Fairchild Republic A-10 Thunderbolt II

An A-10 from the 81st Fighter Squadron, Spangdahlem Air Base, Germany was a ground-attack aircraft manufactured by Fairchild-Republic
First flight : 10 May 1972
Introduced : March 1977
Status : In service
Primary user : United States Air Force
Number built : 716
Unit cost : US$11.8 million (average, 1994 dollars)
General characteristics
Crew: 1
Length: 53 ft 4 in (16.26 m)
Wingspan: 57 ft 6 in (17.53 m)
Height: 14 ft 8 in (4.47 m)
Wing area: 506 ft² (47.0 m²)
Empty weight: 24,959 lb (11,321 kg)
Loaded weight: 30,384 lb (13,782 kg)
On CAS mission: 47,094 lb (21,361 kg)
On anti-armor mission: 42,071 lb (19,083 kg)
Max takeoff weight: 50,000 lb (23,000 kg)
Powerplant: 2× General Electric TF34-GE-100A turbofans, 9,065 lbf (40.32 kN) each
Performance
Never exceed speed: 450 knots (518 mph, 833 km/h) at 5,000 ft (1,500 m) with 18 Mk 82 bombs
Maximum speed: 381 knots (439 mph, 706 km/h) at sea level, clean
Cruise speed: 300 knots (340 mph, 560 km/h)
Stall speed: 120 knots (138 mph, 220 km/h)
Combat radius:
On CAS mission: 250 nmi (288 mi, 460 km) at 1.88 hour single-engine loiter at 5,000 ft (1,500 m), 10 min combat
On anti-armor mission: 252 nmi (290 mi, 467 km), 40 nm (45 mi, 75 km) sea-level penetration and exit, 30 min combat
Ferry range: 2,240 nmi (2,580 mi, 4,150 km) with 50 knot (55 mph, 90 km/h) headwinds, 20 minutes reserve
Service ceiling: 45,000 ft (13,700 m)
Rate of climb: 6,000 ft/min (30 m/s)
Wing loading: 99 lb/ft² (482 kg/m²)
Thrust/weight: 0.3