Specifications (FH-1 Phantom)
Data from McDonnell Douglas Aircraft since 1920 unless otherwise noted
General characteristics
- Crew: One
- Length: 37 ft 3 in (11.35 m)
- Wingspan: 40 ft 9 in; 16 ft 3 in with folded wings (12.42 m / 4.95 m)
- Height: 14 ft 2 in (4.32 m)
- Wing area: 276 sq ft (25.6 m²)
- Empty weight: 6,683 lb (3,031 kg)
- Loaded weight: 10,035 lb (4,552 kg)
- Max. takeoff weight: 12,035 lb (5,459 kg)
- Powerplant: 2 × Westinghouse J30-WE-20 turbojets, 1,600 lbf (7.1 kN) each
- Fuel capacity: 375 gal (1,420 l) internal, 670 gal (2,540 l) with external drop tank
Performance
- Maximum speed: 417 knots (479 mph, 771 km/h) at sea level
- Cruise speed: 216 knots (248 mph, 399 km/h)
- Range: 604 nmi (695 mi, 1,120 km)
- Ferry range: 852 nmi (980 mi, 1,580 km) with external drop tank
- Service ceiling: 41,100 ft (12,525 m)
- Rate of climb: 4,230 ft/min (21.5 m/s)
- Wing loading: 36.4 lb/ft² (178 kg/m²)
- Thrust/weight: 0.32
Armament
- Guns: 4 × .50 in (12.7 mm) machine guns
- Rockets: 8 × 5 in (127 mm) High Velocity Aircraft Rockets
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