling 49,200 ft (15,000 m)
- Rate of climb: 8,360 ft/min (42.5 m/s)
- Wing loading: 69.7 lb/ft (340.4 kg/m)
- Thrust/weight: 0.35 (3.4 N/kg)
Armament
- Rockets:
- 104 x 70 mm (2.75 in) "Mighty Mouse" folding-fin aerial rockets
- 16 x 127 mm (5 in) aerial rockets on underwing racks or
- Bombs: 3,200 lb (1,500 kg)
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